tender no.: mmd/a319, a320 & a321lg/02 date:...

Tender for Advance Exchange and Overhaul of landing gears for A319, A320 & A321 aircraft

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Tender no.: MMD/A319, A320 & A321LG/02

Date: 07/05/2018Close Date: 04/06/2018 - 1100 hrs. IST

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Dear Sirs,

Sub: Advance exchange and Overhaul of Installed landing gears for A319, A320 & A321

aircraft

INTRODUCTION

Air India Limited (AIL), the owner and operator of Air India, invites bids for advance

exchange and overhaul of 27 A320 family aircraft, Fifteen A319/A320 aircraft and Twelve

A321 aircraft as follows:-

The Advance Exchange landing gear and actuators shipset required in accordance with

delivery schedule.

Bidder must either bid for full A319/A320 fleet or full A321 fleet or both the fleets. Bidders

must provide in accordance with delivery schedule two advance exchange shipsets of

A319/A320 if bid is for A319/A320 fleet or two advance exchange shipsets for A321 if bid

is for A321 fleet or two advance exchange shipsets each for A319/A320 & A321 if bid is for

both fleets of A319/A320 & A321.

All Landing gear sets shall be delivered to and collected from AI Facility at Kolkata for

A319 aircraft, Delhi for A320 aircraft and Mumbai for A321aircraft. Packing, custom

clearance and freight etc shall be handled by selected bidder.

INSTRUCTIONS FOR TENDERING

1.

The Bids should be neatly presented. Corrections, if any, should be duly authenticated with

full signature of the person who has signed the Bids, failing which such Bids are liable to be

rejected.

2. Before submitting the tender, the Bidders are requested to carefully examine the Tender

Documents, Terms & Conditions of Assignment, Specifications and if there should be or

appear to be any ambiguity therein they should immediately refer the matter to Air India

Ltd., for clarification.

3. The Bidder shall complete the annexed forms of Tender and information called for therein,

and shall sign with date each of the documents. The Bidder shall initial each page of the

Tender Document.

4. Bids received by Fax or through E-mail will be rejected.

5. The Tender shall accompany the document proofs for qualifying requirements. Documents

not required as part of the Tender should not be provided.


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. TABLE OF CONTENTS

S/N Particulars

1. Terms and Conditions of the tender Page 03-09

2. Delivery Schedule Annexure 1

3. Technical Requirements of Delivery Configuration Annexure 2

4. Technical Data Annexure 3 to 4

5. Technical Bid – Terms, Format & Evaluation Criteria Annexure 5

6. Price bid – Terms & & Evaluation Criteria Annexure 6

7. Price bid – Format Annexure 7

8. Undertaking certificate Annexure 8

9. Authorization for Attending Bid opening Annexure 9

10. Integrity Pact Annexure 10

SUBMISSION OF THE BIDS:

SEALED ENVELOPE - I: TECHNICAL BID

To be superscribed with “Technical Bid for Tender No.MMD/A319 A320 A321 LG/02 Due

on 04/06/2018”, and must contain the conditions as specified in Annexure 5. Please do not

include price & commercial terms in the technical bid.

SEALED ENVELOPE – II: PRICE BID

To be superscribed with “Price Bid for Tender No. MMD/A319 A320 A321 LG/02 Due on

04/06/2018”, and must contain the price bid strictly as per the Format given at Annexure 7.

Air India’s price bid terms are specified in Annexure 6.

MASTER ENVELOPE

Both sealed envelopes should be further sealed in a Master Envelope superscribed “Bid for

Tender No. MMD/A319 A320 A321 LG/02 Due on 04/06/2018”, with details such as bidder

name, address and contact numbers.

Time & Place of submission of bids:

The bids in sealed envelope must be submitted on or before 04/06/2018”1100 Hrs IST at the

following address:-

Materials Management Department

Air India Limited

New Engineering Complex, Sahar,

Vile Parle East, Near Chakala Cigerette Factory, Bamman Wada

Mumbai 400 099

INDIA

Ph: 0091-22-26168569, 8574

For Technical Query pls send email to address: [email protected] and for any

another query send email to address: [email protected]

Technical Bids shall be opened on 04/06/2018 at 11:30hrs at above given address

mailto:[email protected]

mailto:[email protected]


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TERMS & CONDITIONS OF THE TENDER

1 General Terms:

1.1 Tenders received after the closing date & time will not be considered.

1.2 In case the Price bid and the Technical Bid are enclosed in the same envelope and/ or in an

open condition instead of in two separate sealed / closed envelopes, such Bids will be

rejected.

1.3

The Bids should be neatly presented. Corrections, if any, should be duly authenticated with

full signature of the person who has signed the Bids, failing which such Bids are liable to be

rejected.

1.4 All bid documents as per attached annexures are to be submitted on bidder’s company letter-

head.

1.5 The Technical Bid should not contain any indication of price. In case, there is any indication

of the price quoted in the Technical Bid, such Bids will be rejected without any reference to

the bidder. No correspondence will be entertained in this regard.

1.6 All the prices quoted in Price bid should be in USD. In case, any bidder quotes in a currency

other than in USD, the IATA exchange as per Air India’s System on the date of opening of

the Price bids will be used for conversion from the quoted currency to USD for the purposes

of evaluation.

1.7 The prices finalized shall remain firm for the entire period of the awarded contract. All

exchange/ overhaul orders received during the period of contract must be completed by the

selected bidder at the contract price and terms & conditions.

1.8 In case of any deviations/ variations from the terms and conditions of the tender, including

technical terms and commercial terms, the same must be clearly specified/ indicated in the

Technical bid only.

1.9 Air India Ltd. does not bind itself to accept the lowest or any Tender and has the right to

refuse any Tender without assigning any reason or select any Bidder that is in the final

evaluation list. Air India Ltd. also has right to re-issue the Tender without Bidders having

right to object to such reissue.

1.10 Amendments and clarifications, if any, to this tender, will be hosted on the website of Air

India at www.airindia.in . The bidders are, therefore, advised to visit the websites regularly

till the date of closing of the tender. The last amendment, if any, will be hosted a minimum

of seven days before the closing date of the tender.

http://www.airindia.in/


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2. Earnest Money Deposit (hereinafter referred to as “EMD”)

2.1 The prospective Applicants/Bidders are required to submit an Earnest Money Deposit of

USD 25,000.00 (Twenty Five Thousand USD Only). EMD must be submitted by the

Applicant/Bidder by means of wire transfer in favour of Air India Limited, payable at

London, and should be submitted along with Annexure 5. The proof of remittance by wire

transfer is to be submitted along with Technical Bid. No other mode of payment is

acceptable.

2.2 Address/Bank details for wire transfer:

BENEFICIARY NAME : AIR INDIA LTD

USD ACCOUNT NO. : 11040057

NAME OF THE BANK : CITIBANK LONDON

SWIFT CODE : CITIGB2L

IBAN BANK CODE : GB98CITI18500811040057

ADDRESS : CITI GROUP CENTRE, CANARY WHARF, LONDON,

E 14, 5LB

BENEFICIARY : Air India limited

In case of any query relating to wire transfer of the EMD, the bidders may contact Mr.

Vijay Jadhav E-mail: [email protected]

2.3 EMD will not carry any interest.

2.4 EMD of the successful bidder would be retained for the entire contract period.

2.5 EMD of the unsuccessful bidders would be returned without interest after award of contract

to the successful bidder(s).

3. Validity of bids/ offers:

3.1 Prices offered should be valid for a period of 120 days from the closing date for submission

of bids.

3.2 No request for increase in the prices after close date of the tender will be entertained.

4. Agreement

4.1 The contract will be finalized and signed with bidder(s) who will provide in accordance

with delivery schedule two advance exchange shipsets of A319/A320 if bid is for

A319/A320 fleet or two advance exchange shipsets for A321 if bid is for A321 fleet or

two advance exchange shipsets each for A319/A320 & A321 if bid is for both fleets of

A319/A320 & A321 and undertake overhaul of removed landing gear shipsets.

Fifteen A319/A320 aircraft and Twelve A321 aircraft are scheduled to be covered

under the contract, however Air India reserves the right to amend/modify number of

aircraft under the contract.


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4.2 Air India will enter into two separate agreements with selected bidder(s) – one for advance

exchange & overhaul and other for logistics.

4.3 The prices finalized shall remain firm for the entire period of the contract. All exchange/

overhauling orders received during the period of contract must be completed by the selected

bidder at the contract price and terms & conditions.

4.4 A draft copy of the agreement must highlight each corresponding requirements of the

Tender Schedule. The clauses of the draft agreement must conform to the bid offer.

4.5 AIR INDIA LTD. reserves the right to accept / reject any or all the offers submitted or annul

the tender without assigning any reason whatsoever.

5. Validity of the Contract

5.1 The selected bidder for the respective advance exchange and overhaul of the landing gear

will enter into a contract for a period till completion of warranty period of the last gear.

5.2 The contract will have an option to extend the validity of contract by Two or more years by

mutual consent of both parties at same price, terms & conditions due to unforeseen reasons.

6. Payment

6.1 Payment term shall be 60 days from the date of receipt of invoice with all supporting

documents.

6.2 Invoice for advance exchange fee and Fixed Price overhaul charges can be raised after

delivery of advance exchange shipset.

Invoice for logistics can be raised after completion of delivery & return shipment of landing

gear shipset.

Invoices for Exceptions allowed on the Fixed Price if any, are to be submitted and upon

approval by Air India, same will be provided as separate invoice against service order raised

by Air India.

6.3 In case a bidder does not accept this payment term, the price bid would be loaded by

financing cost @ 18 % per annum for the difference between 60 days and the actual credit

period offered by the vendor for the offered amount.

6.4 No advance / pre payment term will normally be accepted. However, if any bidder requires

advance payment, such advance payment will be loaded by financing cost @ 18% per

annum. Advance payment is to be covered by counter Bank Guarantee by the bidder.

6.5 Invoicing address and the necessary contact references for payment will be notified in the

contract.

6.6 Please also indicate the volume discount (it should appear in the Price Bid).

6.7 Payment will be made through wire transfer. Full bank details such as name of Bank, Bank

Account No. and currency, IBAN No. and Swift Code, details of routing bank if any, where

payment is to be effected, should be furnished. Air-India will not accept payment terms of

bank guarantee, letter of credit (LOC) and IATA clearance.


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7. Security Deposit(SD) Successful bidder shall deposit within 15 days of signing of agreement of 5% of value of

Four Landing Gear Shipset Fixed price as Security Deposit that shall be retained by Air

India till the warranty of all shipsets are completed. Security Deposit can be deposited in the

form of Bank Grantee (BG).

BG must have endorsement of the Indian Counterpart of the bank issuing the BG. Cost of

BG has to be borne by successful bidder(s).

8. Penalty

8.1 In case of non adherence to delivery schedule, penalty will be levied for delayed delivery at

the rate 0.5% per week or part thereof of the total price of each advance exchange fee and

overhaul charges (as quoted in Price bid format for each gear) excluding taxes and delivery

charges) subject to a maximum of 10% of the value of the total price of each advance

exchange fee plus overhaul charges. This will be recovered from the amount due to the

selected bidder after due notification to the vendor in advance.

8.2 The tentative delivery schedule of the advance exchange is specified at Annexure-1. In the

eventuality of failure to meet the delivery schedule (exact date of requirement of advance

exchange gear will be notified 60 days in advance), Air India will have the right to cancel

the contract without any financial liability on its part for the work already performed. Air

India in such a case can also cancel the contract with forfeiture of the Security Deposit (SD)

amount, without any liability on its part.

9. Insurance

9.1 The transit insurance for the landing gear to and from Air India will be the responsibility of

selected bidder.

9.2 When the landing gear is in the custody of the repair agency, necessary insurance coverage

including liability for loss due to theft or fire or any natural causes including incident related

/ foreign object damage will be the responsibility of the selected bidder.

9.3 However the goods must be suitably packed as required and packaged for transportation to

Air India as per standard / IATA procedures and / or mandatory requirements. The

successful bidder is liable for damages resulting from inadequate packaging and packing.

10. Warranty

10.1 Bidders must quote for minimum warranty of 3000 landings or 36 months whichever occurs

earlier for the advance exchange gears.

10.2 Warranty from the date of installation of advance gear against poor workmanship/ defective

material/ failures except for FOD, accidents, act of nature related damages.

10.3 The warranty shall be comprehensive and unconditional, apply to all sub-assemblies,

components and will supersede any and all warranties offered by sub-contractors/ material

suppliers.

10.4 In the event of failure of advance gear/exchange overhaul gear received from selected repair


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agency during warranty period, replacement of such gear on Free of Cost basis will be the

responsibility of the selected bidder.

10.5 For gears failing during the warranty period, both ways freight, insurance and customs duty

applicable if any will be borne by the repair agency, for rectification of defects.

11. Documentation

11.1 All relevant documents required are to be submitted by the successful bidder at their own

cost.

11.2 All overhauled landing gears should be supplied to Air India with LLP, SB, AD compliance

lists, FAA/ EASA or equivalent certification and complete Dirty Finger Print of overhaul in

soft as well as hard copy.

11.3 For all removed landing gears sent for overhauling, inspection / tear-down report along with

proposed rectification action should be provided to Air India for evaluation.

11.4 Any abnormal findings will have to be reported to Air India duly substantiated by

photographs, documents as applicable.

11.5 The repair/ overhauling quote should indicate the material and labour charges separately.

The attached strip/ investigation report should also indicate the material and labour charges.

12. Integrity Pact

The Applicants/Bidders should execute an integrity pact with, as given in Annexure 10. The

signed Integrity pact document must be submitted with Technical Bid, otherwise the Bid

will be rejected.

Kindly note that Independent External Monitor (IEM) is Mr.Pratyush Sinha.. For any

clarification related to Integrity Pact, he may be contacted by Post / Email on following

address :-

Shri Pratyush Sinha

Ex. Central Vigilance Commissioner

Apartment no. 304, Tower 7

Commonwealth Games Village

New Delhi-110092

[email protected]

13. Inspection:

13.1 Inspection of bidders’ facilities at the time of evaluation of the Technical Bids: Air India Ltd. reserves the right to inspect at its cost the facility / facilities of the bidders in

order to assess their infrastructure and capability for carrying on the contract as indicated in

this tender.

13.2 Inspection of the facility of the selected bidder who has been awarded the contract:

Air India Ltd. further reserves the right to inspect the facility of the selected bidder, who has


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been awarded the contract.

13.3 Quality Inspection & Rejection after release of contract: Air India Ltd. also reserves the right to cancel the contract in case of complaints, if any, or

service deficiency.

14. Exit clause/ Termination of contract The Contract may be terminated under the following circumstances:

14.1 In the event of failure to meet the contractual obligations including that of delivery schedule,

workmanship etc, Air India will be at liberty to terminate the contract with the notice period

of 120 days.

14.2 If there is a change in Air India Ltd’s requirement, the Contract shall be terminated with 120

days advance notice.

14.3 In the event of deficiency in service of the Agency, Air India Ltd. reserves the right to

cancel the contract with 120 days notice and to claim damages from the selected bidder.

AIR INDIA LTD. also reserves the right to award the contract to another agency at the cost

and risk of the selected bidder. Either party reserves the right to terminate the contract after

giving 120 days written notice to the other party.

15. Rejection of Bids (Technical bid & Price bid)

The response to the Technical Bid & Price bid will be rejected forthwith without evaluation

of the bid on the following grounds:

15.1 If the Technical bid or the Price bid has been received after due date and time of closing of

the tender.

15.2 If only the Technical bid has been received and Price bid has not been received, and vice

versa.

15.3 If the Technical bid or the Price bid has been received by fax or email.

15.4 If the Technical bid or the Price bid has been received unsigned.

15.5 If the Price bid has been received in an open condition in the master envelope containing the

Technical bid or if both the Technical bid & Price bid are received in an open condition in a

single envelope.

15.6 If the Technical Bid has been received without EMD, or the EMD has been

submitted in a mode other than specified in the tender, or a valid proof of exemption from

submission of EMD has not been provided.

16. Evaluation Criteria:

16.1 Technical Bid Evaluation: The Technical Bids would be evaluated for their ‘Compliance to the Technical

Requirement’ of the Tender as indicated at Annexure 5. Air India Ltd. reserves the right at

its sole discretion to seek whatever information, documents etc. from the bidder, as it may

consider necessary for the purpose of evaluation of the bids.


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16.2 Price bid Evaluation: i. The Price bids of only those bidders who qualify and are short listed after evaluation of their

Technical Bids would be opened. The date and time of opening of the Price bids would be

intimated in advance to the bidders who have qualified in the Technical Bid evaluation, and

their authorized representatives only would be permitted to participate in the opening of the

Price bids.

ii. Price bids should be submitted strictly as per the format given at Annexure 7 only.

iii. Price bids will be evaluated in USD currency. In case, any bidder quotes in a currency other

than in USD, the IATA exchange as per Air India’s System on the date of opening of the

Price bids will be used for conversion from the quoted currency to USD for the purposes of

evaluation.

iv. Evaluation will be based on total minimum cost to the Company for advance exchange,

overhaul & logistic for 27 A320 family aircraft - quantity Fifteen of A319 / A320 aircraft

and quantity Twelve of A321aircraft.

v. In case a bidder does not accept standard payment terms of 60 days, the Price bid would be

loaded by financing cost @ 18 % per annum for the difference between 60 days and the

actual credit period offered by the bidder.

vi. Any conditional discounts offered will not be considered.

17. Price negotiation

Generally Air India Ltd. doesn’t carry price negotiations following evaluation of the Price

bids. Therefore, bidders are advised to submit their best quotes in response to this tender.

Air India Ltd. however, reserves the right to carry out negotiations in exceptional cases.

18.

19.

Arbitration

Any dispute arising between the parties in respect of the construction, interpretation,

application, meaning, scope, operation or effect of this document or the validity or breach

thereof, shall first be settled by mutual consultation. If the dispute remains unresolved after a

period of 90 days from the date when the mutual consultation has started, the matter shall be

referred for settlement to 'SCOPE FORUM OF CONCILIATION AND ARBITRATION',

Govt. of India, and the award made in pursuance thereof shall be binding on the parties

Jurisdiction Any dispute whatsoever shall be subject to the jurisdiction of the High Courts of Mumbai,

India only.

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Delivery Schedule Annexure 1

The delivery schedule given below is tentative Landing Gear Replacement Schedule

Note: Exact a/c reg no., date & place of replacement of each ship set will be intimated in advance.

S/N A/C

Type

MSN Regist Replacement

Schedule

Cycle of Advance

Exchange Landing

Gear Shipset

Landing Gear Shipset

required at AI Facility

1 A321 03573 VT-PPJ Jun 18 1 Mumbai

2 A321 03619 VT-PPK Jul 18 2 Mumbai

3 A321 03752 VT-PPL Sep 18 1 Mumbai

4 A321 03792 VT-PPM Oct 18 2 Mumbai

5 A321 03955 VT-PPN Dec 18 1 Mumbai

6 A321 04002 VT-PPO Jan 19 2 Mumbai

7 A321 04009 VT-PPQ Mar 19 1 Mumbai

8 A321 04078 VT-PPT Apr 19 2 Mumbai

9 A321 04096 VT-PPU Jun 19 1 Mumbai

10 A321 04138 VT-PPV Jul 19 2 Mumbai

11 A321 04155 VT-PPW Sep 19 1 Mumbai

12 A321 04280 VT-PPX Oct 19 2 Mumbai

S/N A/C

Type

MSN Regist Replacement

Schedule

Cycle of Advance

Exchange Landing

Gear Shipset

Landing Gear Shipset

required at AI Facility

1 A319 04020 VT-SCS Jul 18 1 Kolkata

2 A319 03551 VT-SCL Aug18 2 Kolkata

3 A319 03620 VT-SCM Oct 18 1 Kolkata

4 A319 04029 VT-SCT Nov18 2 Kolkata

5 A319 03970 VT-SCR Jan 19 1 Kolkata

6 A319 03822 VT-SCO Feb 19 2 Kolkata

7 A319 04052 VT-SCU Apr 19 1 Kolkata

8 A319 03918 VT-SCQ May 19 2 Kolkata

9 A319 04121 VT-SCW Jul 19 1 Kolkata

10 A319 04089 VT-SCV Aug 19 2 Kolkata

11 A319 04164 VT-SCX Oct 19 1 Kolkata

12 A320 04201 VT-EDC Nov-19 2 Delhi

13 A320 04212 VT-EDD Jan-20 1 Delhi

14 A320 04236 VT-EDE Feb-20 2 Delhi

15 A320 04237 VT-EDF Apr-20 1 Delhi


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ANNEXURE - 2

A. TECHNICAL REQUIREMENT FOR

DELIVERY CONFIGURATION

NLG

Nose Landing Gear

Description INCLUDED

NOT

INCLUDED

. Nose Landing Gear Leg X

.. Leg Structure X

… Shock Absorber X

… Swivel Bearings X

… Anti Shimmy Valve X

.. Swivel Selector Valve X

.. Leg Fittings X

.. 1M & 2M Upper Harnesses X

.. Intermediate & Lower Harnesses A/C config.

. Wheel Nuts & Retaining Rings X

. Sensor boxes X

. Forestay Assembly X

.. Forestay X

.. Swivel Bearings X

.. Lock Link X

.. Proximity Switches X

.. Lock Springs X

.. Unlocking Actuator X

. NLG Actuating Cylinder 2527GM X

. Tow Fitting 2701GM

. Axle Sleeves 2825GM, 2826GM X

NLG Wheel & Tire Assy 2659GM, 2660GM X

TPIS Transmission Unit 4GVA, 5GVA X

Steering Control Unit 6GC X

Lights 7LR, 8LR,

3LC1, 3LC2 X


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MLG

Main Landing Gear INCLUDED

NOT

Description INCLUDED

. MLG Leg & Dressing X

.. MLG Leg X

... Damper X

... Proximity Switches X

... Axle Harnesses (1M & 2M) X

.. MLG leg Harnesses (1M & 2M) X

. Side Stay Complete X

.. Side Stay Basic X

.. Lock Spring X

.. Lock Stay Actuator X

.. Lock Stay X

. MLG Retraction Actuator 2503GM, 2604GM X

Aft & Forward Pintle Pin with

nut (Airbus parts) X

BTMU 2GW, 3GW X

Brake Manifold 2612GM, 2613GM X

Wheel & Tire Assemblies 2649 GM,2650GM,

X

2651GM, 2652GM

MLG Brakes 2641GM, 2642GM,

2643GM, 2644GM X

MLG Axle Sleeves 2631GM, 2632GM,

2633GM, 2634GM X

MW Anti-skid Tachometers 19GG, 20GG, 21GG,

22GG X


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A319 AIRCRAFT INDICATIVE LIST OF LANDING GEAR ITEMS

# PART NUMBER PART DESCRIPTION LEG ASSY

1 D67906 UPPER SUPPORT NLG

2 D23613000 NLG RETRACTION ACTUATOR NLG

3 D23612000 LOCK LINK ASSY NLG

4 D23607000-5 LEG DRESSING NLG

5 D23590000-10 LEG STRUCTURE NLG

6 D23076000-3 UNLOCKING ACTUATOR NLG

7 C24998000 SWIVEL SELECT VALVE NLG

8 D23757550-6 LEG ASSY-NLG NLG

9 D67583 BARREL NLG

10 D66677 RACK NLG

11 D59954 PIN NLG

12 D65520 TURNING TUBE NLG

13 D65234 TORQUE LINKS NLG

14 D65566-1 PIN NLG

15 D64433-1 CENTRE PIN NLG

16 D65588-1

HINGE PIN

(BARREL/STRUCTURE) NLG

17 D65588-1

HINGE PIN

(BARREL/STRUCTURE) NLG

18 D64125 PIN NLG

19 D65589-1

PIN RETRACTION

ACTUATOR/LOCK LINK BARREL NLG

20 D65599-1 PIN (FORE STAY/BARREL) NLG

21 D23592020 ABSORBER-SHOCK NLG

22 D65519 CYLINDER NLG

23 D66679 SLIDING TUBE NLG

24 D66680 WHEEL AXLE NLG

25 D65234 TORQUE LINKS NLG

26 D65566-1 PIN NLG

27 D23596000-2 FORE STAY NLG NLG

28 D65237 FORE STAY UPPER PANEL NLG

29 D67802 FORESTAY LOWER LINK NLG


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30 D59638 UNIVERSAL JOINT NLG

31 D65773 PIN (LOWER LINK/UJOINT) NLG

32 D65887 PIN(UPPER PANEL/U JOINT) NLG

33 D67928 LOCK LINK LOWER PIN NLG

34 D67932 CROSS PIN NLG

35 D65616 PIN(UPPER PANEL/STRUCTURE) NLG

36 D65616 PIN(UPPER PANEL/STRUCTURE) NLG

37 D59636-1 LOCK LINK UPPER ARM NLG

38 D59635 LOCK LINK LOWER ARM NLG

39 D60054 LOCK LINK CENTRAL PIN NLG

40 D60739

PIN(LOCK ACTUATOR/UPPER

LINK) NLG

41 D23611000 LOCK-SPRING NLG

42 D59800-004 DOWN LOCK SPRING NLG

43 D23611000 LOCK-SPRING NLG

44 D59800-004 DOWN LOCK SPRING NLG

45 201582001-030 LEG AND DRESSINGS-MLG, LH MLG LH

46 201540300 MAIN FITTING(LH) MLG LH

47 201540303

MLG TORQUE LINK ASSEMBLY

UPPER MLG LH

48 201540302


LOWER MLG LH

49 201042106

AFT PINTLE SPHERICAL

BEARING MLG LH

50 201173600 PINTLE PIN FORWARD MLG LH

51 201540616

FORWARD PINTLE PIN STUB

BOLT MLG LH

52 201540616


BOLT MLG LH

53 201383608

PIN (RETAINING LOWER

BEARING) MLG LH

54 201383608


BEARING) MLG LH


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55 201383608


BEARING) MLG LH

56 201056669 HOUSING MLG LH

57 201383648 UPLOCK PIN MLG LH

58 201383606 TORQUE LINK APEX PIN MLG LH

59 201587612 TORQUE LINK APEX PIN NUT MLG LH

60 201160603 UPPER TORQUE LINK PIN MLG LH

61 201160602 LOWER TORQUE LINK PIN MLG LH

62 201056885 PIN MLG LH

63 201056909 LOCK STAY CARDAN PIN MLG LH

64 201058306 LOCK STAY CARDAN MLG LH

65 201371268

MLG SHOCK ABSORBER

ASSEMBLY MLG LH

66 201371304 SLIDING TUBE MLG LH

67 201371615 UPPER DIAPHRAGM TUBE MLG LH

68 201160317 PIN MLG LH

69 D52041-1 NUT MLG LH

70 D52041-1 NUT MLG LH

71 201419001-020 DAMPER-TORQUELINK MLG MLG LH

72 201160693 PISTON MLG LH

73 201166013-025 STAY-SIDE LH MLG LH

74 201163004-015 STAY-SIDE MLG LH

75 201163300 UPPER SIDE STAY MLG LH

76 201163301 LOWER SIDE STAY MLG LH

77 201163620 UPPER CARDAN MLG LH

78 201163307 LOWER CARDAN MLG LH

79 201163609 SIDE STAY PIVOT PIN MLG LH

80 201163618 SIDE STAY UPPER CARDAN PIN MLG LH

81 201163619 SIDE STAY LOWER CARDAN PIN MLG LH


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82 201057627 LOCK LINK LOWER PIN MLG LH

83 201163944 UPPER CARDAN NUT MLG LH

84 201163945 LOWER CARDAN NUT MLG LH

85 201661613 CUFF MLG LH

86 201661605 PIN(L0CK LINK) MLG LH

87 201661606 LOWER PIN(SPRING) MLG LH

88 201661607 UPPER PIN (SPRINGS) MLG LH

89 201661307 LINK(SPRING) MLG LH

90 201661609 LINK SIDE STAY PIN MLG LH



93 201661306 BANANA LINK(SPRING) MLG LH

94 201661306 BANANA LINK(SPRING) MLG LH

95 201059001 LOCKING SPRING ASSY MLG LH

96 201059602 SPRING MLG LH

97 201059001 LOCKING SPRING ASSY MLG LH

98 201059602 SPRING MLG LH

99 201058003 STAY-LOCK MLG LH

100 201058310 UPPER LOCK LINK MLG LH

101 201058305 LOWER LOCK LINK MLG LH

102 201058608 LOCK LINK CENTER PIN MLG LH

103 201058611 LOCK LINK UPPER PIN MLG LH

104 114095004-010

MLG LOCK STAY ACTUATOR

CYLINDER MLG LH

105 114095305 CYLINDER MLG LH

106 114095667 PISTON ROD MLG LH

107 114095602 EYE END MLG LH

108 201590002-020 RETRACTION ACTUATOR MLG LH

109 201590901

RETRACTION ACTUATOR( REAR

FITTING SIDE) MLG LH

110 201590900

RETRACTION ACTUATOR( MAIN

FITTING SIDE) MLG LH

111 201590906

CYLINDER RETRACTION

ACTUATOR MLG LH

112 201590909 PISTONRETRACTION ACTUATOR MLG LH


17

113 201590910 NUT RETRACTION ACTUATOR MLG LH

114 201590913 GLAND RETRACTION ACTUATOR MLG LH

115 201590908

ROD

PISTONRETRACTIONACTUATOR MLG LH

116 C24837102-2 BRAKE MANIFOLD MLG LH

117 CZ9284E TRANSDUCER MLG LH

118 CZ9284E TRANSDUCER MLG LH

119 C20225410-1 BRAKE ASSEMBLY MLG LH

120 C20225410-1 BRAKE ASSEMBLY MLG LH

121 35-1H5-1002 BTMU MLG LH

122 C20105000-2 TECHOMETER MLG LH

123 C20105000-2 TECHOMETER MLG LH

124 AE1502U02 MOTOR ASSY-BRAKE FAN MLG LH

125 AE1502U02 MOTOR ASSY-BRAKE FAN MLG LH

126 D3214022000200 NUT ASSY MLG LH

127 SLN41193 REAR PINTLE PIN NUT MLG LH

128 D3215303000600 PINTLE PIN REAR MLG LH

129 201582002-030 LEG AND DRESSINGS-MLG MLG RH

130 201540301 MAIN FITTING(RH) MLG RH

131 201540303


UPPER MLG RH

132 201540302


LOWER MLG RH

133 201042106

AFT PINTLE SPHERICAL

BEARING MLG RH

134 201173600 PINTLE PIN FORWARD MLG RH

135 201540616


BOLT MLG RH

136 201540616


BOLT MLG RH

137 201383608


BEARING) MLG RH


18

138 201383608


BEARING) MLG RH

139 201383608


BEARING) MLG RH

140 201056669 HOUSING MLG RH

141 201383648 UPLOCK PIN MLG RH

142 201383606 TORQUE LINK APEX PIN MLG RH

143 201587612 TORQUE LINK APEX PIN NUT MLG RH

144 201160603 UPPER TORQUE LINK PIN MLG RH

145 201160602 LOWER TORQUE LINK PIN MLG RH

146 201056885 PIN MLG RH

147 201056909 LOCK STAY CARDAN PIN MLG RH

148 201058306 LOCK STAY CARDAN MLG RH

149 201371268

MLG SHOCK ABSORBER

ASSEMBLY MLG RH

150 201371304 SLIDING TUBE MLG RH

151 201371615 UPPER DIAPHRAGM TUBE MLG RH

152 201160317 PIN MLG RH

153 D52041-1 NUT MLG RH

154 D52041-1 NUT MLG RH

155 201419001-020 DAMPER-TORQUELINK MLG MLG RH

156 201160693 PISTON MLG RH

157 201166013-025 STAY-SIDE LH MLG RH

158 201163004-015 STAY-SIDE MLG RH

159 201163300 UPPER SIDE STAY MLG RH

160 201163301 LOWER SIDE STAY MLG RH

161 201163620 UPPER CARDAN MLG RH

162 201163307 LOWER CARDAN MLG RH

163 201163609 SIDE STAY PIVOT PIN MLG RH

164 201163618 SIDE STAY UPPER CARDAN PIN MLG RH


19

165 201163619 SIDE STAY LOWER CARDAN PIN MLG RH

166 201057627 LOCK LINK LOWER PIN MLG RH

167 201163944 UPPER CARDAN NUT MLG RH

168 201163945 LOWER CARDAN NUT MLG RH

169 201661613 CUFF MLG RH

170 201661605 PIN(L0CK LINK) MLG RH

171 201661606 LOWER PIN(SPRING) MLG RH

172 201661607 UPPER PIN (SPRINGS) MLG RH

173 201661307 LINK(SPRING) MLG RH

174 201661609 LINK SIDE STAY PIN MLG RH



177 201661306 BANANA LINK(SPRING) MLG RH

178 201661306 BANANA LINK(SPRING) MLG RH

179 201059001 LOCKING SPRING ASSY MLG RH

180 201059602 SPRING MLG RH

181 201059001 LOCKING SPRING ASSY MLG RH

182 201059602 SPRING MLG RH

183 201058003 STAY-LOCK MLG RH

184 201058310 UPPER LOCK LINK MLG RH

185 201058305 LOWER LOCK LINK MLG RH

186 201058608 LOCK LINK CENTER PIN MLG RH

187 201058611 LOCK LINK UPPER PIN MLG RH

188 114095004

MLG LOCK STAY ACTUATOR

CYLINDER MLG RH

189 114095305 CYLINDER MLG RH

190 114095667 PISTON ROD MLG RH

191 114095602 EYE END MLG RH

192 201590002-020 RETRACTION ACTUATOR MLG RH

193 201590901

RETRACTION ACTUATOR( REAR

FITTING SIDE) MLG RH

194 201590900

RETRACTION ACTUATOR( MAIN

FITTING SIDE) MLG RH

195 201590906

CYLINDER RETRACTION

ACTUATOR MLG RH


20

196 201590909 PISTONRETRACTION ACTUATOR MLG RH

197 201590910 NUT RETRACTION ACTUATOR MLG RH

198 201590913 GLAND RETRACTION ACTUATOR MLG RH

199 201590908

ROD

PISTONRETRACTIONACTUATOR MLG RH

200 C24837102-2 BRAKE MANIFOLD MLG RH

201 CZ9284E TRANSDUCER MLG RH

202 CZ9284E TRANSDUCER MLG RH

203 C20225510 BRAKE ASSEMBLY MLG RH

204 C20225510 BRAKE ASSEMBLY MLG RH

205 35-1H5-1002 BTMU MLG RH

206 C20105000-2 TECHOMETER MLG RH

207 C20105000-2 TECHOMETER MLG RH

208 AE1502U02 MOTOR ASSY-BRAKE FAN MLG RH

209 AE1502U02 MOTOR ASSY-BRAKE FAN MLG RH

210 D3214022000200 NUT ASSY MLG RH

211 SLN41193 REAR PINTLE PIN NUT MLG RH

212 D3215303000600 PINTLE PIN REAR MLG RH

A321 AIRCRAFT– INDICATIVE LIST OF LANDING GEAR ITEMS

S/N Part No. Item Description Gear

1 201661306 BANANA LINK SPRINGS L

2 201661306 BANANA LINK SPRINGS L

3 201587611 CROSS BOLT(PINTLE PIN) L

4 201587610 CROSS BOLT(PINTLE PIN) L

5 201661305 CUFF L

6 201661612 PIN, CUFF L

7 201661612 PIN, CUFF L

8 114095305 CYLINDER L


21

9 114095004-010 MLG LOCK STAY ACTUATOR

CYLINDER L

10 201590002-020 MLG CYLINDER ACTUATOR ,

RETRACTION L

11 201590906 CYLINDER- ( RETRACTION

ACTUATOR) L

12 201419001-020 DAMPER TORQUE LINK L

13 114095602 EYE END L

14 201590913 GLAND RETRACTION ACTUATOR L

15 201056669 HOUSING L

16 201531001 LOCK LINK ASSEMBLY L

17 201058608 LOCK LINK CENTER PIN L

18 201057627 LOCK LINK LOWER PIN L

19 201058611 LOCK LINK UPPER PIN L

20 201661609 PIN SIDE STAY LINK L

21 201661307 LINK L

22 201056909 LOCK STAY CARDAN PIN L

23 201059001 LOCKING SPRING ASSY L

24 201059001 LOCKING SPRING ASSY L

25 201058306 LOCK STAY CARDAN (complete) L

26 201661301 LOWER ARM L

27 201403300 LOWER ARM L

28 201525302 LOWER CARDAN L

29 201661606 LOWER PIN [SPRING] L

30 201587304 LOWER TORQUE LINK L

31 201522351 MAIN FITTING L

32 201585003-020 MLG LEG ASSEMBLY LH L

33 201661610 NUT L

34 201587612 NUT (TORQUE LINK APEX PIN) L

35 201383658 NUT L

36 201383658 NUT L

37 201661611 NUT(LOWER CARDAN) L

38 201590910 NUT RETRACTION ACTUATOR L

39 201056885 PIN L

40 201383608 PIN (RETAINING LOWER

BEARING) L


BEARING) L


BEARING) L


22

43 201383604 PIN (TORQUE LINK/MAIN

FITTING) L

44 201383605 PIN (TORQUE LINK/SLIDING

TUBE) L

45 201042415 AFT PINTLE BEARING L

46 201590900 PIN L

47 201590901 PIN L

48 201661601 PIN L

49 201661603 PIN L

50 201525618 PIN L

51 201160317 PIN L

52 201661605 PIN [LOCK LINK/BANANA LINK] L

53 201383648 UPLOCK PIN L

54 201160693 PISTON L

55 201590909 PISTON HEAD RETRACTION

ACTUATOR L

56 114095667 PISTON ROD L

57 201522600 PINTLE PIN FORWARD L

58 201590908 ROD PISTON RETACTION

ACTUATOR L

59 201522266 MLG SHOCK ABSORBER L

60 201522353 SLIDING ROD L

61 201059602 SPRING L

62 201059602 SPRING L

63 201660001-025 SIDE STAY ASSEMBLY LH L

64 201383606 TORQUE LINK APEX PIN L

65 201661300 UPPER ARM L

66 201531300 UPPER ARM L

67 201525607 UPPER CARDAN L

68 201522651 UPPER DIAPHRAGM TUBE L

69 201661607 UPPER PIN [SPRING] L

70 201587303 UPPER TORQUE LINK L

71 D67583 BARREL N

72 D64433-1 CENTRE PIN N

73 D67932 CROSS PIN N

74 22715-000-02 CYLINDER- ACTUATING NLG N

75 D65519 CYLINDER N

76 D23613000 NLG ACTUATING CYLINDER N

77 D59800-0004 DOWNLOCK SPRING N


23

78 D59800-0004 DOWNLOCK SPRING N

79 D23596000-3 FORESTAY ASSY N

80 D67802 FORESTAY LOWER LINK N

81 D65237 FORESTAY UPPER PANEL N

82 D65588-1 HINGE PIN BARREL/STRUCTURE N

83 D65588-1 HINGE PIN BARREL/STRUCTURE N

84 D60054 LOCK LINK CENTRAL PIN N

85 D59635 LOCK LINK LOWER ARM N

86 D67928 LOCK LINK LOWER PIN N

87 D66680 WHEEL AXLE N

88 D59636-1 LOCK LINK UPPER ARM N

89 NA28008-11 NLG LEG ASSEMBLY N

90 D59954 STEERING PIN N

91 D64125 PIN N

92 D65599-1 PIN FORE STAY/BARREL N

93 D60739 PIN(LOCK ACTUATOR/UPPER

LINK) N

94 D65773 PIN(LOWER LINK/U JOINT) N

95 D65566-1 PIN N

96 D65566-1 TORQUE LINK PIN N

97 D65589-1 PIN RETRACTION

ACTUATOR/LOCK LINK BARREL N

98 D65616 PIN(UPPER PANEL/STRUCTURE) N

99 D65616 PIN(UPPER PANEL/STRUCTURE) N

100 D65887 PIN(UPPER PANEL/U/JOINT) N

101 D66677 RACK N

102 D23592020 NLG SHOCK ABSORBER

ASSEMBLY N

103 D66679 SLIDING TUBE N

104 D65234 NLG TORQUE LINK ASSEMBLY N

105 D65234 TORQUE LINKS N

106 D65520 TURNING TUBE N

107 D23611000 UNLOCKING SPRING N

108 D23611000 UNLOCKING SPRING N

109 D59638 UNIVERSAL JOINT N

110 201661306 BANANA LINK SPRINGS R

111 201661306 BANANA LINK SPRINGS R

112 201587611 CROSS BOLT(PINTLE PIN) R


24

113 201587610 CROSS BOLT(PINTLE PIN) R

114 201661305 CUFF R

115 201661612 PIN, CUFF R

116 201661612 PIN, CUFF R

117 114095004 MLG LOCK STAY ACTUATOR

CYLINDER R

118 201590002-020 MLG CYLINDER ACTUATOR ,

RETRACTION R

119 201590906 CYLINDER RETRACTION

ACTUATOR R

120 201419001-020 DAMPER TORQUE LINK R

121 201590913 GLAND RETRACTION ACTUATOR R

122 201056669 HOUSING R

123 201531001 LOCK LINK ASSEMBLY R

124 201058608 LOCK LINK CENTER PIN R

125 201058611 LOCK LINK UPPER PIN R

126 201661609 PIN,SIDE STAY LINK R

127 201042415 AFT PINTLE BEARING R

128 201661307 LINK R

129 201056909 LOCK STAY CARDAN PIN R

130 201059001 LOCKING SPRING ASSY R

131 201059001 LOCKING SPRING ASSY R

132 201058306 LOCK STAY CARDAN R

133 201661301 LOWER ARM R

134 201403300 LOWER ARM R

135 201525302 LOWER CARDAN R

136 201661606 LOWER PIN [SPRING] R

137 201587304 LOWER TORQUE LINK R

138 201522352 MAIN FITTING RH R

139 201585004-020 MLG LEG ASSEMBLY RH R

140 201661610 NUT R

141 201587612 NUT (TORQUE LINK APEX PIN) R

142 201383658 NUT R

143 201383658 NUT R

144 201661611 NUT R

145 201590910 NUT RETRACTION ACTUATOR R

146 201056885 PIN R


BEARING) R


25


BEARING) R


BEARING) R

150 201383604 PIN (TORQUE LINK/MAIN

FITTING) R

151 201383605 PIN (TORQUE LINK/SLIDING

TUBE) R

152 201590901 PIN R

153 201590900 PIN R

154 201525618 PIN R

155 201661601 PIN R

156 201661603 PIN R

157 201057627 PIN (LOCK LINK LOWER PIN) R

158 201160317 PIN R

159 201661605 PIN [LOCK LINK/BANANA LINK] R

160 201383648 UPLOCK PIN R

161 201160693 PISTON R

162 201590909 PISTON HEAD RETRACTION

ACTUATOR R

163 201522600 PINTLE PIN FORWARD R

164 201590908 ROD PISTON RETACTION

ACTUATOR R

165 201522266 MLG SHOCK ABSORBER R

166 201522353 SLIDING ROD R

167 201059602 SPRING R

168 201059602 SPRING R

169 201660002-025 SIDE-STAY ASSY , MLG RH R

170 201383606 TORQUE LINK APEX PIN R

171 201661300 UPPER ARM R

172 201531300 UPPER ARM R

173 201525607 UPPER CARDAN R

174 201522651 UPPER DIAPHRAGM TUBE R

175 201661607 UPPER PIN [SPRING] R

176 201587303 UPPER TORQUE LINK R

177 114095667 PISTON ROD R

178 114095602 EYE END R

179 114095305 CYLINDER R


26

B. OVERHAUL OF REMOVED LANDING GEAR

Overhaul Landing Gear and Actuator Shipsets shall comply with the Airbus Appendix 7- A320 Family

Landing Gear Overhaul Procedures Document.

One ship set means one NLG, one LH MLG and one RH MLG together with Retraction Actuators.

The work scope for the Fixed Price shall cover Material and labour charges as specified below:

1. Following tasks are to be performed on the Landing Gears (MLG-LH; MLG-RH, NLG & and their

associated Retraction Actuators) removed from Aircraft in accordance with applicable CMM (refer

Airbus MPD Rev 44 Appendix 7):

i. Overhaul of Main Landing Gear

MRBR TASK

NUMBER

DESCRIPTION

32.11.00/14 Special Detailed Inspection of Main Landing Gear (Off

Aircraft) Including:

Special Detailed Inspection of MLG Shock Absorber

Internal Components.

Special Detailed Inspection of MLG Fwd Pintle Bearing and

Pin.

Special Detailed Inspection of MLG Aft Pintle Bearing and

Pin.

Special Detailed Inspection of MLG Side Stay Bushes,

Gear Attachment Lug Bushes and Pins.

Special Detailed Inspection of MLG Lock Stay Bushes,

Attachment Lug Bushes and Pins.

Special Detailed Inspection of MLG Lock Stay Actuator

Bushes, Attachment Lug Bushes and Pins.

Special Detailed Inspection of MLG Retraction Actuator

Bushes and Bearings, Gear Attachment Lug Bushes and

Pins.

Special Detailed Inspection of MLG Slave Link Bushes and

Bearings, Attachment Lug Bushes and Pins.

Special Detailed Inspection of MLG Shock Absorber Upper

and Lower Bearings.

Special Detailed Inspection of MLG Torque Link Bushes,


321105-03-1 Special Detailed Inspection of Main Landing

Gear (Off Aircraft) Comprising:

Upper and Lower Side Stay

Upper and Lower Lock Links

Lack Stay Cardan


27

Cuff

Triangulation Link

Banana Link

Forward Pintle Pin

Pintle Pin Lock Bolts/Stub Bolts

Upper Diaphragm Cross Pin

Upper Pin (Springs)

Cuff Pins

Lock Link/Banana Link Pin

MRBR TASK

NUMBER

DESCRIPTION

Lower Banana Link Pin

Triangulation Link Pin

Lock Link Lower Pin

Lock Link Centre Pin

Lock Link Upper Pin

Lock Stay Cardan Pin

Side Stay Upper and Lower Cardan Pin

Side Stay Pivot Pin

Aft Pintle Spherical Bearing.


Gear, Upper and Lower Torque Links (Off

Aircraft) Comprising:

Upper Torque Link

Lower Torque Link

Torque Link Upper Pin

Torque Link Lower Pin

Apex Pin

Apex Pin Nut.


Gear, Side Stay Cardans (Off Aircraft)

Comprising:

Upper Cardan

Lower Cardan

Upper Cardan Nut

Lower Cardan Nut.


Gear, Main Fitting (Off Aircraft) Comprising:

Upper Diaphragm Tube

Sliding Tube

Lower Bearing Housing (Twin Wheel).


Gear, Rear Pintle Pin and Nut (Off Aircraft).


28

ii. Overhaul of Main Landing Gear Retraction Actuators and Attachment Pins

MRBR TASK

NUMBER

DESCRIPTION


Gear, Retraction Actuator (Off Aircraft)

Comprising:

Piston Rod

Piston Head

MRBR TASK

NUMBER

DESCRIPTION

Nut

Cylinder

Gland.


Gear, Retraction Actuator Pins (Off Aircraft)

Comprising:

Retraction Actuator Pin (Main Fitting)

Retraction Actuator Pin (Rear Spar).

iii. Overhaul of Nose Landing Gear

MRBR TASK

NUNBER

DESCRIPTION

32.21.00/05 Special Detailed Inspection of the Nose Landing Gear

(Off Aircraft). Including:

Special Detailed Inspection of NLG Shock Absorber Upper

and Lower Bearings.

Special Detailed Inspection of NLG Down lock Actuator


Special Detailed Inspection of NLG Actuating Cylinder

Bearings, Gear Attachment Lug Bushes and Pins.

Special Detailed Inspection of NLG Lock Link Bushes and


Special Detailed Inspection of NLG Shock Absorber Internal

Components.

Special Detailed Inspection of NLG Torque Link Bushes,


Special Detailed Inspection of NLG Forestay Bushes,


29

Bearings, Gear Attachment Lug Bushes and Pins.

Special Detailed Inspection of NLG Trunion Bushes and

Pins.

32.50.00/02 Special Detailed Inspection of Nose Wheel Steering

Actuator Rack and Pinion Mechanism (Off Aircraft).

322105-03-1 Special Detailed Inspection of Nose Landing Gear

(Off Aircraft) Comprising:

Barrel

Sliding Tube

Turning Tube

Axles

Forestay Upper Panel

Lower Link

Universal Joint

Lock Link Upper Link

MRBR TASK

NUMBER

DESCRIPTION

322110-03-1 Special Detailed Inspection of Nose Landing Gear,

Torque Links (Off Aircraft) Comprising:

Upper Torque Link

Lower Torque Link

Torque Link Pins

Torque Link Apex Pin And Nut.

Lock Link Lower Link

Upper Barrel Hinge Pins

Forestay Barrel Pin

Retaining Nut Shock Assy.

Upper Panel To Structure Pins

Upper Panel To Universal Joint Pin

Lock Link Center Pin

Lower Lock Link Pin

Lower Lock Link To Universal Joint Pin

Cross Pin

Actuating Cylinder To Lock Link Barrel Pin

Cylinder.

iv. Overhaul of Nose Landing Gear Actuating Cylinder and Attachment pin

MRBR TASK

NUMBER

DESCRIPTION

322152-01-1 Special Detailed Inspection of Nose Landing

Gear, Actuating Cylinder (Off Aircraft)


30

Comprising:

Piston Rod

Piston Rod Retaining Ring

Gland Retaining Ring

Piston Nut

Piston Head.

322158-01-1

Special Detailed Inspection of Nose Landing

Gear Pin, Actuating Cylinder to Aircraft

Structure (Off Aircraft).

2. A list of SBs which are required to be complied during overhaul are enclosed in Annexure 4 .

3. Ensure that these are at least complied with, if not already done. Check all other applicable ADs,

AOTs and mandatory SBs falling due at the time of Landing Gear overhaul covering the period of

next overhaul are also to be complied with. A complete serialised modification list

(AD/SB/VSB/AOT etc) is to be provided with overhauled landing gear.

4. The List of of ‘Landing Gear Identified Parts’ consist of overhauled items and inspection

items(LRUs-Not Subject To Overhaul). Check and ensure that Life Limited Parts for compliance

with the Airbus A318/A319/A320/A321 ALS. Refer to Airbus A318/A319/A320/A321 ALS Part 1

and ALS Part 4.

5. The overhauled Landing Gears must be delivered with traceable documentation including

ICR(inspection condition report) for all overhauled parts as well as identified in the Airbus

A318/A319/A320/A321 ALS Part 1 and Part 4.

6. Traceable documentation of Part number and Serial Number (if exist) of Inspected/Tested LRUs

(Not Subject To Overhaul) must be provided to the Air India.

7. Traceable documentation must be provided to the Air India Limited for all Repairs/Replacement

done on the Landing Gear.

8. Scrap parts and materials, which will no longer be used, are to be permanently disposed of. The parts

should be mutilated so that they cannot be re-used for their original intended use. The mutilation

should be sufficient to make sure that parts cannot be repaired or camouflaged to give the

appearance of acceptable parts.

9. Completed Landing Gear Overhaul Reporting Forms should be sent directly to Air India

10. Complete documentations including EASA Authorised Release Certificates and certified copies of

all the DFPs with respect to each of the MLGs and NLGs are to be handed over to Air India Limited.


31

Following minimum requirements are given as a guideline. However, applicable CMMs must be referred

and followed for further details.

Disassembly :

a) Disassemble the Landing Gear into its major sub-assemblies. Refer to DISASSEMBLY section of

the applicable CMM.

b) Remove all bushes and interference fit grease nipples from subassemblies. Refer to

DISASSEMBLY and REPAIR sections of the applicable CMM.

NOTE: It is recommended that removed bushes and interference fit grease nipples are discarded.

c) Remove electrical harnesses.

d) Remove hydraulic hoses and pipe assemblies.

Cleaning :

a) Clean all parts. Refer to CLEANING section of the applicable CMM.

b) Remove protective treatments as detailed in the applicable CMM, if required in the

appropriate inspection process specification.

Inspection :

a) Visually examine each part. Refer to CHECK section of the applicable CMM.

b) Perform dimensional checks where required. Refer to INITIAL MANUFACTURING LIMIT in

FITS AND CLEARANCES section of the applicable CMM.

NOTE: If the component dimensions are not within the tolerances stated in the initial manufacturing

limits in the FITS AND CLEARANCES, and an approved repair or concession has been

applied to the component, refer to that repair or concession for dimensions.

c) Springs are to be checked as detailed in CHECK section of the applicable CMM.

d) Perform NDT checks where required. Refer to tables in CHECK section of the applicable CMM.

Repairs :

a) Wherever required, repair the part. Refer to REPAIR section of the applicable CMM.

b) When beyond CMM limits, only approved repairs are to be applied.

c) If damage is beyond repair the part must be replaced. Dispose of damaged parts in accordance with

approved procedures.

d) Where applicable, and if not covered by the repair, strip and reapply protective treatments. Refer to

PROTECTIVE TREATMENTS in REPAIR section of the applicable CMM.

Restoration of Protective Treatments of Parts :

a) Where applied, strip and reapply protective treatments. Refer to the protective treatments in

REPAIR section of the applicable CMM.

b) Hard coatings (e.g. Chrome, HVOF applied coatings) do not need to be removed unless damage is

found during inspection.


32

c) Reapply protective treatments (paint, etc.) as applicable. Refer to protective treatments in REPAIR

section of the applicable CMM.

Re-assembly :

a) Install bushes and new interference fit grease nipples at the required build stage. Refer to

ASSEMBLY and REPAIR section of the applicable CMM.

b) Paint the part at the required build stage. Refer to REPAIR and ASSEMBLY sections of the

applicable CMM.

c) Assemble and test at the applicable stage of assembly. Refer to ASSEMBLY and TESTING AND

FAULT ISOLATION section of the applicable CMM.

d) Identify all applicable data on new nameplates where installed.

NOTE: The assembly part number must not change, unless specified by a Service

Bulletin.

e) Identify all of the serialised parts in the inspection record.

f) New standard parts prefixed with AN, MS, NAS and S shall be used during the assembly process.

g) All seals, ‘O’ rings, backing rings, split pins and single-use locking devices must be replaced with

new parts during the assembly process at overhaul.

h) Identification plates (where removed) and shims shall be replaced with new parts.

NOTE: When it is necessary to replace the identification nameplate, identify the

replacement nameplate with all the applicable data.

i) Assemble the Landing Gear Complete and test at the applicable stage of assembly. Refer to

ASSEMBLY and TESTING AND FAULT ISOLATION section of the applicable CMM.

j) Fully lubricate all greasing points on the Landing Gear Complete.

LRUs which are not Subject to Overhaul (As stated in Airbus MPD Rev 40 Appendix 7) :

a) Visually examine for indications of damage or corrosion. If necessary repair as detailed in REPAIR


b) Do the functional and leakage tests of LRUs. Refer to TESTING AND FAULT ISOLATION


Electrical Harnesses :

a) Clean the electrical harnesses. Refer to CLEANING section of the applicable CMM.

b) Check the drain holes in the conduit are clear and can drain.

c) Visually examine the external condition of the electrical harness conduit and connectors. Refer to

CHECK section of the applicable CMM.

d) Test the electrical harness. Refer to TESTING AND FAULT ISOLATION section of the applicable

CMM.

e) Where required, repair the electrical harness. Refer to REPAIR section of the applicable CMM.

Hydraulic Hoses and Pipe Assemblies :

a) Clean all Hydraulic Hoses (flexible) and Pipe Assemblies (rigid) internally and externally. Refer to

CLEANING section of the applicable CMM.


33

b) Visually examine the external condition of the Hydraulic Hoses and Pipe Assemblies. Refer to

CHECK section of the applicable CMM. Carefully examine the End Fittings for corrosion or

damage to threads.

c) If the results from the inspections are not satisfactory, replace the Hydraulic Hose or Pipe Assembly

with a new part.

d) Examine the Identification Labels, Fluid Type Labels, Flow Direction Labels and Protective Heat

Shrink Sleeves to make sure that they are not damaged or split and that the Labels can be read. If a

Label is damaged, split or cannot be read, install a new Label and Heat Shrink Sleeve.

e) Install Blanking Caps in the ends of the Hydraulic Hoses and Pipe Assemblies where they will not

be immediately installed.

The Fixed Price shall be for repair/restoration/overhaul/ of all items of landing gear shipset including On Condition items/components(hydraulic and electrical) such as Harnesses and Actuators etc covering

a) Materials

All materials upto unit part number price of USD 5000 (AT JAN 2018 ECONOMIC

CONDITION)and cost of Modification Kit used during the overhaul/ up gradation

All materials for compliance with all applicable mandatory inspections/ modifications

issued by FAA/EASA, France as on D2/N2/2018.

Cost of testing of on-condition equipment (hydraulics, electrical etc.)

b) Labour

All man-hours required for overhaul/upgradation of the gear.

All labour required for re-work beyond CMM limits including chromium/nickel plating.

Labour for test of on-condition equipment.-(hydraulic, electrical etc).

Exceptions allowed on the Fixed Price are repair or replacement of major items whose unit price

exceeds USD 5000 (AT JAN 2018 ECONOMIC CONDITION)such as the Sliding Rod, Cylinder,

Barrel etc.

1. Quotation for Exception allowed on Fixed Price must reflect the work performed. Quotation shall

contain or be accompanied by the following substantiating data or reasonable equivalent (to the

extent such data is applicable):

a) Overhaul agency/ Vendor/OEM shop report

b) Work scope (routine, non-routine and materials)

c) Overhaul agency/ Vendor/OEM concession/repair and overhaul

instructions/certification/replacement against scrap with FAA/EASA/BTB documents

d) Overhaul agency/ Vendor/OEM invoice and billing summary

2. Labour to comply with Air India standard modification, including compliance with all applicable

mandatory inspections/modifications issued by FAA/EASA, France as on 04/06/2018.

3. The Exception allowed on Fixed Price invoice should be accompanied by vendor/OEM invoice &

for all such items costing more than USD 5000 (AT JAN 2018 ECONOMIC CONDITION) and

used in the overhaul


34

4. If used part is installed during the overhaul of landing gear, please indicate the cost in terms of

percentage of new unit price and additionally provide FAA/EASA form with Back To Birth

certification where applicable at the time of seeking Air India’s approval.

5. All missing & damaged parts must be intimated to Air India with evidence like photograph,

technical report etc. within 10 days of receipt of landing gear at your facility for approval. Any

claims made after this time limit will not be entertained.

6. Quotation and Invoice-Time frame:

a) The quotation for Exceptions allowed on Fixed Price must be forwarded within 15 days of

induction for approval /inspection of our Technical representative, exception being where

the items are referred to OEM for obtaining concession for repairs.

b) The request for concession must be made to OEM as soon as possible but not later than 15

days from the date of detection of defects which are beyond CMM limits.

2. MISCELLANEOUS REQUIREMENT

a) All missing & damaged parts must be intimated to Air-India with evidence like photograph,

technical report, etc. within 10 days of receipt of Landing Gear at repair facility for approval.

Any claims made after this time limit will not be entertained.

b) Technical Representative from Air-India will be present during the process of

inspection/overhaul of removed landing gears.

c) Minimum required warranty is 3000 landings or 36 months whichever occurs earlier.

Warranty should be transferable / assignable.

d) The party agrees to comply with the INTEGRITY PACT which is attached herewith.

e) Installation of PMA parts on Advance Exchange Landing Gears is not acceptable.

3. MANDATORY REQUIREMENT

Director General of Civil Aviation, India (DGCA, India) approval is a MUST for carrying out

overhaul/repair of these landing gears. While all the bidders are encouraged to obtain this approval, the

selected bidder shall produce the approval within 3 weeks after being intimated of the selection. Failure

may lead to cancellation of the selection. DGCA approval should be current during the contract period.

OEM is not required to seek DGCA’s approval.

****************


35

ANNEXURE-3

LIST OF SB’S AND FAA AD ACCOMPLISHED

For A319 aircraft the list is :-

S/N AD/AOT/SB No. Subject

1

EASA AD 2013-0283R1/

FAA AD 2014-23-05/

AIRBUS SB 32-1408

MLG Retraction Actuator - Inspection/ Replacement.

2 EASA AD 2014-0141 Main Landing gear upper cardan-life limitation.

3 AIRBUS SB 32-1351 MLG - Introduce Enhanced standard sliding tube on original

standard main fitting.

4 AIRBUS SB 32-1357 Inspection of the Shock Absorber Lugs of the NLG.

5 AIRBUS SB 32-1392 Nose Gear - Define new nose gear LRU Breakdown.

For A321 aircraft the list is :-

S/N SB / AD No. SUBJECT

1

SB A320-32-1307 ; VSB

580-32-3160 ; MPD 323100-

08-1

NLG - SPECIAL DETAILED INSPECTION (

OVERHAUL ) OF THE NOSE LANDING GEAR

ACTUATING CYLINDER AND AIRFRAME

ATTACHMENT PIN AND SLEEVE ( OFF AIRCRAFT

) .

2 SB A320-32-1408 ; EASA

AD 2013 - 0283

MLG - CARRY OUT INSPECTION OF MLG

RETRACTION ACTUATOR RETAINING RING.

3 SB A320-32-1357 NLG - CARRY OUT INSPECTION OF THE SHOCK

ABSORBER LUGS OF THE NOSE LANDING GEAR.

4 SB A320-32-1392 NLG - DEFINE NEW NOSE GEAR LINE.

5 MESSIER DOWTY SB 201-

32-51

LANDING GEAR - MAIN LANDING GEAR -

RETRACTION ACTUATOR -

INTRODUCTION OF A NEW CYLINDER

SUBASSEMBLY


36

ANNEXURE 4

Date of induction of Airplanes in AI India fleet, TSN & CSN as on 28.2.2018

S/N A/C Type MSN Regist Date of

Manufacture

Airframe Cycles as on

23.2.18

1 A319 04020 VT-SCS 31-Aug-09 18663

2 A319 03551 VT-SCL 14-Oct-08 18571

3 A319 03620 VT-SCM 07-Nov-08 16662

4 A319 04029 VT-SCT 29-Sep-09 18271

5 A319 03970 VT-SCR 30-Jul-09 17987

6 A319 03822 VT-SCO 04-Mar-09 16313

7 A319 04052 VT-SCU 27-Oct-09 17451

8 A319 03918 VT-SCQ 28-May-09 16657

9 A319 04121 VT-SCW 21-Dec-09 17181

10 A319 04089 VT-SCV 27-Nov-09 13226

11 A319 04164 VT-SCX 27-Jan-10 15293

12 A320 04201 VT-EDC 24-02-2010 14523

13 A320 04212 VT-EDD 23-02-2010 14794

14 A320 04236 VT-EDE 29-03-2010 14982

15 A320 04237 VT-EDF 30-03-2010 15077

S/N A/C Type MSN Regist Date of

Manufacture

Airframe Cycles as on

23.2.18

1 A321 03573 VT-PPJ 01-Jul-08 15996

2 A321 03619 VT-PPK 22-Aug-08 14583

3 A321 03752 VT-PPL 13-Jan-09 15652

4 A321 03792 VT-PPM 11-Feb-09 15609

5 A321 03955 VT-PPN 30-Jun-09 14322

6 A321 04002 VT-PPO 28-Aug-09 14266

7 A321 04009 VT-PPQ 27-Aug-09 14381

8 A321 04078 VT-PPT 30-Oct-09 14120

9 A321 04096 VT-PPU 27-Nov-09 14290

10 A321 04138 VT-PPV 22-Dec-09 14353

11 A321 04155 VT-PPW 27-Jan-10 14107

12 A321 04280 VT-PPX 29-Apr-10 12270


37

Annexure -5

TECHNICAL BID

Technical Bid - Terms

Documents to be enclosed with Technical offer:-

1) FAA or EASA and DGCA India approval certificate for carrying out repair/overhaul of A320 Landing

Gears & associated components and shall comply with the Airbus Appendix 7- A320 Family Landing

Gear Overhaul Procedures Document .

2) Capability list as per FAA/EASA approved rating must be supplied.

3) List of airlines to whom the overhauled/repaired landing gears are supplied in last five years.

4) Copy of current DGCA (India) approval certificate, if available.

The prospective Applicants / Bidders are required to note that all the AIR INDIA LTD. specified

conditions under this Annexure, are met with and responded in order to qualify for the Technical

Evaluation. The Price bids of only those Applicants/Bidders would be opened who qualify the

Technical Evaluation.

Technical Bid Format

Sl.

No. Requirement Response

Response is

Mandatory

1 Name of the company, address, contact person & contact

details. Provide the details

Yes

2 List of customers to whom A320 family landing gear

overhaul services provided for last 5 years Provide the details Yes

3

Compliance with the delivery requirements for Landing

Gear Shipsets - shown in Annexure . Air India reserves

the right to install the landing gear or its constituent or

part/s on any aircraft/s of A320 family.

Yes/No

(If No - provide

alternate schedule)

Yes

4

Two advance exchange shipsets for A319/A320 bid or

Two advance exchange shipsets for A321 bid or Four

advance exchange shipsets for both bids - two for

A319/A320 & two for A321.

Provide the details Yes

5 AI requires first overhaul landing gear shipset with zero

time since overhaul. Confirm compliance Yes/No Yes

6 Advance Exchange gears be in RFI delivery condition as

detailed in Annexure 2 Part A Yes/No Yes

7

Confirm that the Landing Gear Shipsets will comply with

the Airbus document - Appendix 7- A320 Family

Landing Gear Overhaul Procedures Document. Confirm

compliance of Technical Requirement Annexure 2 and

SB compliance Annexure 4

Yes/No Yes

To be printed on bidder’s company letter-head


38

8

Confirm that the status of all Landing Gear Shipsets will

be without any watch item and limited to MPD

requirement

Yes/No Yes

9

Confirm that the LLP’s status of the Landing Gear

Shipsets meets the requirement of Airbus ALS part 1

and provided with each shipset

Yes/No Yes

10 Confirm that all the FAA/EASA AD's issued as of

04/06/2018 will be complied with. Yes/No Yes

11 ‘Back-to-birth' traceability will be provided for LLPs and

major components with each shipset Yes/No Yes

12 DGCA approval validity with current validity. If no

current DGCA approval submit DGCA application status.

Yes/No

…………

Yes

13

Minimum required warranty is 3000 landings or 36

months whichever occurs earlier. Warranty is

transferable/assignable.

Yes/No Yes

14

5% of value of Four Landing Gear Shipset Fixed price as

Security Deposit that shall be retained by Air India till the

warranty of all shipsets are completed.

Yes/No Yes

15

Confirm Advance Exchange for A319/A320 & A321

aircraft on schedule and overhaul requirement as

indicated will be met. Provide Advance Exchange

Landing gear shipset details with estimate TSN & CSN.

Yes/No Yes

16

We require a draft copy of agreement along with Price

bid. Confirm that a draft copy of agreement is enclosed

with Price bid

Yes/No Yes

17 We require Annexure 1,2 , 3 &7 to be part of a signed

contract. Please confirm. Yes/No Yes

18 The duly signed integrity pact must be submitted along

with the Technical Bid. Confirm. Yes/No Yes

19 Capability of concession repair beyond CMM limits with

approval of OEM Yes/No Yes

20

Landing Gears inspection/tear-down report with proposed

rectification action shall be provided for evaluation

providing the material and labour charges separately in

weekly status report

Yes/No Yes

21 Delivery Report EASA Form , FAA Form 8130-3,

EASA/FAA Dual Release Form Yes/No Yes

22

All overhauled landing gears should be supplied to Air

India with LLP, SB, AD compliance lists,

FAA/EASA/DGCA or equivalent certification and Non

Incident Statement by Quality department with complete

Dirty Finger Print of overhaul in soft copy

Yes/No Yes


39

23

The final overhaul report shall contain the following

substantiating data or reasonable equivalent (to the extent

such data is applicable):

Overhaul Agency/ Outsourced Vendor/OEM shop report.

Work scope (routine, non-routine and materials)

Vendor/OEM concession/repair authorization / overhaul

instructions/Shop Certification/BTB Doc

Yes/No Yes

24

Tender is for 27 A320 family aircraft - quantity Fifteen of

A319 / A320 aircraft and quantity Twelve of

A321aircraft, however Air India reserves the right to

amend/modify number of aircraft

Yes/No Yes

25

Earnest Money Deposit of USD 25,000.00 with wire

transfer details. Proof of Wire transfer to be provide with

this Technical Bid

Yes/No Yes

26 List of Documents with enclosures submitted with the

Technical Bid Yes/No Yes

Note: Criteria for Technical Evaluation (Any bidder not fulfilling below criteria shall be rejected)

1. Bidders must have experience of carrying out overhaul of at least 10 ship sets of A320 family

Landing Gears.

2. Bidders must provide Advance Exchange Landing Gear Shipset details as part of Technical bid with

estimated hours and cycle at delivery and confirm delivery schedule compliance. One ship set means

as per Delivery Configuration under Annexure 2.

3. Bidders must bid with at least Two Advance Exchange Landing Gear Shipset for A319/A320 or

Two advance exchange shipsets for A321 or Four advance exchange shipsets two for A319/A320

a/c & two for A321 a/c.

4. Bidders must quote for minimum warranty of 3000 landings or 36 months whichever occurs earlier.

5. EASA and DGCA current approval/ updated status.

6. Bidders must agree for separate agreement to execute logistic door to door delivery of landing gear

shipsets inclusive of packing, freight and duty payment to and from Air India facility at Kolkata,

Delhi and Mumbai.


40

ANNEXURE ‘6’

PRICE BID – TERMS

1. The Fixed Price shall be for repair & overhaul of landing gear shipset inclusive of receiving,

cleaning, Disassembly, preliminary inspection, bushing Removal, paint stripping, Stress relief,

cadmium stripping, and clean-up corroded surfaces, NDT inspection, detailed table inspection

and analysis. Repair schemes of mechanical parts and/or Components within and out of

overhaul manual limits. Cadmium / chromium plating, de-embrittlement, post plate treatment,

Bushing replacement, painting, and pre-assembly process, Bush sealing and

painting,Reassembly and functional test, Final Inspection / Preparation for shipment.

Repair/restoration/overhaul of all On Condition items/components(hydraulic and electrical)

such as Harnesses and Actuators etc covering

c) Materials

All materials upto unit part number price of USD 5000 (AT JAN 2018

ECONOMIC CONDITION) and cost of Modification Kit used during the

overhaul/ up gradation

All materials for compliance with all applicable mandatory inspections/

modifications issued by FAA/EASA, France as on D2/N2/2018.

Cost of testing,repair/restoration/overhaul of on-condition equipment

(hydraulics, electrical etc.)

d) Labour

All man-hours required for overhaul/upgradation of the gear.

All labour required for re-work beyond CMM limits including

chromium/nickel plating.

Labour for test/ repair/restoration/overhaul of on-condition component

equipment.-(hydraulic, electrical etc).

Exceptions allowed on the Fixed Price are repair or replacement of major items whose unit

price exceeds USD 5000 (AT JAN 2018 ECONOMIC CONDITION)such as the Sliding Rod,

Cylinder Barrel etc.

The Advance Exchange Fee

Fixed Fee in currency

Preferably quotes should be in US Dollars. The quotes should be firm for the entire period of

the contract.

2. Please quote for complete overhaul each of the landing gear aircraft wise in the Price bid

format. Also provide split up of material and labour charges for each landing gear.

3. The bidders must quote the prices in absolute value for all gears which are scheduled for

removal till 2020. No escalation formula or calculation formula in relation with material and

labor index will be accepted.

4. The prices quoted should be inclusive of all the direct & indirect taxes, VAT, duties, levies,

royalties, surcharges including withholding taxes applicable if any in the country of repair

vendor.


41

5.

Air-India reserves the right to exclude any of the Gears from the program.

6. The successful bidder will arrange through designated agency, logistics for air shipment of

landing gear ship sets (including cost of packaging, Insurance and other applicable costs)

to/fro Air India facility at Kolkata & Mumbai.

The selected bidder will also arrange for Custom clearance upon arrival at Kolkata/Delhi and

Mumbai towards which, AIL shall render assistance on documentation.

7. Air India will handover the removed landing gear within 15 working days to the designated

agency appointed by the successful bidder after receiving of the landing gears for onward

despatch by air.

8. The selected bidder will arrange logistics for shipment of the removed ship set (including

Insurance and other applicable costs) through designated agency to the facility of the

successful bidder. The export clearance will be the responsibility of successful bidder. For all

export formalities AIL shall render assistance on documentation.

9. Please specify freight charges separately for both journeys (to and from Air India, Kolkata,

Delhi & Mumbai) in the Price bid format.

10. In case a bidder does not accept standard payment terms of 60 days, the Price bid would be

loaded by financing cost @ 18 % per annum for the difference between 60 days and the actual

credit period offered by the bidder. No charges, other than the charges reflected above would

be borne by Air India Ltd.

11 Quotation for Exception allowed on Fixed Price must reflect the work performed with

substantiating data or reasonable equivalent (to the extent such data is applicable):

a) Overhaul agency/ Vendor/OEM shop report

b) Work scope (routine, non-routine and materials)

c) Overhaul agency/ Vendor/OEM concession/repair and overhaul

instructions/certification/replacement against scrap with FAA/EASA/BTB

documents

d) Overhaul agency/ Vendor/OEM invoice and billing summary

12. Disposal of scrapped high cost item -Air India reserves the right on the scrapped items and to

be suitably disposed through salvage program agency.

Evaluation will be based on total minimum cost to Air India for advance exchange,

overhaul & logistic for 27 A320 family aircraft - quantity Fifteen of A319 / A320 aircraft

and quantity Twelve of A321aircraft, however Air India reserves the right to

amend/modify number of aircraft under the contract.

The contract shall be finalized and signed with the bidder(s) who shall be selected for

advance exchange and overhauling of the landing gears for A319/A320 & A321

respectively or both A319/A320 & A321.

***********


42

PRICE BID FORMAT

Annexure – 7

PRICE BID FORMAT SN Aircraft

Landing

Gear

Currency Fixed Price

of complete

Overhaul

A

Import Air

Freight

charges

B

Export Air

Freight

charges

C

Advance

Exchange

fee

D

Total price

=

A+B+C+D

Total price for

ship set =

RH-MLG +

LH-MLG +

NLG

Labour

Man-hour

Rate

% mark-up

and capping

on

material cost

1 VT-SCS

LH-MLG

RH-MLG

NLG

2 VT-SCL

LH-MLG

RH-MLG

NLG

3 VT-SCM

LH-MLG

RH-MLG

NLG

4 VT-SCT

LH-MLG

RH-MLG

NLG

5 VT-SCR

LH-MLG

RH-MLG

NLG

6 VT-SCO

LH-MLG

RH-MLG

NLG

7 VT-SCU

LH-MLG

RH-MLG

NLG

8 VT-SCQ

LH-MLG

RH-MLG

NLG



43

Annexure –7 SN Aircraft

Landing

Gear


of complete

Overhaul

A

Import Air

Freight

charges

B

Export Air

Freight

charges

C

Advance

Exchange

fee

D

Total price

=

A+B+C+D

Total price for ship

set =

RH-MLG +

LH-MLG +

NLG

Labour

Man-hour

Rate

% mark-up

and

capping on

material

cost

9 VT-SCW

LH-MLG

RH-MLG

NLG

10 VT-SCV

LH-MLG

RH-MLG

NLG

11 VT-SCX

LH-MLG

RH-MLG

NLG

12 VT-EDC

LH-MLG

RH-MLG

NLG

13 VT-EDD

LH-MLG

RH-MLG

NLG

14 VT-EDE

LH-MLG

RH-MLG

NLG

15 VT-EDF

LH-MLG

RH-MLG

NLG

Volume Discount for A319/A320 -----------------

Import & Export Air Freight charges for transportation of gear from Repair vendor from & to Air India Limited, Kolkata, Delhi and Mumbai .

Inclusive of packing charges for core (removed) landing gear shipsets. GST shall be paid by Air India. Customs charges in India if applicable shall

be reimbursed at actual.

Signature of the bidder

Name:______________________

Designation:_________________



44

PRICE BID FORMAT

Annexure – 7 SN Aircraft

Landing

Gear


of complete

Overhaul

A

Import Air

Freight

charges

B

Export Air

Freight

charges

C

Advance

Exchange

fee

D

Total price

=

A+B+C+D


set =

RH-MLG +

LH-MLG +

NLG

Labour

Man-

hour

Rate

% mark-up

and

capping on

material

cost

1 VT-PPJ

LH-MLG

RH-MLG

NLG

2 VT-PPK

LH-MLG

RH-MLG

NLG

3 VT-PPL

LH-MLG

RH-MLG

NLG

4 VT-PPM

LH-MLG

RH-MLG

NLG

5 VT-PPN

LH-MLG

RH-MLG

NLG

6 VT-PPO

LH-MLG

RH-MLG

NLG

7 VT-PPQ

LH-MLG

RH-MLG

NLG

8 VT-PPT

LH-MLG

RH-MLG

NLG



45

PRICE BID FORMAT

Annexure – 7

SN Aircraft

Landing

Gear


of complete

Overhaul

A

Import Air

Freight

charges

B

Export Air

Freight

charges

C

Advance

Exchange

fee

D

Total price

=

A+B+C+D


set =

RH-MLG +

LH-MLG +

NLG

Labour

Man-hour

Rate

% mark-

up

and

capping

on

material

cost

9 VT-PPU

LH-MLG

RH-MLG

NLG

10 VT-PPV

LH-MLG

RH-MLG

NLG

11 VT-PPW

LH-MLG

RH-MLG

NLG

12 VT-PPX

LH-MLG

RH-MLG

NLG

Volume Discount for A321 -----------------

Volume Discount for A319/A320 and A321-------------------

Import & Export Air Freight charges for transportation of gear from Repair vendor from & to Air India Limited, Kolkata, Delhi and Mumbai .

Inclusive of packing charges for core (removed) landing gear shipsets. GST shall be paid by Air India. Customs charges in India if applicable shall

be reimbursed at actual.


Name:______________________

Designation:_________________



46

CERTIFICATION

Certified that:

1. There are no hidden costs to Air India Ltd. over and above the charges quoted.

2. We agree to hold the quoted offer firm till completion of Contract.

3. We have read, understood, and agree to comply with the terms & conditions of the tender


Name:______________________

Designation:_________________



47

ANNEXURE – 8

UNDERTAKING CERTIFICATE

To

Dy. General Manager

Materials Management Dept.

New Engineering Complex, Sahar, Vile Parle(East),

Mumbai 400099

Sir,

It is certified that we have studied and understood the terms and conditions of the tender for Advance

Exchange and overhauling of Landing gears for A319 A320 & A321 aircraft vide Tender Enq.

No………….and agree to abide by the same unconditionally.

AUTHORISED SIGNATORY



48

ANNEXURE – 9

AUTHORIZATION LETTER FOR ATTENDING BID OPENING

To

Dy. General Manager

Materials Management Dept.

New Engineering Complex, Sahar, Vile Parle(East),

Mumbai 400099

Dear Sir,

Sub: Authorization for attending opening of TECHNICAL / PRICE BID vide Tender Enq.

No……………..

On Tender Date: Closing Date:

Opening Date: Time:

The following person(s) is/are hereby authorized to attend Technical/ Price bid opening of subject tender.

S.No. Name E.Mail Contact No Signature

Signature: ………………………………..

Authorized Signatory’s Name:……………..

Company Name: ………………………

NOTE:

1. Permission for entry to the Hall where bids are opened may be refused in case authorization as

prescribed above is not received.

2. The authorized representatives, in their own, interest, must reach venue of bid opening well in time.

3. The authorized representatives must carry a valid photo identity.

4. Separate authorization letters would be required for Technical and Price bid opening.

*************
