moqa program sky airline - international civil aviation ... · pdf filemoqa program sky...

MOQA Program SKY Airline RASG-PA Flight Data Analysis Programme seminar (FDAP) | Miami Oct_16

Una nueva experiencia…

Claudio Tobar J. Flight Data Monitoring Chief

[email protected]

A new experience…

mailto:[email protected]

Content

Data Process

ACMS - MOQA

MOQA Management

Specific Maintenance Events

Components - Monitoring

MOQA Initiatives

1

2

3

4

5

6

Data Process

Flight Data Interface Management Unit

(FDIMU)

Computador de Adquisición de datos.

Wireless GroundLink® (WGL) System

Computador grabador y

Transmisor de datos

Local Cell Tower

Internet

Server Data Analysis

AirFASE®- Aircraft Flight

Analysis & Safety Explorer

Operations Maintenance & Engineering

Data Analysis

Flight Data Monitoring

Content

Data Process

ACMS - MOQA

MOQA Management



MOQA Initiatives

1

2

3

4

5

6

MOQA (Maintenance Operation Quality Assurance)

Principio de adquisición de datos para MOQA


Crash protected Flight Data Recorder (DFDR) 25 Hours recorder time

Flight Data Interface Management Unit (FDIMU)

WQAR Comm+ Servidor Wireless

ACMS Aircraft Condition Monitoring System

ACMS MOQA


Flight Data Interface Management Unit (FDIMU)

Generar grabaciones de datos de vuelo no Mandatorios con Parámetros específicos a monitorear.

Crear Reportes con información específica de componentes y sistemas del avión.

Creación de nuevas MCDU Display (información entrada/salida) para las tripulaciones de vuelo.

ACMS: Función de procesamiento dentro de sistemas de Adquisición, FDIMU/DMU.

Aplicaciones

ACMS | Funciones para MOQA


Las principals funciones del ACMS son:

Adquisición de Parámetros

Lógica de Eventos / Trigger

Generación de Reportes

MCDU Displays

Grabación de Raw Data y Mensajes

• ACARS Management Unit • Flight Deck Printer • QAR (Quick Acces Recorder) • DAR (Direct Access Recorder)

Interfaz con:

Content

Data Process

ACMS - MOQA

MOQA Management



MOQA Initiatives

1

2

3

4

5

6

MOQA Process SKY… Flight Data Monitoring

Server Data Analysis

Data Analysis

ACARS (Aircraft Communications Addressing and Reporting System)

FDIMU (Flight Data Interface Management Unit)

Data Analysis

ENG Oil Report IDG Oil Report APU Report

Data Mantto.

ACARS Data

Raw Data

ING.

PLANNING

T/S

MANTTO.

CCM

Comité_MOQA

ACMS

MOQA Benefits

MOQA: Maintenance Operation Quality Assurance

Aumenta la disponibilidad de datos de mantenimiento.

Mejora en la disponibilidad de la aeronave, permitiendo el mantenimiento preventivo.

Mejora la detección de problemas en el avión antes de que se conviertan en riesgos para la seguridad.

Mantenimiento Preventivo

Datos Mantenimiento

Fuel Saver

Disponibilidad despacho

APM Aircraft Perf. Monitoring


Software ACMS

Software data Frame A319 Fleet…


Data Frame A319

1024 wps


Data Frame A319 | Reportes Flight Data Monitoring

Software data Frame flota A320…


Data Frame A320

512 wps


Data Frame A320 | Reportes


Eventos | Parámetros MOQA

Eventos MOQA

• Engine Shut Down in Flight

• EGT Warning • Climb / Idle / Takeoff / Engine Start

• Vertical Acceleration High at Touch Down • Vertical Acceleration High During Flight

• Speed Above MMO/VMO • Speed Above VFE

• Overweight Landing

• Rejected Takeoff Detected


Ingeniería & Mantenimiento

Events & Parameters

Hard Landing / Overweight Landing

VMO/MMO Exceedance / Turbulence

Engine Vibration Exceedance

Engine Parameters

Fuel Consumption

Events & Parameters

Flight Controls

Ldg Gear Operation & Position

Presurization System

Door Indicating System

NLG Steering Sys. Operation/Indication


Ingeniería & Mantenimiento

Events & Parameters

Hydraulic System

APU Monitoring

Fuel System

Auto Pilot Operation

Slats / Flaps System

Events & Parameters

Electrical Power

Windshield Heater System

Bleed System

Packs System

Auto Brake / Antisked System


Parámetros en Data Frame

HYD SYSTEM ENGINE

APU (Auxiliary Power Unit)

CABIN

IDG (Integrated Drive Generator)


Nuevos Parámetros en Data Frame

ENGINE ENG 1 BLEED PB ENG 2 BLEED PB ENG2 AICE PB ENG1 AICE PB ENGINE 1 PRV POSITION ENGINE 2 PRV POSITION ENG FUEL USED ENG FUEL USED ENG2 HPV POSITION ENG1 HPV POSITION ENG1 PRECOOLER INLET P ENG2 PRECOOLER INLET P ENG 1 PRECOOLER OUTLET T° ENG 2 PRECOOLER OUTLET T° SELECTED VARIABLE STATOR SELECTED VARIABLE STATOR T2.5 (LPC EXIT TEMPERATUR T2.5 (LPC EXIT TEMPERATUR T3 (HPC EXIT TEMPERATURE) T3 (HPC EXIT TEMPERATURE) T5 TEMPERATURE AT POSITIO T5 TEMPERATURE AT POSITIO

IDG IDG 1 INLET TEMP IDG 1 OUTLET TEMP IDG 2 INLET TEMP IDG 2 OUTLET TEMP IDG 1 DISCRETES SDAC STA IDG 2 DISCRETES SDAC STAT IDG1 DISCONNECTED IDG1 DISC P/B OFF IDG1 OIL OVERHEAT IDG1 OIL LOW PRESSURE IDG2 DISCONNECTED IDG2 DISC P/B OFF IDG2 OIL OVHT IDG2 OIL LOW PRESSURE

APU APU BLEED VALVE OPEN APU FUEL LOW PRESSURE APU STARTER APU BLEED PB APU FIRE SYS. 1 APU START SWITCH APU STOP SWITCH EGT (APU) APU OIL SUMP TEMP APU GEN LOAD SYS. 1 APU GEN P/B OFF APU GEN FAULT APU GEN OVERLOAD APU MASTER SWITCH P/B OFF IGV ACTUATOR IGV LVDT IGV POSITION RPM BLEED AIR TEMP BLEED AIR PRESSURE

CABIN NO_SMOKING FASTEN SEAT BELT CABIN ALTITUDE CABIN ALTITUDE SDAC CABIN DIFF. PRESSURE SYS. CABIN PRESSURE SDAC EXCESSIVE CABIN ALTITUDE FWD CABIN COMPT TEMPERATU FWD CABIN COMPT TEMPERATU AFT CABIN COMPT TEMPERATU CKPT COMPT TEMPERATURE AFT CABIN COMPT TEMPERATU SELECTED CKPT COMPT TEMP SEL FWD CAB COMPT TEMP SY SEL AFT CAB COMPT TEMP SY

HYD SYSTEM YELLOW HYD LOW PRESSURE S YELLOW ELECTRIC PUMP P/B YELLOW ELECTRIC PUMP YELLOW ENGINE PUMP YELLOW SYS PRESSURE YELLOW RSVR QUANTITY YELLOW RSVR TEMPERATURE GREEN ENGINE PUMP GREEN SYS PRESSURE GREEN RSVR QUANTITY GREEN RSVR TEMPERATURE BLUE ELECTRIC PUMP PB BLUE ELECTRIC PUMP BLUE SYS PRESSURE BLUE RSVR QUANTITY BLUE RSVR TEMPERATURE PTU PB PTU VALVE CONTROL


Monitoreo por ATA Análisis Específicos

ATA 34 – Pitot & Static Press

ALT_STD

LH_STATIC_PRESS

RH_STATIC_PRESS

LH_PITOT_PRESS RH_PITOT_PRESS

CENTER_PITOT_PRESS


ATA 24 – IDG’s Oil Temperature

ALT_STD

IDG1_OUT_OIL_T°

IDG1_IN_OIL_T°

IDG2_OUT_OIL_T°

IDG2_IN_OIL_T°


ATA 21 – Cabin Temperature

ALT_STD

CKPT_T°

AFT_CAB_T°

FWD_CAB_T°


ATA 21 – Cabin Pressure

ALT_STD

CAB_DIF_PRESS

CABIN_ALTITUDE


ATA 27 – Flight Controls

ALT_STD

RUDD_ANGLE

LH_AILERON_POSITION

RH_AILERON_POSITION

LH_ELEV_POSITION

RH_ELEV_POSITION TAXI_OUT

ATA 28 – Fuel Temperature

ALT_STD

FUEL_T°_LH_OUTE

FUEL_T°_LH_INNE

FUEL_T°_RH_INNE

FUEL_T°_RH_OUTE

ATA 29 – HYD GRN Qty – Pressure – Temperature

ALT_STD

HYD_GRN_PRESS

HYD_GRN_QTY

HYD_GRN_T°

ATA 49 – APU Monitoring

ALT_STD

APU_RPM

APU_EGT

APU_GENERATOR_LOAD

APU_OIL_T°

APU_BLEED_AIR_FLOW


ATA 72 – Engine VSV

ALT_STD

SELECTED_VSV_ENG1

DEMAND_VSV_ENG1

Content

Data Process

ACMS - MOQA

MOQA Management



MOQA Initiatives

1

2

3

4

5

6


19

25

4

16

15

3

6

13

7

4

3

7

7

7

5

5

3

3

3

6

5

7

11

5

5

3

200 25 20 15 10 5 0

Dec

Nov

Oct

Total 136 63

Mar

Feb 1

Jan 1

Sep

Aug

Jul

Jun

May

Apr

Mar

Feb

Jan

High count

Medium count

2 2 4 3

1

47

2 2

CC-AFY

CC-ADO

CC-ABV

CC-AJF

CC-AJG

CC-AHE

CC-AFZ

CC-AMP

19

7 33

4

INC

CLB

APP

DES

# Events (Med_High Sev) by month # Events High Sev. by Aircraft

# Events High Sev. by Flight Phase # Events High Sev. by Flight Phase_AC

AC APP CLB DES INC Total ACCC-ABV 1 2 1 4CC-ADO 1 1 2CC-AFY 2 2CC-AFZ 1 1 1 3CC-AHE 1 1CC-AJF 1 1 2CC-AJG 1 1 2CC-AMP 28 19 47Total FP 4 33 7 19 63


ATA 27 – Flight Controls AL

T_ST

D

CONF

SLAT FLAP

CONF 1+F

CONF 1

CONF 0

FLAP

_LEV

ER_P

OS

FLAP_ANGLE

SLAT_ANGLE

SLAT: 0 FLAP: 0

POS_0: OFF

POS_1: ON

POS_1: OFF

POS_0: ON 10:52:27

POS_2: OFF

POS_3: OFF

POS_FULL: OFF

4 seg

10:52:27

10:52:51

TIME FLAP 0: 8 seg

TIME SLAT 0: 24 seg

10:52:27

10:52:35


ATA 27 – Flight Controls AL

T_ST

D

CONF SLAT FLAP

CONF 1+F

CONF 1

CONF 0

FLAP

_LEV

ER_P

OS

FLAP_ANGLE

SLAT_ANGLE

SLAT: 0 FLAP: 0

POS_0: OFF

POS_1: ON

POS_1: OFF

POS_0: ON 21:51:42

POS_2: OFF

POS_3: OFF

POS_FULL: OFF

2 seg

21:51:43

21:51:55

TIME FLAP 0: 7 seg

TIME SLAT 0: 12 seg

21:51:43

21:51:50


ATA 28 – Fuel

ATA 28 – Fuel Indication (CC-AMP)

800 kg


ATA 28 – Fuel Indication | Intercambio

CC-AMP LOAIZA CELIS-GALAZ HAFEMANN SCL

TRANSIT CHECK.A319-53/1721 AFT CARGO FLOOR PANELSE EFECTUO EI-2015-25-047 REMOVE LIFE LINE DECAL.CERRADO DMI N° 131, SE REEMPLAZO SUN VISOR CLIP CAPT SIDE.G/I AUTO FEED FAULT WITH CENTER QTY INDICATION EMPTY. SIGUIENDO EL T/SH, SE INTERCAMBIAN FUSER ADAPTOR 7509 UCB Y 7512UCB CON A/C AJG. TEST EN AMBOS OK.

“Fused Adaptor”

CC-AMP CC-AJG


ATA 28 – Fuel Indication (CC-AJG)

LH INNER FUEL QTY IND

700 kg

CENTER TANK FUEL QTY INDICATION


ATA 32 – Landing Gear

ATA 32 – Brake Temperature

BRAKE_T°_1

BRAKE_T°_2

BRAKE_T°_3

BRAKE_T°_4

BRK_T°_1 Abnormal Indication


ATA 32 – Brake Temperature

WIRING DAMAGE (conector)


ATA 34 – Navigation

ATA 34 – Autoland Fail

RA#1 FAIL

RA#1 FAIL RA #2


ATA 34 – Autoland Fail


Presenter

Presentation Notes

El coaxial hacia contacto entre sus partes (malla con alma)

ATA 34 – Navigation

ATA 34 – TAT & Pitot Temperature

Eventos Detectados hasta la Fecha. AFX_SCL-FLN (TAT & PITOT RH)

ICE Event



ZONA 1



ZONA 2



ALT_STD

TAT 1

TAT 2

TAT 3

Zona 1

Zona 2


ATA 34 – TAT & Pitot Temperature Flight Data Monitoring

Envío de Raw Data Airbus

Análisis para Operaciones

Análisis para Ingeniería & Mantto. SKY

ATA 35 – Oxygen

ATA 35 – Crew Oxygen Leak Flight Data Monitoring

ATA 35 – Crew Oxygen Leak


Crew Oxygen Leak

Recambio Botella

ATA 35 – Oxygen Pressure

ALT_STD

OXY_PRESS

TAT



0100200300400500600700800900

1000110012001300140015001600170018001900

PRES

ION

DE

OXY

EN

PSI

Flights

OXY-PRESS

OXY

1300 psi

1800 psi




0100200300400500600700800900

100011001200130014001500160017001800190020002100

1011

0919

4155

1015

1420

1111

2113

0013

2547

2205

3218

2040

8323

218

5036

1015

0418

4147

2427

1234

5322

3728

2140

5116

2320

2201

5218

4737

9152

820

1424

1423

2621

5718

1946

1122

2415

1626

5921

5504

1617

5714

3117

1004

0719

4058

2222

2018

3031

1215

2121

4336

1740

0812

3202

1857

4314

944

1453

4883

121

1822

4411

2653

2230

1319

4214

1329

1195

120

2322

1716

5937

2350

3418

1347

1537

5323

1854

1641

4722

2143

1315

3920

3815

1229

4722

4125

1710

4710

2229

1853

5491

818

1901

0311

0817

1750

4731

201

1642

0622

1407

1652

3322

1211

9/1/20169/2/20169/3/20169/4/20169/5/20169/6/20169/7/20169/8/20169/9/20169/10/20169/11/20169/12/20169/13/20169/14/20169/15/2016

9/16/20169/17/2016

9/18/20169/19/20169/20/20169/21/20169/22/20169/23/20169/24/20169/25/20169/26/20169/27/20169/28/20169/29/201610/1/201610/2/201610/3/201610/4/201610/5/201610/6/201610/7/201610/9/201610/10/201610/11/201610/12/201610/13/201610/14/201610/15/2016

10/16/201610/19/201

6

CC-AJF

Sep Oct



0100200300400500600700800900

100011001200130014001500160017001800190020002100

1424

4521

5336

2017

1011

5445

1147

5382

609

2156

2420

2549

1431

1712

5006

9165

416

2521

2156

0219

5507

1116

2415

1312

1952

0314

0318

2213

5522

5752

2217

5722

4802

1620

4011

4707

1522

922

4444

1291

220

1654

1540

2910

1738

1232

622

5113

1832

1718

3258

1623

5790

924

2491

623

0645

1621

4214

3207

2140

1590

841

2007

2520

1248

1626

3318

3851

1155

4121

4221

2304

3285

630

2320

12

9/1/2016

9/2/2016

9/3/20169/5/20169/6/20169/7/20169/8/20169/9/20169/10/20169/11/20169/12/20169/13/20169/14/20169/15/20169/16/20169/17/2016

9/18/20169/19/20169/20/20169/21/20169/22/20169/23/20169/24/20169/25/20169/26/20169/27/20169/28/20169/29/20169/30/201610/3/201610/4/201610/5/201610/6/201610/7/201610/8/201610/9/201610/10/201610/11/201610/12/201610/13/201610/14/201610/15/2016

10/16/201610/17/2016

10/18/201610/19/2016

CC-AJG

ATA 49 – APU (Auxilliary Power Unit)

ATA 49 – Oil Temperature

APU_RPM

APU_OIL_T°

APU AUTO SHUTDONW HIGH OIL T°

163 °C


ATA 49 – Oil Temperature

APU OIL COOLER CLOGGED AND POLLUTED


Takeoff Aeropuertos cercanos volcán Calbuco

ATA 77 – Engine Indicating

ATA 77 – Engine Vibration

VIB_N1_ENG1

VIB_N1_ENG2

VIB_N2_ENG1

VIB_N2_ENG2

BIRD STRIKE EVENT (MAX VIB 9,6) 9,6


ATA 77 – Engine Vibration

FAN BLADE DAMAGE


Hyd Green Sys Low Press

Hydraulic Green System Low Press


AirmanWeb



HYD GREEN PRESS (PSI) Normal

HYD GREEN PRESS 0 (PSI)

HYD GREEN T°

HYD GREEN QTY

ALT_STD

ENG HYD GREEN PUMP OFF



LOST

Vertical Acceleration High in Flight

Vertical Acceleration High in Flight Flight Data Monitoring

VRTG: 1,89 g CAS: 279 kts ALT_STD: 11000 ft CONF: 0 LDG_GEAR: UP


CONF 0

Lateral Acceleration

NO AP

FSB ON

Longitudinal Acceleration

1.89 g

0.43 g

Content

Data Process

ACMS - MOQA

MOQA Management



MOQA Initiatives

1

2

3

4

5

6

Health Monitoring APU

Health Monitoring APU

ACARS (Aircraft Communications Addressing and Reporting System)

FDIMU (Flight Data Interface Management Unit)

MACRO

Engine Oil Report • OIQ – Oil Quantity • OIP – Oil pressure • OIT – Oil Temp.

IDG Oil Report • IDG OLV – Oil Level • IDGT – Oil temp. • IDG RISE – Oil Rise

APU Report 13 Health Monit. • EGTA (Exhaust Gas Temp) • STA (APU Start Time) • EGTP Peak • IGV (Inlet Guide Vane) Position • NPA (APU Peak Speed) • PT (Bleed Air Pressure)


Health Monitoring APU Flight Data Monitoring

IDG Oil Temperature Warning

Oil Temperature Warning Flight Data Monitoring

“OIL OUT” – “OIL IN” = IDG OIL T° Difference

= Temperatura x trabajo IDG IDG OIL T° Difference

OIL IN

OIL OUT

IDG Oil Temp Difference (Sal – Ent | T°)


570

036

881008232

67773949

0

100

200

300

400

500

600

Total Oct Feb Jan Sep Ago Jul Jun May Abr Mar

High Sev.

000

50

100

150

200

Total CC-AIC

High Sev.

IDG 2

1971

1946

1871

1342

1758

1633

111 (Oct)

2080

2028

2029

1258

Oct_16

Oil Temperature Warning Flight Data Monitoring

IDG 1 DIF

IDG 2 DIF

ALT_STD

IDG Oil Cooler System

Oil Cooler System Flight Data Monitoring

OIL IN

OIL OUT

OIL OUT= T° de Aceite de Salida (incluye trabajo de cooler)

= Temperatura de aceite de salida de la IDG IDG OUT OIL TEMP

IDG Oil Temp | by Month & Severity


220

763 05213

38

141161

0

19

118

7259

9579

59

16

150

100

50

0

650

600

550

Med

525

Low

648

Sep

14 1

Ago

85

Jun

0

May

0

Abr

62

Mar Oct

131

Feb Jul High

Low count

Medium

High

106

16

0

00

00

0

0

5

10

15

20

25

30

35

Total AHC AIC

Low

Medium

High

Oil Cooler System

OIL IDG 2 OUT T° = 140°

OIL IDG 2 IN T°

OIL IDG 1 OUT T°

OIL IDG 1 IN T°

ALT_STD

FRV-2_I

FRV-2_II

FRV-1_I

FRV-1_II


Oil Cooler System

ENG 2 OIL T° = 127°

ENG 1 OIL T°

ALT_STD


Engine Vibration

Engine Vibration N1 & N2 Flight Data Monitoring

Engine Vibration (Birdstrike)

VIB_N1_ENG2: 5.0 unit

VIB_N1_ENG1: 2.0 unit

ALT_STD

N1_1

N1_2


Engine Vibration (Birdstrike)

0123456789

1011

12-Nov 2-Dec 22-Dec 11-Jan 31-Jan 20-Feb 11-Mar 31-Mar 20-Apr

VIB

Date

Vibración N1 / CLB

VIB_11 VIB_12

0123456789

1011


VIB

Date

Vibración N1 / TKO

VIB_11 VIB_12

0123456789

1011


VIB

Date

Vibración N1 / CRS

VIB_11 VIB_12

0123456789

1011


VIB

Date

Vibración N1 / DSC

VIB_11 VIB_12


Content

Data Process

ACMS - MOQA

MOQA Management



MOQA Initiatives

1

2

3

4

5

6

Iniciativas MOQA

Rigging (Alerones, Rudder con Desviación)

Generación de Reportes ACMS: (1) Uso de APU por Aeropuerto y Flota. (2) Tiempo y % de conexión de energía EXT_PWR.

Generación de Data Base ACMS (A319/A320)

Identificación de problemas en aeronaves que generan mayor consumo de combustible, generando acciones correctivas para solucionar fallas previamente identificadas. Rigging

Uso de APU


Iniciativas MOQA – Preventivas y Predictivas

Programa de Monitoreo Online y Reportes de Tendencias APU_Health Monitoring, Engine Vibration y Oil Temp. IDG.

Componentes Removidos Preventivamente.

Soporte a CCM_H24 Análisis eventos AOG, Análisis eventos No AOG.

Monitoreo Continuo MOQA IDG Oil Temp. Monitoring

Soporte FDM eventos AOG


Questions…


Depto. Flight Data Monitoring E-mail: [email protected] Tel: (56-2) 2663 3877

www.skyairline.com

BEST REGIONAL AIRLINE IN SOUTH AMERICA 2014 / 2015

mailto:[email protected]

moqa program sky airline - international civil aviation ... · pdf filemoqa program sky...

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