# Service difficulty reports: N178AW, cancelled Feb 9, 2005

A list on [N178AW, cancelled Feb 9, 2005](https://openairdocs.org/deregistered/N178AW-2005-02-09.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 135 reports

- [SDR AWXA200400848](https://openairdocs.org/sdr/AWXA200400848.md): Transmitter · false indication · Aug 3, 2004 · N178AW · Boeing 737277 · Engine Oil Pressure
  > ON CLIMBOUT OF LAS EN ROUTE FOR SFO AT FL 190 NR 1 ENGINE OIL PRESSURE DROPPED TO 10 PSI, FOLLOWED QRH AND SHUTDOWN NR 1 ENGINE, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IAW BMM
- [SDR AWXA200400841](https://openairdocs.org/sdr/AWXA200400841.md): Transmitter · faulty · Aug 1, 2004 · N178AW · Boeing 737277 · Engine Pressure Ratio (EPR)
  > ON TAKEOFF ROLL AT LAS EN ROUTE FOR LAX NR 1 ENGINE TAKEOFF EPR ONLY REACHED 1.57, NR 2 ENGINE WAS NORMAL, REJECTED TAKEOFF AT 75 KTS. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER IAW BMM 77-011-21-4. ENGINE RUN OPERATIONAL TEST WAS GOOD. VEN
- [SDR AWXA200400577](https://openairdocs.org/sdr/AWXA200400577.md): Battery · discharged · May 26, 2004 · N178AW · Boeing 737277 · Emergency Lighting
  > DEN - EEL - DURING 4-DAY CHECK THE OVERHEAD (CEILING) EMERGENCY EXIT LIGHT AT SEAT ROW 9 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK AT BS 617, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400345](https://openairdocs.org/sdr/AWXA200400345.md): Battery · discharged · Apr 4, 2004 · N178AW · Boeing 737277 · Emergency Equipment
  > PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400309](https://openairdocs.org/sdr/AWXA200400309.md): Splice · broken · Mar 25, 2004 · N178AW · Boeing 737277 · Electrical Connectors
  > PHX - EEL - FLIGHT CREW REPORTED EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION, IN ON POSITION ALL EMERGENCY EXIT LIGHTS ILLUMINATED, AND IN OFF POSITION ALL EMERGENCY LIGHTS WERE OFF. MAINTENANCE FOUND OPEN SPLICE, REMOVED AND REPLACED SPLI
- [SDR AWXA200400301](https://openairdocs.org/sdr/AWXA200400301.md): Charger · failed · Mar 22, 2004 · N178AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED AND REMAINED ON WITH THE FLIGHT DECK SWITCH IN ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER AT BS 920 AND BATTERY PACKS AT SEAT ROWS 3, 11 & 17 LT A
- [SDR AWXA200400229](https://openairdocs.org/sdr/AWXA200400229.md): Battery Pack · discharged · Feb 26, 2004 · N178AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING 4-DAY CHECK FOUND THE L-1 & R-1 DOOR EXTERNAL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN FORWARD CARGO COMPARTMENT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400199](https://openairdocs.org/sdr/AWXA200400199.md): Battery · discharged · Feb 20, 2004 · N178AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING 4-DAY CHECK MAINTENANCE FOUND THE LT FORWARD AND MID CABIN SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT BATTERIES AT SEAT ROWS 4 AND 11, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200301569](https://openairdocs.org/sdr/AWXA200301569.md): Reflector · defective · Dec 20, 2003 · N178AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING 4-DAY CHECK FOUND THE R-2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOPERATIVE, AFTER BULB REPLACEMENT LIGHT WAS INTERMITTENT. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT REFLECTOR ASSEMBLY. OPERATIONAL CHECK WAS
- [SDR AWXA200301568](https://openairdocs.org/sdr/AWXA200301568.md): Reflector · defective · Dec 20, 2003 · N178AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING 4-DAY CHECK THE RT LOWER EXTERNAL GROUND ILLUMINATION EMERGENCY ESCAPE LIGHT WAS FOUND INOPERATIVE, BULB REPLACEMENT HAD NO EFFECT. MAINTENANCE REMOVED AND REPLACED RT LOWER EXTERNAL GROUND ILLUMINATION EMERGENCY ESCAPE LIGHT REFLECTOR ASSE
- [SDR AWXA200301513](https://openairdocs.org/sdr/AWXA200301513.md): Cover · damaged · Dec 5, 2003 · N178AW · Boeing 737277 · Passenger/Crew Doors
  > DURING CLIMB OUT OF OAK EN ROUTE FOR PHX A VERY LOUD SQUEALING SOUND WAS OBSERVED COMING FROM THE L-1 DOOR LOWER FORWARD HINGE SEAL, PRESSURIZATION WAS NORMAL, TURNED BACK TO OAK DUE TO LOUD NOISE. MAINTENANCE FOUND THE LOWER HINGE COVER DAMAGED. REMOVED AND
- [SDR AWXA200301262](https://openairdocs.org/sdr/AWXA200301262.md): Battery Pack · discharged · Oct 16, 2003 · N178AW · Boeing 737277 · Emergency Lighting
  > DURING INSPECTION THE L-2 & R-2 DOOR EMERGENCY EXIT EXTERIOR LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT ESCAPE SLIDES BATTERY BACK IN THE AFT CARGO COMPARTMENT BS 920 IAW BMM 33-51-71, OPERATIONAL CHECK C/W IAW BMM 33-51-11.
- [SDR AWXA200301057](https://openairdocs.org/sdr/AWXA200301057.md): Garlock Seal · failed · Sep 13, 2003 · N178AW · Boeing 737277 · AC Generator-Alternator
  > ON CLIMB OUT OF PHX EN ROUTE FOR BOI THE NR 1 GENERATOR TEMPERATURE WENT INTO THE YELLOW FOLLOWED BY A GENERATOR HIGH TEMPERATURE LIGHT, ATTEMPT APU START WITH NO SUCCESS. FOLLOWED QUICK REFERENCE HANDBOOK AND DISCONNECTED THE NR 1 GENERATOR, TURNED BACK TO PH
- [SDR AWXA200301004](https://openairdocs.org/sdr/AWXA200301004.md): Wire · broken · Aug 31, 2003 · N178AW · Boeing 737277 · Light System Wiring
  > DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200300772](https://openairdocs.org/sdr/AWXA200300772.md): Circuit Breaker · weak · Jul 2, 2003 · N178AW · Boeing 737277 · Light System Wiring
  > EN ROUTE FROM AUS TO PHX ALL EMERGENCY EXIT LIGHTS ILLUMINATED. EMERGENCY EXIT LIGHT WAS SWITCHED OFF TO CONSERVE BATTERY ENERGY. MAINTENANCE FOUND A WEAK EMERGENCY LIGHT SYSTEM CONTROL CIRCUIT BREAKER (5 AMP) ON THE P-18 PANEL. REMOVED AND REPLACED 5 AMP C
- [SDR AWXA200300687](https://openairdocs.org/sdr/AWXA200300687.md): Skin · corroded · May 15, 2003 · N178AW · Boeing 737277 · Wing, Plate/Skin
  > DURING C-15 CHECK CORROSION WAS FOUND ON LT WING LOWER SURFACE SKIN AT NR 2 FLAP TRACK ATTACH POINT. MAINTENANCE REMOVED CORROSION ON LT WING LOWER SURFACE SKIN BY MACHINING A FLAT STEP; PERFORMED A HFEC INSPECTION TO VERIFY MACHINED AREA WAS NOT CRACKED; FAB
- [SDR AWXA200300683](https://openairdocs.org/sdr/AWXA200300683.md): Skin · cracked · May 15, 2003 · N178AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING C-15 CHECK A.375 INCH CRACK WAS FOUND AT FASTENER HOLE ON FUSELAGE SKIN, LOWER FORWARD CORNER OF R-1 DOOR CUTOUT BS 294.5. MAINTENANCE REMOVED FASTENER AT LOWER FORWARD CORNER OF R-1 DOOR CUTOUT BS 294.5; PERFORMED NDT INSPECTION TO VERIFY CRACK CONTA
- [SDR AWXA200300686](https://openairdocs.org/sdr/AWXA200300686.md): Skin · delaminated · May 14, 2003 · N178AW · Boeing 737277 · Trailing Edge Flaps
  > DURING C-15 CHECK THE RT OUTBOARD HINGED FLAP TRAILING EDGE WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGE AND PERFORMED COMPOSITE REPAIR IAW BAC5514-589/5101 AND DWG 65-71930.
- [SDR AWXA200300685](https://openairdocs.org/sdr/AWXA200300685.md): Door Frame · cracked · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Structure
  > DURING C-15 CHECK A.25 INCH CRACK WAS FOUND ON FRAME OF R-1 DOOR AT UPPER HINGE CUTOUT. MAINTENANCE PERFORMED A HFEC INSPECTION TO VERIFY END OF CRACK; STOP DRILLED CRACK IAW B737-200 SRM 52-00-2 FIG 7 PG 32.
- [SDR AWXA200300684](https://openairdocs.org/sdr/AWXA200300684.md): Skin · corroded · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING C-15 CHECK CORROSION WAS FOUND ON LOWER FUSELAGE SKIN AT BS 727-727A AND LT KEEL BEAM. MAINTENANCE REMOVED EXISTING DOUBLER & TRIPLER AND TRIMMED OUT CORRODED SKIN; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPLACEMENT DOUBLER
- [SDR AWXA200300682](https://openairdocs.org/sdr/AWXA200300682.md): Stringer · corroded · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 RT LOWER LOBE AT BS 907. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AND TRIMMED AWAY CORROSION ON STRINGER 27 RT, BS 907; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-45895-3 AND A
- [SDR AWXA200300649](https://openairdocs.org/sdr/AWXA200300649.md): Frame · cracked · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Frame
  > DURING C-15 CHECK A.5000 INCH CRACK WAS FOUND ON FUSELAGE LOWER LOBE FRAME AT BS 827, LBL 22. MAINTENANCE TRIMMED OUT DAMAGE ON FUSELAGE LOWER LOBE FRAME AT BS 827, LBL 22, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED FILLER, RADIUS F
- [SDR AWXA200300638](https://openairdocs.org/sdr/AWXA200300638.md): Floorbeam · cracked · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor Beam
  > YVR - MAJOR REPAIR - DURING C-15 CHECK A.25 INCH CRACK WAS ON FLOORBEAM WEB ANGLE AT BS 639, LBL 45.50. MAINTENANCE REMOVED DAMAGED FLOORBEAM WEB ANGLE AT BS 639, LBL 45.50; FABRICATED A NEW REPLACEMENT ANGLE AND STRAP; INSTALLED REPAIR PARTS IAW SB 737-53-1
- [SDR AWXA200300637](https://openairdocs.org/sdr/AWXA200300637.md): Frame · cracked · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Frame
  > YVR - MAJOR REPAIR - DURING C-15 CHECK A.5 INCH CRACK WAS FOUND ON R-1 DOOR FRAME AT AFT NR 4 STOP FITTING CUTOUT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC TO VERIFY CRACK WAS CONTAINED, ALODINED AND PRIMED IAW B737-200 SRM 51-10-2 PG 7.
- [SDR AWXA200300636](https://openairdocs.org/sdr/AWXA200300636.md): Skin · cracked · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > YVR - MAJOR REPAIR - DURING C-15 CHECK A.25 INCH CRACK WAS FOUND AT L-1 DOOR ON THE AFT EDGE OF THE CENTER DOOR STOP ACCESS HOLE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR P
- [SDR AWXA200300608](https://openairdocs.org/sdr/AWXA200300608.md): Floorbeam · cracked · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-15 CHECK A 2 INCH CRACK WAS FOUND ON TRANSVERSE FLOORBEAM WEB OUTBOARD OF LBL 45.50, BS 639. MAINTENANCE REMOVED DAMAGED ON WEB AT LBL 45.50, BS 639; FABRICATED REPAIR DOUBLERS AND A STRAP PER SB 737-53-1061 R4; INSTALLED REPAIR PARTS IAW E.R. 15-5300
- [SDR AWXA200300602](https://openairdocs.org/sdr/AWXA200300602.md): Floorbeam · cracked · May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND ON FLOORBEAM WEB AT BS 639, RBL 45-50. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM; FABRICATED A FILLER, DOUBLER, AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-2, FIG. 1, PG. 1.
- [SDR AWXA200300648](https://openairdocs.org/sdr/AWXA200300648.md): Floorbeam · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor Beam
  > YVR - MAJOR REPAIR - DURING C-15 CHECK 2 EACH 1INCH CRACKS WERE FOUND ON FLOORBEAM STRUCTURE AT AFT END OF AILERON TOWER SHAFT QUADRANT CUTOUT BS 676, LBL 24.5. MAINTENANCE REMOVED ANGLE AND STIFFENER AT BS 676, RBL 24.5; FABRICATED DOUBLERS; INSTALLED REPAIR
- [SDR AWXA200300647](https://openairdocs.org/sdr/AWXA200300647.md): Floorbeam · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-15 CHECK 2 EACH 1 INCH CRACKS WERE FOUND ON FLOOR BEAM UPPER STRUCTURE AT AFT END OF AILERON QUADRANT CUTOUT BS 676, RBL 24.5. MAINTENANCE CUTOUT DAMAGE ON FLOORBEAM UPPER STRUCTURE BS 676, RBL 24.5; FABRICATED 3 EACH DOUBLERS; INSTALLED REPAIR PART
- [SDR AWXA200300646](https://openairdocs.org/sdr/AWXA200300646.md): Frame · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, Frame
  > DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON MAIN WHEEL WELL UPPER COMPRESSION FRAME AT BS 663, RBL 24.5. MAINTENANCE REMOVED VERTICAL STIFFENER, WEB DOUBLER, VERTICAL ANGLE, AND FORWARD AND AFT STIFFENER BRACKETS TO FACILITATE REPAIR; CUT AND TRIMMED DAMAGE
- [SDR AWXA200300645](https://openairdocs.org/sdr/AWXA200300645.md): Panel · delaminated · May 13, 2003 · N178AW · Boeing 737277 · Spoilers
  > DURING C-15 CHECK THE NO. 5 SPOILER WAS FOUND DELAMINATED AT THE INBOARD AFT EDGE. MAINTENANCE REMOVED AND REPLACED THE NO.5 SPOILER PANEL IAW BMM 27-62-12, PG. 401.
- [SDR AWXA200300644](https://openairdocs.org/sdr/AWXA200300644.md): Web · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-15 CHECK A.7500 INCH CRACK WAS FOUND ON FUSELAGE INTERIOR SHEAR WEB BELOW THE RT EMERGENCY ESCAPE HATCH CUTOUT. MAINTENANCE REMOVED DAMAGED SHEAR WEB BELOW THE RT EMERGENCY ESCAPE HATCH CUTOUT BS 616 TO BS 639, STR 27 RT; FABRICATED A NEW REPLACEMENT
- [SDR AWXA200300643](https://openairdocs.org/sdr/AWXA200300643.md): Frame · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, Frame
  > DURING C-15 CHECK A.5000 INCH CRACK WAS FOUND ON RADIUS OF SIDE FRAME AT BS 597, LBL 70. MAINTENANCE TRIMMED OUT DAMAGE AT BEND OF THE FLANGE ON SIDE FRAME AT BS 597, LBL 70; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR ANGLE AN
- [SDR AWXA200300642](https://openairdocs.org/sdr/AWXA200300642.md): Frame · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, Frame
  > YVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON MAIN WHEEL WELL COMPRESSION CHORD AT BS 663, LBL 24.5. MAINTENANCE REMOVED WEB STIFFENER, FLOOR BEAM FITTING, AND 2 EACH ANGLE STIFFENERS TO FACILITATE REPAIR; REMOVED DAMAGED PORTION OF UPPE
- [SDR AWXA200300634](https://openairdocs.org/sdr/AWXA200300634.md): Panel · delaminated · May 13, 2003 · N178AW · Boeing 737277 · Spoilers
  > YVR - FLIGHT CONTROL - DURING C-15 CHECK THE NO. 8 SPOILER WAS FOUND DELAMINATED AT THE MID CENTER AFT EDGE. MAINTENANCE REMOVED AND REPLACED THE NR 8 SPOILER PANEL IAW BMM 27-62-91, PG. 401.
- [SDR AWXA200300633](https://openairdocs.org/sdr/AWXA200300633.md): Skin · delaminated · May 13, 2003 · N178AW · Boeing 737277 · Leading Edge Devices
  > DURING C-15 CHECK THE NR 3 SLAT INBOARD END UPPER SKIN WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 3 SLAT IAW AWA T/C R3M27002.
- [SDR AWXA200300632](https://openairdocs.org/sdr/AWXA200300632.md): Slat · delaminated · May 13, 2003 · N178AW · Boeing 737277 · Leading Edge Devices
  > DURING C-15 CHECK THE NR 5 SLAT OUTBOARD TRAILING EDGE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 5 SLAT IAW AWA T/C R3M27008.
- [SDR AWXA200300630](https://openairdocs.org/sdr/AWXA200300630.md): Charger · inoperative · May 13, 2003 · N178AW · Boeing 737277 · Emergency Lighting
  > DURING C-15 CHECK EMERGENCY LIGHT BATTERY CHARGER M1051 LOCATED IN AFT AISLE CEILING HAS NO OUTPUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER M1051, OPERATIONAL CHECK WAS GOOD IAW AWA T/C A1C33005.
- [SDR AWXA200300609](https://openairdocs.org/sdr/AWXA200300609.md): Frame · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, Frame
  > YVR - MAJOR REPAIR - DURING C-15 CHECK A.25 INCH CRACK WAS FOUND ON LT FUSELAGE FRAME AT BS 639. MAINTENANCE REMOVED DAMAGED SECTION OF LT FUSELAGE FRAME AT BS 639; FABRICATED SPLICE REPAIR AND NEW SECTION PER S/B 737-53-1061, INSTALLED REPAIR PARTS IAW ER 1
- [SDR AWXA200300604](https://openairdocs.org/sdr/AWXA200300604.md): Web · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > YVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND AT RIVET HOLE ON INTERNAL FUSELAGE CENTER WEB BS 706, BL 0. MAINTENANCE REMOVED CRACKED AREA OF CENTER WEB BS 706, BL 0; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND FILLER PLATES; INSTALLED RE
- [SDR AWXA200300603](https://openairdocs.org/sdr/AWXA200300603.md): Angle · cracked · May 13, 2003 · N178AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND ON CENTER SECTION ANGLE BS 663, LBL 60. MAINTENANCE REMOVED CRACKED ANGLE AT BS 663, LBL 60; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-37422; INSTALLED REPAIR PART IAW B737-200 SRM 51-10-2, PG. 8.
- [SDR AWXA200300678](https://openairdocs.org/sdr/AWXA200300678.md): Web · cracked · May 7, 2003 · N178AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-15 CHECK A.5 INCH CRACK WAS FOUND ON SHEAR BEAM WEB OF STR 18A LT, AFT OF BS 706 FRAME TRUNNION BEAM SUPPORT FITTING IN FORWARD OUTBOARD CORNER. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED
- [SDR AWXA200300224](https://openairdocs.org/sdr/AWXA200300224.md): Battery Pack · discharged · Mar 1, 2003 · N178AW · Boeing 737277 · Emergency Lighting
  > DURING INSPECTION THE AFT LT ENTRY DOOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE AFT GALLEY EMERGENCY LIGHTS, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200300112](https://openairdocs.org/sdr/AWXA200300112.md): Cable · out of rig · Feb 9, 2003 · N178AW · Boeing 737277 · Landing Gear Position and Warning
  > ON DECENT INTO PHX EN ROUTE FROM AUS AFTER LOWERING LANDING GEAR RECEIVED UNSAFE LANDING GEAR INDICATION, 3 RED OVER 3 GREEN, DECLARED EMERGENCY, LANDED WITHOUT EVENT. MAINTENANCE LUBRICATED THE LANDING GEAR HANDLE AND ADJUSTED CABLE RIG FROM THE LANDING GEAR
- [SDR AWXA200300042](https://openairdocs.org/sdr/AWXA200300042.md): Battery Pack · discharged · Jan 15, 2003 · N178AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING INSPECTION THE VERTICAL EMERGENCY EXIT LIGHT AT THE L2 DOOR AND OVER WING EXIT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200201184](https://openairdocs.org/sdr/AWXA200201184.md): Battery Pack · discharged · Dec 11, 2002 · N178AW · Boeing 737277 · Emergency Lighting
  > DURING INSPECTION THE EMERGENCY EXIT LIGHTS AT LT OVERWING EXIT, L-2 DOOR, AND R-2 DOOR WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACK (M1051), OPERATIONAL TEST WAS GOOD.
- [SDR AWXA200201110](https://openairdocs.org/sdr/AWXA200201110.md): Battery · discharged · Nov 12, 2002 · N178AW · Boeing 737277 · Emergency Lighting
  > DURING INSPECTION THE R-2 DOOR WALL MOUNTED EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR WALL MOUNTED EMERGENCY EXIT SIGN BATTERY PACK, OPERATIONAL CHECK GOOD.
- [SDR AWXA200201109](https://openairdocs.org/sdr/AWXA200201109.md): Battery · discharged · Nov 12, 2002 · N178AW · Boeing 737277 · Emergency Lighting
  > DURING INSPECTION THE L-2 DOOR WALL MOUNTED EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR WALL MOUNTED EMERGENCY EXIT SIGN BATTERY PACK, OPERATIONAL CHECK GOOD.
- [SDR AWXA200201108](https://openairdocs.org/sdr/AWXA200201108.md): Battery · discharged · Nov 12, 2002 · N178AW · Boeing 737277 · Emergency Lighting
  > DURING INSPECTION THE LT EXIT ROW WALL MOUNTED EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EXIT ROW WALL MOUNTED EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK GOOD.
- [SDR AWXA200201058](https://openairdocs.org/sdr/AWXA200201058.md): Coalescer Bag · contaminated · Oct 29, 2002 · N178AW · Boeing 737277 · Humidity Control System
  > FLT 0221 - EN ROUTE FROM PHX TO AUS PASSENGER AT SEAT ROW 18 COMPLAINED OF NOXIOUS ODOR THAT CAUSED EYES TO IRRITATE. FLIGHT ATTENDANT ALSO SMELLED NOXIOUS ODOR FROM REAR OF CABIN TO SEAT ROW 6, ODOR EVEN CIRCULATED INTO THE FLIGHT DECK AREA, DIVERTED TO SAT A

Next page: https://openairdocs.org/deregistered/N178AW-2005-02-09/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N178AW' AND deregistration_id = 'N178AW-2005-02-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N178AW-2005-02-09/reports

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