# Service difficulty reports: N908AW, cancelled Jan 30, 2018

A list on [N908AW, cancelled Jan 30, 2018](https://openairdocs.org/deregistered/N908AW-2018-01-30.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 4 · 176 reports

- [SDR AALA201609029015](https://openairdocs.org/sdr/AALA201609029015.md): Slide · low pressure · Sep 1, 2016 · N908AW · Boeing 7572G7 · Escape Slide
  > AIRCRAFT WAS GROUNDED, R4 DOOR SLIDE BOTTLE PRESSURE LOW. REPLACED R4 DOOR SLIDE TASK CARD 19L80025002.
- [SDR AALA201606289003](https://openairdocs.org/sdr/AALA201606289003.md): Control Valve · defective · Jun 27, 2016 · N908AW · Boeing 7572G7 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A RT ENGINE BLEED OFF EICAS MESSAGE AND A RT ENGINE BLEED EICAS MESSAGE DURING TAKEOFF ROLL AND ABORTED THE TAKEOFF AT 60 KNOTS. MAINTENANCE REPLACED FLOW CONTROL VALVE IAW AMM 21-51-01-201. ALSO, REPLACED COMPRES
- [SDR AALA201604289010](https://openairdocs.org/sdr/AALA201604289010.md): Flashlight · inoperative · Apr 27, 2016 · N908AW · Boeing 7572G7 · Emergency Equipment
  > AIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANTS FLASHLIGHT AT 1L DOOR INOPERATIVE. REPLACED FLASHLIGHT & ACCOMPLISHED AS SATISFACTORY OPERATIONAL CHECK IAW AMM 25-60-00.
- [SDR AALA201604199008](https://openairdocs.org/sdr/AALA201604199008.md): Eec · defective · Apr 18, 2016 · N908AW · Boeing 7572G7 · Fuel Control/Turbine Engines
  > AIRCRAFT WAS GNDED. RT ENG SLOW TO ACCELERATE TO TAKEOFF POWER. TARGET EPR 1071 RT ENG STOPPED ACCELERATING AT 1.65 EPR. MANUALLY SET 1.71 EPR. REPLACED THE RT EEC & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 73-21-07.
- [SDR AALA201603219002](https://openairdocs.org/sdr/AALA201603219002.md): Control Lever · defective · Mar 17, 2016 · N908AW · Boeing 7572G7 · Landing Gear Selector
  > AIRCRAFT WAS GNDED. DURING THE APPROACH, THE GEAR DISAGREE LIGHT ILLUMINATED & THE CREW PERFORMED A GO AROUND & ACCOMPLISHED THE QRH CHECKLIST. THE ACFT LANDED SAFELY & NO FURTHER INCIDENTS WERE REPORTED. REPLACED THE LG CONTROL LEVER MODULE & ACCOMPLISHED
- [SDR AALA201512189003](https://openairdocs.org/sdr/AALA201512189003.md): Warning Light · false activation · Dec 17, 2015 · N908AW · Boeing 7572G7 · Landing Gear Position and Warning
  > GEAR DISAGREE MESSAGE & FWD LIGHT APPEARED DURING GEAR EXTENSION. ABORTED APPROACH. RETRACTED GEAR, DURING GO AROUND MSG WENT OUT & DID NOT REAPPEAR. PREFORMED BITE TEST ON PSEU IAW AMM 32-09-03-815-804 WITH NO FAULTS OR DISCREPANCIES NOTED. ACFT GOOD FOR
- [SDR AALA201511239006](https://openairdocs.org/sdr/AALA201511239006.md): Battery · discharged · Nov 20, 2015 · N908AW · Boeing 7572G7 · Emergency Equipment
  > FLASHLIGHT AT L2 DOOR INOPERATIVE, NO FLASHING RED INDICATOR. REPLACED FLASHLIGHT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA201509309011](https://openairdocs.org/sdr/AALA201509309011.md): Wire · broken · Sep 28, 2015 · N908AW · Boeing 7572G7 · Light System Wiring
  > FLIGHT 583 SEAT MOUNTED EMER LIGHT INOPERATIVE AT SEAT 19C. FOUND WIRE BROKEN. R & R SEAT MOUNTED EMER LIGHT ASSEMBLY AT SEAT 19C. OPERATIONAL CHECKED GOOD.
- [SDR AALA201508149001](https://openairdocs.org/sdr/AALA201508149001.md): Flashlight · inoperative · Aug 13, 2015 · N908AW · Boeing 7572G7 · Emergency Equipment
  > AFT GALLEY FLIGHT ATTENDANT EMER FLASHLIGHT NO LED FLASH. REPLACED FLASHLIGHT.
- [SDR AALA201507069001](https://openairdocs.org/sdr/AALA201507069001.md): Latch · out of adjust · Jul 3, 2015 · N908AW · Boeing 7572G7 · Passenger Oxygen System
  > FORWARD LAVATORY O2 DOOR LATCH ACTUATOR FAILED TEST, COULD NOT RESET. ADJUSTED LATCH MECHANISM AS REQUIRED. OPERATIONS OK.
- [SDR AALA201506059009](https://openairdocs.org/sdr/AALA201506059009.md): Pin · worn · Jun 2, 2015 · N908AW · Boeing 7572G7 · Nose/Tail Landing Gear Attach Section
  > NOSE LANDING GEAR RT TRUNNION PIN WORN. REPLACED TRUNNION PIN.
- [SDR AALA201506059008](https://openairdocs.org/sdr/AALA201506059008.md): Pin · worn · Jun 2, 2015 · N908AW · Boeing 7572G7 · Nose/Tail Landing Gear Attach Section
  > NOSE LANDING GEAR LT TRUNNION PIN WORN. REPLACED TRUNNION PIN.
- [SDR AALA201505229005](https://openairdocs.org/sdr/AALA201505229005.md): Module · faulty · May 21, 2015 · N908AW · Boeing 7572G7 · Landing Gear Position and Warning
  > FLIGHT 663 EN-ROUTE, EICAS MSG & AUDIO ALARM. GEAR NOT DOWN RED CONFIGURATION LIGHT, RED WARNING LIGHT ON GLARE SHIELD. GEAR HANDLE UP & OFF, NO CHANGE. PRESSED GND PROX & CONFIG GEAR OVERRIDE TO TURN OFF AUDIO WARNING ALARM. THE FLIGHT LANDED WITHOUT FURT
- [SDR AALA201504209016](https://openairdocs.org/sdr/AALA201504209016.md): Shear Tie · cracked · Apr 10, 2015 · N908AW · Boeing 7572G7 · Fuselage Internal Mounting Structure
  > C4 CHECK, L4 DOOR FUSELAGE UPPER LOBE INTERIOR FRAME & SKIN SHEAR TIE HAS 0.5 INCH CRACK NEXT TO RADIUS AT STATION 1661 BETWEEN STRINGER 5L & 6L. R & R SHEAR TIE IAW SRM 51-40-02 & DWG 146N1024.
- [SDR AALA201504209015](https://openairdocs.org/sdr/AALA201504209015.md): Stringer · cracked · Apr 10, 2015 · N908AW · Boeing 7572G7 · Fuselage Main, Longeron/Stringer
  > C4 CHECK, STRINGER AT STRINGER 13R CRACKED AT BS 619. REPAIRED CRACKED STRINGER IAW EA 250005.
- [SDR AALA201505049005](https://openairdocs.org/sdr/AALA201505049005.md): Intercostal · cracked · Apr 8, 2015 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > C4 CHECK, CRACK IN INTERCOSTAL BETWEEN STATION 680 & 685 BELOW STRINGER 11L, FWD OF L2 DOOR IN RADIUS NEXT TO SKIN. R & R CRACKED INTERCOSTAL IAW SRM 51-10-02 & DWG N8338.
- [SDR AALA201505049004](https://openairdocs.org/sdr/AALA201505049004.md): Support Angle · cracked · Apr 5, 2015 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > C4 CHECK, FLOORBOARD SUPPORT ANGLE CRACKED BETWEEN STATION 780 & 800 AT BL 0. FABRICATED & INSTALLED NEW ANGLE IAW DWG 143N5140.040 7075 T6 FROM BAC1493-412.
- [SDR AALA201504209014](https://openairdocs.org/sdr/AALA201504209014.md): Channel · corroded · Apr 4, 2015 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > C4 CHECK, CORROSION ON GALLEY AREA FLOOR STRUCTURE AT STATION 398, RBL 20. R & R CHANNEL IAW DWG 141N5186 & SRM 51-10-02 51-40-02.
- [SDR AALA201504209013](https://openairdocs.org/sdr/AALA201504209013.md): Support Fitting · corroded · Apr 4, 2015 · N908AW · Boeing 7572G7 · Fuselage Main, Attach Fittings
  > C4 CHECK, CORROSION ON GALLEY SUPPORT FITTING AT STATION 398, RBL 14. R & R SUPPORT FITTING IAW DWG 141N5186 & SRM 51-10-02 51-40-02.
- [SDR AALA201505079001](https://openairdocs.org/sdr/AALA201505079001.md): Keelbeam · corroded · Apr 3, 2015 · N908AW · Boeing 7572G7 · Fuselage Main, Keel
  > C4 CHECK, CORROSION ON INNER ATTACH FLANGE OF KEEL BEAM IN RT WW AT APPROX STATION 1120 & RBL 10. REPAIRED IAW EA 106566.
- [SDR AALA201504209017](https://openairdocs.org/sdr/AALA201504209017.md): Floorbeam · corroded · Mar 28, 2015 · N908AW · Boeing 7572G7 · Fuselage Main, Floor Beam
  > C4 CHECK, CORROSION ON FLOORBEAM T CAP AT BS 365 & RBL 45.5. REPAIRED FLOORBEAM T CAP IAW SRM 53-00-51-2R PROCEDURE 10.
- [SDR AALA201505049003](https://openairdocs.org/sdr/AALA201505049003.md): Frame · cracked · Mar 26, 2015 · N908AW · Boeing 7572G7 · Fuselage Main, Frame
  > C4 CHECK, CRACK FOUND ON FRAME AT BS 1400, LT STRINGER 24. REMOVED DAMAGED AREAS OF FRAME. FABRICATED REPAIR SECTION OF FRAME & TWO DOUBLERS. INSTALLED REPAIR & FASTENERS IAW EA 250014.
- [SDR USAA2014121200002](https://openairdocs.org/sdr/USAA2014121200002.md): Slide · unserviceable · Dec 10, 2014 · N908AW · Boeing 7572G7 · Escape Slide
  > R4 DOOR SLIDE OUT OF GREEN BAND. R & R R4 DOOR EVACUATION SLIDE. REPAIRED SLIDE. UNIT WAS PARTIALLY DISASSEMBLED, CLEANED & INSPECTED, REPLACING ALL PARTS NECESSARY FOR REPAIR. PASSED LIGHT SYS TEST & HEIGHT CHECK. OVERHAULED & CHARGED RESERVOIR & VLV ASSE
- [SDR USAA2014120100015](https://openairdocs.org/sdr/USAA2014120100015.md): Window · delaminated · Nov 30, 2014 · N908AW · Boeing 7572G7 · Flight Compartment Windows
  > RON REPLACE THE CAPTAINS NR 3 WINDOW FOR DELAMINATION. R & R CAPTAINS NR 3 WINDOW IAW AMM 56-11-10-424-015. PERFORMED WINDOW HEAT TEST IAW AMM 30-11-00-715-001.
- [SDR USAA2014072200004](https://openairdocs.org/sdr/USAA2014072200004.md): Coffeemaker · faulty · Jul 21, 2014 · N908AW · Boeing 7572G7 · Buffet/Galleys
  > AFT GALLEY COFFEE MAKERS REPORTED TO HAVE ELEC SMOKE SMELL WHEN TURNED ON, REMAINED OFF DURING FLIGHT. COULD NOT DISTINGUISH WHICH POSITION ON BOTH. REPLACED ALL COFFEE MAKERS IN AFT GALLEY. OPERATIONS CHECKED NORMAL.
- [SDR USAA2014051200031](https://openairdocs.org/sdr/USAA2014051200031.md): Access Door · missing · May 9, 2014 · N908AW · Boeing 7572G7 · Engine Cowling System
  > FLT 693 NR 1 ENG OIL SERVICE DOOR MISSING AFTER FLIGHT. REPLACED NR 1 ENG OIL SERVICE DOOR IAW SRM 51-40-02. OK FOR SERVICE.
- [SDR USAA2014080100011](https://openairdocs.org/sdr/USAA2014080100011.md): Door · missing · May 6, 2014 · N908AW · Boeing 7572G7 · Engine Cowling System
  > OIL FILL DOOR MISSING NR 1 ENG AFTER FLIGHT. REPLACED NR 1 ENG OIL SERVICE DOOR IAW SRM 51-40-02. OK FOR SERVICE.
- [SDR USAA2014020700003](https://openairdocs.org/sdr/USAA2014020700003.md): Skin Panel · delaminated · Jan 29, 2014 · N908AW · Boeing 7572G7 · Horizontal Stabilizer, Plate/Skin
  > C1 CHECK DELAMINATION ON LT HORIZONTAL SKIN UPPER SURFACE INBD PANEL AT STAB STATION 224.249 APPROXIMATELY 6 INCHES FROM LE. REPLACED LT HORIZONTAL UPPER INBD PANEL IAW SRM 51-40-02, EA 105500 & EA 105582.
- [SDR USAA2013050200004](https://openairdocs.org/sdr/USAA2013050200004.md): Wire Harness · disconnected · May 1, 2013 · N908AW · Boeing 7572G7 · Light System Wiring
  > PHX - SEAT ROW 35 C EMERGENCY SEAT LIGHTS INOP. RELAMPED, NO HELP. CHANGED LIGHT ASSY, NO HELP. CONNECTED SEAT HARNESS, OPS CHECK GOOD.
- [SDR USAA2012091900011](https://openairdocs.org/sdr/USAA2012091900011.md): Door Frame · cracked · Sep 4, 2012 · N908AW · Boeing 7572G7 · Passenger/Crew Doors
  > C2 CHECK - CRACK ON L2 UPPER HINGE CUTOUT AT FORWARD DOOR FRAME. REPAIRED L2 UPPER HINGE CUTOUT AT FORWARD DOOR FRAME IAW B757 SRM 52-10-02-2R-1.
- [SDR USAA2012090700014](https://openairdocs.org/sdr/USAA2012090700014.md): Skin · debonded · Aug 30, 2012 · N908AW · Boeing 7572G7 · Leading Edge Devices
  > C2 CHECK - DISBONDING ON UPPER TRAILING EDGE SURFACE OF NR 3 SLAT AT INBOARD CORNER. REPAIRED NR 3 SLAT UPPER SURFACE IAW B757 SRM 51-70-10 & TYPICAL REPAIR TR-757-5130-10-0058.
- [SDR USAA2012052500022](https://openairdocs.org/sdr/USAA2012052500022.md): Attach Fitting · severed · May 23, 2012 · N908AW · Boeing 7572G7 · Nacelle/Pylon, Attach Fittings
  > PYLON FITTING INSPECTION - NR 1 ENGINE INBOARD C DUCT AFT MOUNT PYLON ATTACH FITTING CENTER LUG UPPER MATERIAL SEVERED. REPLACED NR 1 ENGINE INBOARD C DUCT AFT MOUNT PYLON ATTACH FITTING AT PP STA 174.30 IAW EA 202636, EA 202610A AND EO 5408R114.
- [SDR USAA2012031600013](https://openairdocs.org/sdr/USAA2012031600013.md): Lock Pin · worn · Mar 15, 2012 · N908AW · Boeing 7572G7 · Flight Compartment Equipment
  > FLT 23. F/O SEAT LATERAL ADJUSTMENT LOCKING MECHANISM NOT LOCKING PROPERLY SEAT UNLOCKED AND SLID AFT DURING CLIMB. REMOVED AND REPLACED SEAT. SHOP FOUND GUIDE STRAP WORN, HARDWARE WORN/MISSING, LABELS MISSING, ARMREST PADS TORN, END PLUGS WORN, GROMMETS MI
- [SDR USAA2012030500001](https://openairdocs.org/sdr/USAA2012030500001.md): Hinge Fitting · cracked · Mar 1, 2012 · N908AW · Boeing 7572G7 · Nacelle/Pylon, Attach Fittings
  > PHX VISUAL - NR 2 ENGINE OUTBOARD `C` DUCT AFT MOUNT PYLON ATTACH FITTING, CENTER LUG CRACKED APPROX 1 INCH. REPLACED NR 2 ENGINE OUTBOARD THRUST REVERSER AFT HINGE FITTING IAW EA 201955 & EO 5408R114.
- [SDR USAA20110616BB054](https://openairdocs.org/sdr/USAA20110616BB054.md): Wire Harness · faulty · Jun 15, 2011 · N908AW · Boeing 7572G7 · Light System Wiring
  > PHX - AISLE SEAT 8L EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE HARNESS ON ROW 8L EMERGENCY LIGHTS. OPS CHECK GOOD.
- [SDR USAA20110301BB013](https://openairdocs.org/sdr/USAA20110301BB013.md): Bottle · low pressure · Feb 25, 2011 · N908AW · Boeing 7572G7 · Passenger/Crew Doors
  > PHX - THE L4 DOOR ASSIST BOTTLE READS LOW ON PRESSURE. MAINTENANCE REMOVED AND REPLACED THE L4 DOOR ASSIST BOTTLE.
- [SDR USAA20101215BB090](https://openairdocs.org/sdr/USAA20101215BB090.md): Bearing · failed · Dec 12, 2010 · N908AW · Boeing 7572G7 · Turbine Engine Accessory Drive
  > SAT EN-ROUTE CUN TO PHX. ABOUT 20 MINUTES FROM SAT, IT WAS DETERMINED THAT THE LEFT ENGINE OIL QUANTITY AND PRESSURE WERE DROPPING. THE CAPTAIN SHUT DOWN THE LEFT ENGINE AND DIVERTED TO SAT. SINGLE ENGINE TIME WAS APPROXIMATELY 20 MINUTES. THE FLIGHT LAND
- [SDR USAA20100920BB056](https://openairdocs.org/sdr/USAA20100920BB056.md): Bearing · smoke · Sep 17, 2010 · N908AW · Boeing 7572G7 · Air Distribution System
  > FLT 432, WHILE IN CRUISE FLIGHT, EXPERIENCED SMOKE IN THE COCKPIT AND CABIN. THE COCKPIT CREW SELECTED LEFT BLEED WITH PACK OFF, WHICH RESULTED IN SMOKE REDUCTION. THE FLIGHT DIVERTED TO SFO. AFTER LANDING, THE LT ENGINE OIL QUANTITY WENT TO ZERO WHILE ALL
- [SDR USAA20100723BB043](https://openairdocs.org/sdr/USAA20100723BB043.md): Fan · faulty · Jul 20, 2010 · N908AW · Boeing 7572G7 · Air Distribution Fan
  > PHX FLT 23 EN ROUTE HNL TO PHX. AN UNUSUAL ODOR COMING FROM THE GASPER VENTS OVER ROW 19, AIRCRAFT LEFT, WAS NOTICED. THE ODOR WAS DESCRIBED AS SIMILAR TO BURNING RUBBER, OR OIL ODOR. SMELL STOPS WITH THE GASPER VENT CLOSED. NO SMOKE OR HOT FLOOR, SIDEWA
- [SDR USAA2010030390482](https://openairdocs.org/sdr/USAA2010030390482.md): Slat · corroded · Mar 1, 2010 · N908AW · Boeing 7572G7 · Leading Edge Devices
  > PHX - A-CHECK - MAJOR REPAIR - CORROSION ON NR 2 SLAT AT WS 594. REPAIR COMPLETED.
- [SDR USAA20091006BB142](https://openairdocs.org/sdr/USAA20091006BB142.md): Air Filter · dirty · Oct 3, 2009 · N908AW · Boeing 7572G7 · Air Distribution System
  > PHX FLT 9254 MCN TO PHX. DURING DESCENT, ODOR IN CABIN/FLT DECK. ODOR CLEARED WHEN POWER ABOVE IDLE THRUST, NOT BELIEVED TO BE ELECTRICAL OR PETROLEUM. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RECIRCULATION FILTERS.
- [SDR USAA2009100192683](https://openairdocs.org/sdr/USAA2009100192683.md): Skin · cracked · Sep 30, 2009 · N908AW · Boeing 7572G7 · Nacelle/Pylon, Plate/Skin
  > MCN - C4 - MAJOR REPAIR - CRACK AT NR 1 PYLON OUTBOARD THRUST REVERSER AFT MOUNT FITTING UPPER AFT FASTENER HOLE AT 12:30 POSITION ON PYLON ALUMINUM OUTER SKIN ONLY. REPAIRED NR 1 PYLON OUTBOARD THRUST REVERSER AFT MOUNT FITTING SKIN IAW EA 130334.
- [SDR USAA2009100192682](https://openairdocs.org/sdr/USAA2009100192682.md): Skin · cracked · Sep 30, 2009 · N908AW · Boeing 7572G7 · Nacelle/Pylon, Plate/Skin
  > MCN - C4 - MAJOR REPAIR - CRACK AT NR 1 PYLON INBOARD THRUST REVERSER AFT MOUNT FITTING UPPER AFT FASTENER HOLE AT 12:30 POSITION ON PYLON ALUMINUM OUTER SKIN ONLY. REPAIRED NR 1 PYLON INBOARD THRUST REVERSER AFT MOUNT FITTING SKIN IAW EA 130334.
- [SDR USAA2009093092669](https://openairdocs.org/sdr/USAA2009093092669.md): Fuse · blown · Sep 29, 2009 · N908AW · Boeing 7572G7 · Emergency Lighting
  > MCN - C4 - EEL - BULLNOSE EMERGENCY LIGHT NOT FUNCTIONING AT ROWS 5L, 17L, 30L, 22R & 18R. REPLACED EMERGENCY POWER SUPPLY FUSE, BULLNOSE EMERGENCY LIGHT ROWS 5L, 17L, 30L, 22R & 18R. OPS CHECK GOOD IAW B757 AMM 33-51-05-2.
- [SDR USAA2009093092668](https://openairdocs.org/sdr/USAA2009093092668.md): Pin · not seated · Sep 29, 2009 · N908AW · Boeing 7572G7 · Light System Wiring
  > MCN - C4 - EEL - EMERGENCY ESCAPE PATH LIGHTS AND EMERGENCY EXIT IDENTIFIER LIGHT QUIT WORKING. RESEATED PIN ON CONNECTOR ON LEFT EMERGENCY EXIT SIGN, OPS CHECKED GOOD IAW B757 AMM 33-51-11-3.
- [SDR USAA2009092892656](https://openairdocs.org/sdr/USAA2009092892656.md): Socket · damaged · Sep 29, 2009 · N908AW · Boeing 7572G7 · Light System Wiring
  > MCN - C4 - EEL - EMERGENCY EXTERIOR DOOR LIGHT NOT ILLUMINATING AT THE R-3 & L-2 DOORS. REPLACED SOCKETS IN D74 PIN 9 & D72 PIN9 IAW BSWPM 20-60-02, OPS CHECK GOOD.
- [SDR USAA2009092292584](https://openairdocs.org/sdr/USAA2009092292584.md): Structure · cracked · Sep 19, 2009 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > MCN - C4 - MAJOR REPAIR - CRACK ON CHORD BETWEEN BS 1480 TO BS 1500. REPLACED CHORD BETWEEN BS 1480 TO BS 1500 IAW B757 SRM 51-40-02 & BOEING DRAWING 146N5448.
- [SDR USAA2009092592627](https://openairdocs.org/sdr/USAA2009092592627.md): Intercostal · corroded · Sep 11, 2009 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL UPPER CHORD BETWEEN BS1360, WL514, RBL20. REPLACED INTERCOSTAL UPPER CHORD BETWEEN BS1360 TO BS1380, WL514, RBL20 IAW SRM 51-40-02. (K)
- [SDR USAA2009092592628](https://openairdocs.org/sdr/USAA2009092592628.md): Shear Tie · corroded · Sep 11, 2009 · N908AW · Boeing 7572G7 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS1380, WL145, RBL20. REPLACED SHEAR TIE AT BS 1380, WL145, RBL20 IAW SRM 51-40-02 AND DWG 146N5421. (K)
- [SDR USAA2009092192568](https://openairdocs.org/sdr/USAA2009092192568.md): Fitting · corroded · Sep 11, 2009 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > MCN - C4 - MAJOR REPAIR - CORROSION ON CLIP AT BS 1380, RBL 20. REPLACED CLIP AT BS 1380, RBL 20 IAW B757 SRM 51-40-05 & 53-00-53.

Next page: https://openairdocs.org/deregistered/N908AW-2018-01-30/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 = 'N908AW' AND deregistration_id = 'N908AW-2018-01-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N908AW-2018-01-30/reports

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