# Service difficulty reports: N905AW, cancelled Jul 12, 2016

A list on [N905AW, cancelled Jul 12, 2016](https://openairdocs.org/deregistered/N905AW-2016-07-12.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 · 180 reports

- [SDR AALA201511199003](https://openairdocs.org/sdr/AALA201511199003.md): D-Ring · out of position · Nov 18, 2015 · N905AW · Boeing 7572S7 · Escape Slide
  > L1 DOOR SLIDE D RING NOT VISIBLE. FOUND L1 DOOR MANUAL RELEASE D RING UNDER BUSSEL. MOUNTED OUTSIDE FRONT LOWER PART OF BUSSEL SO IT'S VISIBLE.
- [SDR USAA2015021900011](https://openairdocs.org/sdr/USAA2015021900011.md): Megaphone · unserviceable · Feb 18, 2015 · N905AW · Boeing 7572S7 · Emergency Equipment
  > TWO MEGA PHONES NEED REPLACED ABOVE ROWS 1L & 34L. REPLACED 2 MEGA PHONES WITH NEW MEGA PHONES.
- [SDR USAA2015012800005](https://openairdocs.org/sdr/USAA2015012800005.md): Sliding Window · unsecure · Jan 27, 2015 · N905AW · Boeing 7572S7 · Flight Compartment Windows
  > EN-ROUTE, FIRST OFFICER`S SLIDING WINDOW OPENED ON TAKEOFF ROLL ABOVE 80 KTS, BELOW V1. PERFORMED AN OPERATIONAL TEST ON THE FIRST OFFICER`S NR 2 WINDOW. OPERATIONAL TEST CHECKED GOOD.
- [SDR USAA2014080600017](https://openairdocs.org/sdr/USAA2014080600017.md): Intercostal · cracked · Aug 5, 2014 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > WEEKLY VISIT 6 INCH CRACK ON INTERCOSTAL AT BS 1440, STRINGER 24R. REPLACED INTERCOSTAL IAW SRM 51-40-02 & DWG 146N8545.
- [SDR USAA2014030300007](https://openairdocs.org/sdr/USAA2014030300007.md): Angle · cracked · Feb 26, 2014 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C3 CHECK 2 INCH CRACK IN INTERCOSTAL CHORD ANGLE AT BS 1671, WL 208 & BL 0. REPLACED INTERCOSTAL CHORD ANGLE AT BS 1671, WL 208 & BL0 IAW SRM 51-10-02 & DWG 146N5180.
- [SDR USAA2014030600006](https://openairdocs.org/sdr/USAA2014030600006.md): Strap · cracked · Feb 20, 2014 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C3 CHECK, 1 INCH CRACK ON STABILIZATION STRAP AT BS 1380, RBL 45. REPAIRED STABILIZATION STRAP AT BS 1380, RBL 45 IAW SRM 53-00-51-2R-12.
- [SDR USAA2014030600011](https://openairdocs.org/sdr/USAA2014030600011.md): Stringer · corroded · Feb 16, 2014 · N905AW · Boeing 7572S7 · Fuselage Main, Longeron/Stringer
  > C3 CHECK, LEVEL 2 CORROSION ON STRINGER BETWEEN BS 1408 TO S1420, S29R. REPAIRED STRINGER BETWEEN BS 1408 TO S1420, S29R IAW EA 105708.
- [SDR USAA2013111500002](https://openairdocs.org/sdr/USAA2013111500002.md): Bearing · failed · Nov 11, 2013 · N905AW · Boeing 7572S7 · Wheel/Ski/Float
  > DURING LANDING ROLL OUT, CREW FELT A VIBRATION IN THE NOSE GEAR SIMILAR TO A FLAT TIRE. MAINTENANCE INSPECTED ACFT AND FOUND THE RT NLG WHEEL ASSY BEARING ON AXLE NUT SIDE OF THE WHEEL ASSY HAD FAILED. A TEMPORARY RT NLG WHEEL ASSY WAS INSTALLED. FURTHER
- [SDR USAA2013060700001](https://openairdocs.org/sdr/USAA2013060700001.md): Power Supply · inoperative · Jun 4, 2013 · N905AW · Boeing 7572S7 · Emergency Lighting
  > EMER LIGHT IN FWD DOOR SURROUND LIGHT L7 AND R4 INOP. R & R AFT LT POWER SUPPLY M736.
- [SDR USAA2012120500002](https://openairdocs.org/sdr/USAA2012120500002.md): Fuse · blown · Dec 4, 2012 · N905AW · Boeing 7572S7 · Emergency Lighting
  > PHX - LOWER EXIT SIGN AT 1L AND R1 DOOR INOP. REMOVED AND REPLACED BAD FUSE ON POWER SUPPLY/BATTERY PACK FOR LOWER EMERGENCY SIGNS 1L 1R.
- [SDR USAA2012102300004](https://openairdocs.org/sdr/USAA2012102300004.md): Panel · delaminated · Oct 19, 2012 · N905AW · Boeing 7572S7 · Vertical Stabilizer Miscellaneous Structure
  > C2 CHECK - AREA OF DELAMINATION ON LEFT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL AT FSS 220. REPLACED LEFT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL AT FSS 220 IAW B757 SRM 55-30-01 & 51-70-10.
- [SDR USAA2012101800009](https://openairdocs.org/sdr/USAA2012101800009.md): Skin Panel · delaminated · Oct 18, 2012 · N905AW · Boeing 7572S7 · Horizontal Stabilizer, Plate/Skin
  > C2 CHECK - DELAMINATION ON RIGHT STABILIZER TORQUE BOX, UPPER SKIN PANEL, INNER SKIN AT STAB STA 130 APPROX 10 INCHES AFT OF AUXILLARY SPAR. REPAIRED RIGHT STABILIZER TORQUE BOX, UPPER SKIN PANEL IAW B737 SRM 51-40-03 & EA 502286.
- [SDR USAA2012101500020](https://openairdocs.org/sdr/USAA2012101500020.md): Web · cracked · Oct 13, 2012 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C2 CHECK - CRACK AT L2 DOOR CUTOUT WEB PANEL AT BS 686 APPROX 1 INCH ABOVE S13L. REPAIRED L2 DOOR CUTOUT WEB PANEL AT BS 686 APPROX 1 INCH ABOVE S13L IAW # 104310.
- [SDR USAA2012071300001](https://openairdocs.org/sdr/USAA2012071300001.md): Battery · discharged · Jul 11, 2012 · N905AW · Boeing 7572S7 · Emergency Equipment
  > PHX - FWD F/A FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPS CHECK GOOD.
- [SDR USAA2012062500015](https://openairdocs.org/sdr/USAA2012062500015.md): Skin · delaminated · Jun 22, 2012 · N905AW · Boeing 7572S7 · Leading Edge Devices
  > WEEKLY CHECK - DELAMINATION ON NR 7 SLAT ON UPPER SURFACE AT INBOARD END AT WS 397. REPLACED NR 7 SLAT IAW JOB CARD 19L52027002.
- [SDR USAA2012052900039](https://openairdocs.org/sdr/USAA2012052900039.md): Bearing · worn · May 25, 2012 · N905AW · Boeing 7572S7 · Aileron Control System
  > PHX FLT 47 EN ROUTE LIH TO PHX. AILERONS STIFF- DO NOT RETURN TO CENTER. REMOVED AND REPLACED CENTERING BEARING ON LATERAL CONTROL FEEL AND TRIM MECHANISM ASSY. OP'S CHECKS GOOD. RIGGING NOT DISTURBED.
- [SDR USAA2011091500004](https://openairdocs.org/sdr/USAA2011091500004.md): Oven · inoperative · Sep 12, 2011 · N905AW · Boeing 7572S7 · Buffet/Galleys
  > OGG FLT 432 EN ROUTE PHX TO OGG. BOTH OVENS AT G1B FIRST CLASS GALLEY INOP. INTERMITTENT ON AND OFF WITH ACRID ELECTRICAL ODOR. REPLACED BOTH FWD GALLEY OVENS.
- [SDR USAA2011082600027](https://openairdocs.org/sdr/USAA2011082600027.md): Hub · loose · Aug 24, 2011 · N905AW · Boeing 7572S7 · Passenger/Crew Doors
  > PHX - THE L-4 DOOR INTERIOR OPEN/CLOSE HANDLE IS LOOSE. REMOVED AND REPLACED HANDLE HUB.
- [SDR USAA2011072700003](https://openairdocs.org/sdr/USAA2011072700003.md): Lanyard · out of position · Jul 26, 2011 · N905AW · Boeing 7572S7 · Escape Slide
  > PHX - DOOR 1R VERY DIFFICULT TO ARM AND DOES NOT APPEAR NORMAL WHEN FORCED TO ARM. REF PRIOR ENTRY LOG PAGE 7583660. MAINTENANCE FOUND LANYARD FROM SLIDE IMPEDING GIRT BAR. STOWED LANYARD INTO SLIDE, VERIFIED GIRT BAR ENGAGES BRACKETS FULLY, OP NORMAL.
- [SDR USAA2011072700002](https://openairdocs.org/sdr/USAA2011072700002.md): Smoke Detector · inoperative · Jul 26, 2011 · N905AW · Boeing 7572S7 · Smoke Detection
  > PHX - SMOKE DET INOP LAV MID RT. MAINTENANCE REMOVED AND REPLACED RT MID LAV SMOKE DETECTOR TR26-005AW, NO FAULTS NOTED ON GROUND AT THIS TIME.
- [SDR USAA2011032191155](https://openairdocs.org/sdr/USAA2011032191155.md): Pin · backed out · Mar 13, 2011 · N905AW · Boeing 7572S7 · Light System Wiring
  > MCN - C1 - EEL - LOWER LEFT EMERGENCY LIGHT NEXT TO L-3 DOOR SAYING "EXIT" IS INOP. RESEATED PUSHED BACK PIN ON LOWER LEFT EMERGENCY LIGHT NEXT TO L-3 DOOR SAYING "EXIT" AS REQUIRED. OPS CHECK GOOD.
- [SDR USAA2011031691064](https://openairdocs.org/sdr/USAA2011031691064.md): Battery · weak · Mar 11, 2011 · N905AW · Boeing 7572S7 · Emergency Equipment
  > MCN - C1 - EEL - L-2 DOOR FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY IS WEAK. REPLACED L-2 DOOR FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY AS NEEDED. OPS CHECK GOOD.
- [SDR USAA2011031591061](https://openairdocs.org/sdr/USAA2011031591061.md): Fitting · cracked · Mar 5, 2011 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > MCN - C1 - MAJOR REPAIR - CRACK ON CLIP AT BS 865, BL 0. REPLACED CLIP AT BS 865, BL 0 IAW B757 SRM 51-40-02.
- [SDR USAA2011030991008](https://openairdocs.org/sdr/USAA2011030991008.md): Panel · cracked · Feb 24, 2011 · N905AW · Boeing 7572S7 · Leading Edge Devices
  > MCN - C1 - MAJOR REPAIR - CRACK ON LEFT WING NR 2 SLAT COVE PANEL AT WS 580. REPLACED LEFT WING NR 2 SLAT COVE PANEL AT WS 580 IAW B757 SRM 51-40-02.
- [SDR USAA20100913BB054](https://openairdocs.org/sdr/USAA20100913BB054.md): Reservoir · low pressure · Sep 11, 2010 · N905AW · Boeing 7572S7 · Passenger/Crew Doors
  > THE L2 DOOR EMERGENCY POWER RESERVOIR HAS LOW PRESSURE. REMOVED AND REPLACED THE L2 DOOR EMERGENCY POWER RESERVOIR. ASSEMBLY WAS REPLACED WITH AN EQUIVALENT ASSEMBLY.
- [SDR USAA20100903BB053](https://openairdocs.org/sdr/USAA20100903BB053.md): Light · inoperative · Sep 2, 2010 · N905AW · Boeing 7572S7 · DME/TACAN System
  > LAX - EN ROUTE FROM PHX TO LAX, CREW REPORTED THE FIRST OFFICER'S VOR/DME SWITCH WAS INOPERATIVE. WHEN SWITCH WAS PUSHED, A POP WAS HEARD AND A SMELL OF FUMES WAS NOTED. MAINTENANCE FOUND DEFECTIVE LAMP IN SWITCH BUTTON. REPLACED LAMP. TEST/OPS CHECK GOOD.
- [SDR USAA20100305BB012](https://openairdocs.org/sdr/USAA20100305BB012.md): Light · inoperative · Mar 3, 2010 · N905AW · Boeing 7572S7 · Emergency Lighting
  > PHX - RED AISLE EMERGENCY EXIT LIGHT WAS INOPERATIVE AND MISSING AT SEAT 10C. REMOVED AND REPLACED RED AISLE EMERGENCY EXIT LIGHT ASSEMBLY.
- [SDR USAA20091116BB154](https://openairdocs.org/sdr/USAA20091116BB154.md): Socket · inoperative · Nov 12, 2009 · N905AW · Boeing 7572S7 · Emergency Lighting
  > PHX - THE 16ABC SEAT MOUNT EMERGENCY LIGHT INOP. MAINTENANCE REPLACED SOCKET ASSEMBLY.
- [SDR USAA2009111193084](https://openairdocs.org/sdr/USAA2009111193084.md): Slat · corroded · Nov 10, 2009 · N905AW · Boeing 7572S7 · Leading Edge Devices
  > BFM - C4 - MAJOR REPAIR - CORROSION AROUND FASTENERS ON NR 8 SLAT AT WS 509.50. REPLACED NR 8 SLAT AT WS 509.50 IAW B757 AMM 27-81-02.
- [SDR USAA2009111193083](https://openairdocs.org/sdr/USAA2009111193083.md): Sill · corroded · Nov 10, 2009 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON LOWER SILL & CHORD BETWEEN BS 1380 TO BS 1440, WL 145, RBL 20. REPLACED LOWER SILL & CHORD BETWEEN BS 1380 TO BS 1440, WL 145, RBL 20 IAW B757 SRM 51-40-02 & 51-20-01.
- [SDR USAA2009111093077](https://openairdocs.org/sdr/USAA2009111093077.md): Skin · corroded · Nov 9, 2009 · N905AW · Boeing 7572S7 · Fuselage Main, Plate/Skin
  > BFM - C4 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN AT BS 1525 BETWEEN S29L TO S30L. REPAIRED FUSELAGE SKIN AT BS 1525 BETWEEN S29L TO S30L IAW EA 134168.
- [SDR USAA2009111093076](https://openairdocs.org/sdr/USAA2009111093076.md): Skin · corroded · Nov 9, 2009 · N905AW · Boeing 7572S7 · Fuselage Main, Plate/Skin
  > BFM - C4 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN AT BS 1554 BETWEEN S29L TO S30L. REPAIRED FUSELAGE SKIN AT BS 1554 BETWEEN S29L TO S30L IAW EA 134169.
- [SDR USAA2009110993071](https://openairdocs.org/sdr/USAA2009110993071.md): Doubler · cracked · Nov 7, 2009 · N905AW · Boeing 7572S7 · Nacelle/Pylon, Plate/Skin
  > BFM - MAJOR REPAIR - C4 CHECK - CRACKED PYLON SKIN REPAIR DOUBLER ON NR 2 PYLON. REPLACED PYLON SKIN REPAIR DOUBLER ON NR 2 PYLON IAW EA 134171.
- [SDR USAA2009110993060](https://openairdocs.org/sdr/USAA2009110993060.md): Skin · corroded · Nov 4, 2009 · N905AW · Boeing 7572S7 · Fuselage Main, Plate/Skin
  > BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON FUSELAGE SKIN AT BS 1480 - BS 1500, S29R - S30, BL 0. REPAIRED FUSELAGE SKIN AT BS 1480 - BS 1500, S29R - S30, BL 0 IAW EA 134.
- [SDR USAA2009102392857](https://openairdocs.org/sdr/USAA2009102392857.md): Plate · corroded · Oct 22, 2009 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT GALLEY FLOOR DECK PLATE AT BS 1715, LBL 6 - RBL 47, WL 208.1. REPAIRED AFT GALLEY FLOOR DECK PLATE AT BS 1715, LBL 6 - RBL 47, WL 208.1 IAW B757 SRM 53-60-51, 51-21-01 AND 53-00-51.
- [SDR USAA2009102392856](https://openairdocs.org/sdr/USAA2009102392856.md): Plate · corroded · Oct 22, 2009 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT GALLEY FLOOR DECK PLATE, BS 1687 - BS 1715 RBL 50, WL 208.1. REPAIRED AFT GALLEY FLOOR DECK PLATE, BS 1687 - BS 1715 RBL 50, WL 208.1 IAW B757 SRM 53-60-01 AND 51-40-02.
- [SDR USAA2009102392855](https://openairdocs.org/sdr/USAA2009102392855.md): Plate · corroded · Oct 22, 2009 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT GALLEY FLOOR DECK PLATE AT BS 1681, RBL 50, WL 208.1. REPAIRED AFT GALLEY FLOOR DECK PLATE AT BS 1681, RBL 50, WL 208.1 IAW B757 SRM 53-60-01 AND 51-40-02.
- [SDR USAA2009102292842](https://openairdocs.org/sdr/USAA2009102292842.md): Skin · delaminated · Oct 15, 2009 · N905AW · Boeing 7572S7 · Spoilers
  > BFM - C4 - MAJOR REPAIR - NR 4 SPOILER DISBONDED BETWEEN ACTIVATOR & INBOARD HINGE. REPAIRED NR 4 SPOILER SKIN IAW B757 SRM 57-50-01 & 51-70-04.
- [SDR USAA20090807BB121](https://openairdocs.org/sdr/USAA20090807BB121.md): Fuse · blown · Aug 6, 2009 · N905AW · Boeing 7572S7 · Emergency Lighting
  > PHX - EMERGENCY LIGHTS FROM ROW 19 THROUGH AFT GALLEY WERE INOPERATIVE. REPLACED FUSES EXT AFT EMERGENCY LIGHT BATTERY PACK.
- [SDR USAA20090616BB100](https://openairdocs.org/sdr/USAA20090616BB100.md): Actuator · defective · Jun 14, 2009 · N905AW · Boeing 7572S7 · Emergency Equipment
  > PHX - THE SLIDE ARMED LIGHT OVER DOOR L4 DOES NOT ILLUMINATE. REPLACED FORWARD GIRT ACTUATOR.
- [SDR USAA20090424BB071](https://openairdocs.org/sdr/USAA20090424BB071.md): Lanyard · unsecure · Apr 23, 2009 · N905AW · Boeing 7572S7 · Escape Slide
  > PHX - THE LANYARD FOR SLIDE AT DOOR R1 NEEDS TO BE PROPERLY STOWED. THE LANYARD ON SLIDE AT DOOR R1 WAS STOWED.
- [SDR USAABB09017](https://openairdocs.org/sdr/USAABB09017.md): Light · inoperative · Jan 28, 2009 · N905AW · Boeing 7572S7 · Emergency Lighting
  > PHX - THE L1 DOOR EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE RELAMPED THE L1 DOOR EXIT EMERGENCY LIGHT. OPERATIONALLY CHECKS GOOD.
- [SDR USAABB09006](https://openairdocs.org/sdr/USAABB09006.md): Proximity Sensor · faulty · Jan 14, 2009 · N905AW · Boeing 7572S7 · Door Warning System
  > PHX - THE ARMING INDICATOR LIGHT AT DOOR 4R WAS FOUND INOPERATIVE. MAINTENANCE REPLACED PROXIMITY SENSOR (S10224) ON DOOR 4R. OPERATIONALLY CHECKS OK.
- [SDR USAABB08164](https://openairdocs.org/sdr/USAABB08164.md): Gcu · loose · Oct 31, 2008 · N905AW · Boeing 7572S7 · AC Regulator
  > PHX - FLT 45 PHX TO KOA. UPON ROTATION, THE LEFT AC BUS TRIPPED OFF AND COULD NOT BE RESET, OR POWERED BY ANOTHER GENERATOR. THE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE BITE CHECKED THE BUS PROTECTION CONTROL UNIT (BPCU) AND
- [SDR USAABB08163](https://openairdocs.org/sdr/USAABB08163.md): Circuit Breaker · malfunctioned · Oct 17, 2008 · N905AW · Boeing 7572S7 · Navigation System Wiring
  > FLT 119 IN CRUISE, EICAS MESSAGES "L GEN OFF" AND "L AC BUS OFF". DISPLAYED WITH THE CORRESPONDING "L GEN OFF" AND "L BUS OFF" LIGHTS ILLUMINATED. A GENERATOR RESET DID NOT CORRECT THE CONDITION. ATTEMPTS TO POWER THE L AC BUSS FROM THE OTHER POWER SOURCES
- [SDR USAABB08161](https://openairdocs.org/sdr/USAABB08161.md): Circuit Breaker · failed · Oct 17, 2008 · N905AW · Boeing 7572S7 · AC Power Distribution System
  > FLT 119- IN CRUISE, LT AC BUSS FAILED. GENERATOR RESET DID NOT CORRECT CONDITION. ATTEMPTS TO POWER LT AC BUSS FROM OTHER POWER SOURCES NOT SUCCESSFUL. FLT DIVERTED & LANDED WITHOUT INCIDENT. REPLACED GROUND POWER CONTACTOR, CURRENT XFORMERS, & BUSS TIE C/B
- [SDR USAA920081204](https://openairdocs.org/sdr/USAA920081204.md): Angle · cracked · Jun 5, 2008 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C12/ NR 6109923 - INTERCOSTAL UPPER ANGLE CRACKED BS 440 TO 460, WL 208.1, BL0 (HFEC VERIFIED). REPLACED INTERCOSTAL UPPER ANGLE CRACKED BS 440 TO 460, WL 208.1, BL 0 IAW SRM 51-40-02-0G. (K)
- [SDR USAA920081231](https://openairdocs.org/sdr/USAA920081231.md): Structure · corroded · Jun 4, 2008 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > MCN - C12 - MAJOR REPAIR - NR 6061159 - R2 DOOR CUTOUT HAS CORROSION ON INNER STRUCTURE AT BS 686 TO 729.6, WL 208.1. REPLACED R2 DOOR CUTOUT INNER STRUCTURE AT BS 686 TO 729.6, WL 208.1 IAW SRM 51-40-02-0G. (K)
- [SDR USAA920081230](https://openairdocs.org/sdr/USAA920081230.md): Floorbeam · cracked · Jun 2, 2008 · N905AW · Boeing 7572S7 · Fuselage Main, Floor Beam
  > MCN - C12 - MAJOR REPAIR - NR 6111603 - FLOORBEAM CRACKED UPPER T-CAP AFT RADIOS B/S 700 RBL 45 W/L 208.1. REPAIRED FLOORBEAM UPPER T-CAP AFT B/S 700 RBL 45 W/L 208.1 IAW B757 SRM 53-00-51-2R1. (K)
- [SDR USAA920081227](https://openairdocs.org/sdr/USAA920081227.md): Intercostal · cracked · Jun 2, 2008 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > MCN - C112 - MAJOR REPAIR - NR 6109932 - INTERCOSTAL WEB CRACKED B/S 550 RBL 54 W/L 208.1 (HFEC VERIFIED). REPLACED INTERCOSTAL WEB B/S 550 RBL 54 W/L 208.1 IAW SRM 51-40-02-0G. (K)

Next page: https://openairdocs.org/deregistered/N905AW-2016-07-12/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 = 'N905AW' AND deregistration_id = 'N905AW-2016-07-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N905AW-2016-07-12/reports

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