# Service difficulty reports: N910AW

A list on [N910AW](https://openairdocs.org/aircraft/N910AW.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 · 157 reports

- [SDR AALA201608299005](https://openairdocs.org/sdr/AALA201608299005.md): Slide · dislodged · Aug 28, 2016 · N910AW · Boeing 7572G7 · Escape Slide
  > AIRCRAFT WAS NOT GROUNDED: CABIN SERVICE REPORTS L4 DOOR HARD TO CLOSE. FOUND SLIDE PACK TO BE DISLODGED. SAFETY PIN INSTALLED ON INFLATION CYLINDER, REINSTALLED ESCAPE SLIDE IAW AMM 25-66-01 AND REMOVED SAFETY PIN, REMOVED FROM INFLATION CYLINDER.
- [SDR AALA201603299007](https://openairdocs.org/sdr/AALA201603299007.md): Unknown · odor · Mar 28, 2016 · N910AW · Boeing 7572G7 · Air Distribution System
  > AIRCRAFT WAS GNDED. DURING DESCENT THE AFT CABIN FLIGHT ATTENDANT REPORTED SMELL OF SMOKE, NO SOURCE FOUND. DISAPPEARED AFTER 30 SECONDS. DECLARED AN EMER & LANDED SAFELY WITHIN 10 MINUTES WITH NO FURTHER INCIDENTS REPORTED. INSPECTED AREA, NO LINGERING OD
- [SDR AALA201603159019](https://openairdocs.org/sdr/AALA201603159019.md): Flashlight · defective · Mar 14, 2016 · N910AW · Boeing 7572G7 · Emergency Equipment
  > AIRCRAFT WAS NOT GNDED. AFT FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT.
- [SDR AALA201602159004](https://openairdocs.org/sdr/AALA201602159004.md): Wire Harness · damaged · Feb 12, 2016 · N910AW · Boeing 7572G7 · Fire Protection System Wiring
  > RETURNED, ACFT WAS GNDED. CREW NOTED A STATUS MSG, R ENG OH LP1, RESULTING IN THE ACFT RETURNING WHERE IT LANDED SAFELY WITH NO INCIDENTS REPORTED. NO EMER WAS DECLARED & THE ACFT DID NOT LAND OVERWEIGHT. REPLACED THE NR 2 ENG NACELLE OVERHEAT DETECTOR IAW
- [SDR AALA201602159003](https://openairdocs.org/sdr/AALA201602159003.md): Detector · defective · Feb 12, 2016 · N910AW · Boeing 7572G7 · Overheat Detection
  > RETURNED, ACFT WAS GNDED. CREW NOTED A STATUS MSG, RT ENG OH LP1, RESULTING IN THE ACFT RETURNING WHERE IT LANDED SAFELY WITH NO INCIDENTS REPORTED. NO EMER WAS DECLARED & THE ACFT DID NOT LAND OVERWEIGHT. REPLACED THE NR 2 ENG NACELLE OVERHEAT DETECTOR IAW
- [SDR AALA201510159009](https://openairdocs.org/sdr/AALA201510159009.md): Slat · delaminated · Oct 13, 2015 · N910AW · Boeing 7572G7 · Leading Edge Devices
  > LEFT WING NR 4 SLAT HAS DELAMINATION AT INBD TE BOTTOM SIDE. REPLACED SLAT IAW 19L52027002.
- [SDR AALA201510159008](https://openairdocs.org/sdr/AALA201510159008.md): Slat · delaminated · Oct 13, 2015 · N910AW · Boeing 7572G7 · Leading Edge Devices
  > RIGHT WING NR 8 SLAT HAS DELAMINATION AT PREVIOUS REPAIRS, 3 EACH, AREA 1. APPROX 70" FROM INBD EDGE. AREA 2, 19" FROM INBD EDGE. AREA 3, 13" FROM OTBD END & 2" FROM TE. R & R NR 8 SLAT IAW 19L52027002.
- [SDR AALA201504229008](https://openairdocs.org/sdr/AALA201504229008.md): Light · inoperative · Apr 21, 2015 · N910AW · Boeing 7572G7 · Emergency Lighting
  > ROW 26 LT EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT 26 LT EMERGENCY LIGHT.
- [SDR AALA201504149030](https://openairdocs.org/sdr/AALA201504149030.md): Access Panel · cracked · Apr 11, 2015 · N910AW · Boeing 7572G7 · Wing, Plate/Skin
  > RIGHT WING FUEL ACCESS PANEL 641GB CRACKED & LEAKING FUEL. REPLACED RT WING FUEL ACCESS PANEL 641GB IAW AMM 28-11-00. LEAK CHECKED GOOD.
- [SDR USAA2015012300002](https://openairdocs.org/sdr/USAA2015012300002.md): Lock · lack of lube · Jan 22, 2015 · N910AW · Boeing 7572G7 · Flight Compartment Equipment
  > EN-ROUTE, CAPTAIN`S SEAT TRACK LOCK FAILED ON TAKEOFF, SEAT ROLLED BACK. LUBED THE SEAT TRACK LOCK MECHANISM.
- [SDR USAA2015011200012](https://openairdocs.org/sdr/USAA2015011200012.md): Aileron · debonded · Dec 26, 2014 · N910AW · Boeing 7572G7 · Ailerons
  > C2 CHECK, DISBONDING ON LT AILERON AT MOST INBD END & 12 INCHES FWD OF TE. REPLACED LT AILERON IAW JOB CARD 19L56827001.
- [SDR USAA2015011200013](https://openairdocs.org/sdr/USAA2015011200013.md): Skin Panel · delaminated · Dec 24, 2014 · N910AW · Boeing 7572G7 · Fuselage Main, Plate/Skin
  > C2 CHECK, DELAMINATION ON APU COMPARTMENT RT INTERIOR SKIN PANEL AT BS 1926, WL 247.6. REPAIRED APU COMPARTMENT RT INTERIOR SKIN PANEL AT BS 1926, WL 247.6 IAW SRM 51-70-10, REPAIR 4 & EA 106387.
- [SDR USAA2014122600003](https://openairdocs.org/sdr/USAA2014122600003.md): Skin Panel · delaminated · Dec 24, 2014 · N910AW · Boeing 7572G7 · Fuselage Main, Plate/Skin
  > C2 CHECK DELAMINATION & CRACK AT APU COMPARTMENT TAIL CONE RT INTERIOR FUSELAGE SKIN PANEL AT STATION 1925 ON BACK SIDE OF ELEVATOR INDEX. ACCOMPLISHED TIME LIMITED REPAIR IAW EA 106387.
- [SDR USAA2015011200014](https://openairdocs.org/sdr/USAA2015011200014.md): Panel · cracked · Dec 11, 2014 · N910AW · Boeing 7572G7 · Leading Edge Devices
  > C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 3 LE COVE PANEL AT APPROX 354 INCHES FROM INBD EDGE & 14 INCHES DOWN FROM TE. REPLACED LT WING NR 3 LE COVE PANEL IAW DWGS 114N4004 & 114N4077.
- [SDR USAA2015011200016](https://openairdocs.org/sdr/USAA2015011200016.md): Panel · cracked · Dec 10, 2014 · N910AW · Boeing 7572G7 · Leading Edge Devices
  > C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 1 LE COVE PANEL AT APPROX 30 INCHES FROM OTBD EDGE & 13 INCHES DOWN FROM TE. REPLACED LT WING NR 3 LE COVE PANEL IAW DWG 114N4075.
- [SDR USAA2015011200015](https://openairdocs.org/sdr/USAA2015011200015.md): Panel · cracked · Dec 10, 2014 · N910AW · Boeing 7572G7 · Leading Edge Devices
  > C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 1 LE COVE PANEL AT APPROX 54 INCHES FROM INBD EDGE & 11.250 INCHES DOWN FROM TE. REPLACED LT WING 1 LE COVE PANEL IAW DWG 114N4075.
- [SDR USAA2014052300003](https://openairdocs.org/sdr/USAA2014052300003.md): Wire Harness · broken · May 22, 2014 · N910AW · Boeing 7572G7 · Light System Wiring
  > PHX SEAT ROW 6 EMERGENCY LIGHT HAS BROKEN WIRE AT CONNECTOR. REPLACED WIRE HARNESS, OPERATIONS GOOD.
- [SDR USAA2014042100021](https://openairdocs.org/sdr/USAA2014042100021.md): Switch · no test · Apr 21, 2014 · N910AW · Boeing 7572G7 · Emergency Lighting
  > PHX IAW OVERNIGHT CHECK STEP 4, EMERGENCY LIGHTING TEST SWITCH OVER L3 DOOR ESCAPE WILL NOT TEST. R & R EMERGENCY LIGHT TEST SWITCH AT L3 DOOR.
- [SDR USAA2014031800001](https://openairdocs.org/sdr/USAA2014031800001.md): Slide · multiple fail · Mar 17, 2014 · N910AW · Boeing 7572G7 · Escape Slide
  > DOOR 4L GIRT BAR CAME OUT FROM SLIDE ASSEMBLY. 4L SLIDE REMOVED & REINSTALLED. PROBLEM WITH ARM & DISARM RIG. REPLACED THE L4 DOOR GIRT BAR OPERATING MECHANISM AFT LIFTER ATTACHMENT BRACKET & PIVOT POINT BEARINGS, VERTICAL ROD LOWER ROD END BEARINGS, AFT CR
- [SDR USAA2014013100004](https://openairdocs.org/sdr/USAA2014013100004.md): Girt Bar · defective · Jan 29, 2014 · N910AW · Boeing 7572G7 · Emergency Equipment
  > PHX 4L DOOR ARMED LIGHT WOULD NOT ILLUMINATE WHEN ARMED. REINSTALLED GIRT BAR FOOT, OPERATIONS CHECKED GOOD.
- [SDR USAA2013121700002](https://openairdocs.org/sdr/USAA2013121700002.md): Transceiver · faulty · Dec 15, 2013 · N910AW · Boeing 7572G7 · HF Communications System
  > FLIGHT 694 ENROUTE. HF NR 1 WILL NOT TUNE. DETECTED SMOKE & TURNED OFF HF NR 1 RADIO UNTIL SMOKE ODOR WENT AWAY. LEFT OFF REMAINDER OF FLIGHT. HF NR 2 TUNE & WORKS NORMAL. REPLACED LEFT HF TRANSCEIVER. OPS CHECKED NORMAL.
- [SDR USAA2013120200016](https://openairdocs.org/sdr/USAA2013120200016.md): Frame · damaged · Nov 7, 2013 · N910AW · Boeing 7572G7 · Fuselage Main, Frame
  > C1 CHECK ELEC ARCING DAMAGE AT TERMINAL LUG BRACKET & FRAME ATTACH POINTS AT BS 1480 BETWEEN STRINGER 23R TO STRINGER 24R. REPAIRED FUSELAGE FRAME AT BS 1480 BETWEEN STRINGER 23R TO STRINGER 24R IAW EA 105310.
- [SDR USAA2013110800010](https://openairdocs.org/sdr/USAA2013110800010.md): Skin · cracked · Nov 6, 2013 · N910AW · Boeing 7572G7 · Wing, Plate/Skin
  > DURING C1 CHECK, CRACK FOUND ON NR 2 OTBD SLAT COVE PANEL AT APPROX. 29 INCHES INBD FROM OTD EDGE & 3 INCHES UP FROM LOWER SIDE. REPLACED LT WING 2 OTBD SLAT COVE PANEL IAW SRM 51-40-02 & DWG 114N4076.
- [SDR USAA2013110800011](https://openairdocs.org/sdr/USAA2013110800011.md): Skin · cracked · Nov 5, 2013 · N910AW · Boeing 7572G7 · Wing, Plate/Skin
  > DURING C1 CHECK, CRACK FOUND ON NR 3 SLAT COVE PANEL AT APPROX 5 INCHES INBD FROM OTBD PANEL EDGE & 2 INCHES UP FROM BOTTOM EDGE. REPLACED LT WING NR 3 SLAT COVE PANEL IAW SRM 51-40-02 & DWG 114N4004.
- [SDR USAA2013030100004](https://openairdocs.org/sdr/USAA2013030100004.md): Stator · failed · Feb 26, 2013 · N910AW · Boeing 7572G7 · Air Distribution Fan
  > HNL - FLT 22 EN ROUTE PHX TO HNL. SMOKE SMELL IN CABIN, EICAS R RECIRC FAN, OVERHEAD RIGHT RECIRC FAN INOP. REPLACED THE RIGHT CABIN AIR RECIRCULATION FAN. FOUND STATOR AND BEARING FAILED.
- [SDR USAA2012112300014](https://openairdocs.org/sdr/USAA2012112300014.md): Lens · damaged · Nov 22, 2012 · N910AW · Boeing 7572G7 · Emergency Lighting
  > PHX - SEAT MOUNTED EMERGENCY EXIT LIGHT (RED) LENSES DAMAGED 2 EA ROW 10ABC. REPLACED LENSES AS NEEDED.
- [SDR USAA2012092100001](https://openairdocs.org/sdr/USAA2012092100001.md): Solenoid · failed · Sep 18, 2012 · N910AW · Boeing 7572G7 · Autopilot Main Servo
  > PHX FLT 125 EN ROUTE HNL TO PHX. WHEN AUTOPILOT WAS DISCONNECTED AT 6000FT ON APPROACH THE ROLL YOKE CONTROL WAS VERY HEAVY (ABOUT 3X NORMAL FORCE). IT WAS THE SAME IN BOTH CAPT AND F/O YOKE. (PITCH CONTROL WAS NORMAL) THIS HEAVINESS REMAINED AFTER LANDIN
- [SDR USAA2012091400065](https://openairdocs.org/sdr/USAA2012091400065.md): Megaphone · inoperative · Sep 13, 2012 · N910AW · Boeing 7572G7 · Emergency Equipment
  > PHX - AFT MEGAPHONE INOP. REPLACED AFT EMERGENCY MEGAPHONE.
- [SDR USAA2012061400028](https://openairdocs.org/sdr/USAA2012061400028.md): Diode · failed · Jun 13, 2012 · N910AW · Boeing 7572G7 · Trailing Edge Flap Control System
  > PHX - FLT 26 EN ROUTE OGG TO PHX. FLAPS FAILED TO MOVE, TRAILING EDGE LIGHT ON, AND EICAS MSG TRAILING EDGE DISAGREE DISPLAYED. FLAPS NORMAL ON ALTERNATE SYS. THE FLIGHT PERFORMED A GO-AROUND TO RUN THE CHECKLIST. ON THE SECOND APPROACH, THE FLIGHT LANDED
- [SDR USAA2012061400003](https://openairdocs.org/sdr/USAA2012061400003.md): Syncronizer · failed · Jun 13, 2012 · N910AW · Boeing 7572G7 · Trailing Flap Position Indicating System
  > PHX - FLT 26 EN ROUTE OGG TO PHX. FLAPS FAILED TO MOVE, TRAILING EDGE LIGHT ON, AND EICAS MSG TRAILING EDGE DISAGREE DISPLAYED. FLAPS NORMAL ON ALTERNATE SYS. THE FLIGHT PERFORMED A GO-AROUND TO RUN THE CHECKLIST. ON THE SECOND APPROACH, THE FLIGHT LANDE
- [SDR USAA2012051700028](https://openairdocs.org/sdr/USAA2012051700028.md): Survival Kit · unserviceable · May 14, 2012 · N910AW · Boeing 7572G7 · Escape Slide
  > PHX - INFLIGHT CREW REPORTS SLIDE RAFT SURVIVAL KITS NOT SEALED. REPLACED 4 EA SLIDE RAFT SURVIVAL KITS ASSY.
- [SDR USAA2012040500001](https://openairdocs.org/sdr/USAA2012040500001.md): Web · corroded · Mar 27, 2012 · N910AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR WEB PANEL AT BS 1420, S17R. REPAIRED FLOOR WEB PANEL AT BS 1420, S17R IAW EA 103818.
- [SDR USAA2012032000002](https://openairdocs.org/sdr/USAA2012032000002.md): Angle · cracked · Mar 16, 2012 · N910AW · Boeing 7572G7 · Fuselage Main, Frame
  > C4 CHECK - CRACK ON FORWARD SIDE OF FRAME L-ANGLE AT BS 350, S7L. REPLACED FRAME L-ANGLE AT BS 350, S7L IAW B757 SRM 51-40-10.
- [SDR USAA2012040500004](https://openairdocs.org/sdr/USAA2012040500004.md): Pin · cracked · Mar 14, 2012 · N910AW · Boeing 7572G7 · Nacelle/Pylon, Attach Fittings
  > C4 CHECK - CRACK IN LOWER FUSE PIN OF RIGHT ENGINE NACELLE STRUT DIAGONAL BRACE AT PPS 300, PPWL 161.70. REPLACED LOWER FUSE PIN OF DIAGONAL BRACE AT PPS 300, PPWL 161.70 IAW B757 AMM 54-51-02.
- [SDR USAA2012040900025](https://openairdocs.org/sdr/USAA2012040900025.md): Wedge · delaminated · Mar 9, 2012 · N910AW · Boeing 7572G7 · Leading Edge Devices
  > C4 CHECK - DELAMINATION ON NR 7 SLAT TRAILING EDGE WEDGE AT WS 397.50, WBL 740.00, 6 INCHES FROM INBOARD END AT LOWER SKIN. REPAIRED NR 7 SLAT TRAILING EDGE WEDGE AT WS 397.50, WBL 740.00 IAW B757 SRM 51-70-10.
- [SDR USAA2012031300015](https://openairdocs.org/sdr/USAA2012031300015.md): Skin · damaged · Mar 9, 2012 · N910AW · Boeing 7572G7 · Trailing Edge Flaps
  > C4 CHECK - SMALL 1 INCH SPLIT IN RIGHT INBOARD AFT FLAP ON OUTBOARD END AT WS 258.50, WBL 740. REPAIRED RIGHT INBOARD AFT FLAP SKIN IAW B757 SRM 51-70-17.
- [SDR USAA2012040500003](https://openairdocs.org/sdr/USAA2012040500003.md): Stiffener · cracked · Mar 6, 2012 · N910AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > C4 CHECK - CRACK ON FLOORBEAM STIFFENER STRAP AT BS 718, RBL 48. REPAIRED FLOORBEAM STABILIZER STRAP AT BS 718, RBL 48 IAW EA 103787.
- [SDR USAA2012032200005](https://openairdocs.org/sdr/USAA2012032200005.md): Strap · cracked · Mar 6, 2012 · N910AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > C4 CHECK - CRACK ON STRAP AT BS 720, LBL 24. REPAIRED STRAP AT BS 720, LBL 24 IAW TYPICAL REPAIR TR 757-5335-11-0334.
- [SDR USAA2012032000003](https://openairdocs.org/sdr/USAA2012032000003.md): Floorbeam · corroded · Mar 3, 2012 · N910AW · Boeing 7572G7 · Fuselage Main, Floor Beam
  > C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS 377.7 & BETWEEN LBL 54 TO LBL 60. REPAIRED FLOORBEAM AT BS 377.7 & BETWEEN LBL 54 TO LBL 60 IAW B757 SRM 53-00-51-2R-5.
- [SDR USAA2012040500002](https://openairdocs.org/sdr/USAA2012040500002.md): Floorbeam · corroded · Feb 29, 2012 · N910AW · Boeing 7572G7 · Fuselage Main, Floor Beam
  > C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR BEAM T-CAP AT BS 365 BETWEEN RBL 36 TO RBL 59. REPAIRED FLOORBEAM T-CAP AT BS 365 BETWEEN RBL 36 TO RBL 59 IAW EA 103801.
- [SDR USAA2012030800005](https://openairdocs.org/sdr/USAA2012030800005.md): Floor Support · corroded · Feb 29, 2012 · N910AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > C4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT AT BS 1316, RBL 18. REPLACED FLOOR SUPPORT AT BS 1316, RBL 18 IAW B757 SRM 51-10-02 & 51-40-00.
- [SDR USAA2012011700024](https://openairdocs.org/sdr/USAA2012011700024.md): Fitting · missing · Jan 16, 2012 · N910AW · Boeing 7572G7 · Emergency Equipment
  > PHX - GIRT BAR ENGAGEMENT LIGHT EXTIN WITH EVACUATION SLIDE ARMING LEVER IN ENGAGE POS AT ENTRY/SERVICE DOOR L-4. FOUND FWD GIRT BAR END FITTING MISSING. REPLACED MISSING GIRT BAR END FITTING.
- [SDR USAA2011122300020](https://openairdocs.org/sdr/USAA2011122300020.md): Girt Bar · missing · Dec 22, 2011 · N910AW · Boeing 7572G7 · Emergency Equipment
  > PHX - AFT LEFT SLIDE ARM DOOR LIGHT INOP. FOUND L4 DOOR, FWD GIRT BAR SLIDER MISSING. INSTALLED SLIDER. DOOR ARM LIGHT OPS GOOD.
- [SDR USAA2011080900011](https://openairdocs.org/sdr/USAA2011080900011.md): Pin · backed out · Aug 7, 2011 · N910AW · Boeing 7572G7 · Light System Wiring
  > PHX - EMERGENCY LIGHT ON SEAT 7 INOP. RELAMP, NO HELP. RESEATED PUSHED PIN IN EMER LIGHT CONNECTOR FOR SEAT 7.
- [SDR USAA2011080200027](https://openairdocs.org/sdr/USAA2011080200027.md): Wire Harness · inoperative · Jul 31, 2011 · N910AW · Boeing 7572G7 · Light System Wiring
  > PHX - EMERGENCY LIGHT ON SEAT 23 INOP. MAINTENANCE REPLACED FLOOR TO LIGHT HARNESS. OPS GOOD.
- [SDR USAA20110204BB006](https://openairdocs.org/sdr/USAA20110204BB006.md): Girt Bar · bent · Feb 2, 2011 · N910AW · Boeing 7572G7 · Emergency Equipment
  > PHX - THE L4 DOOR GIRT BAR AFT SPRING TAB WAS BENT. REMOVED AND REPLACED THE L4 DOOR GIRT BAR.
- [SDR USAA2010111092583](https://openairdocs.org/sdr/USAA2010111092583.md): Support Angle · corroded · Nov 5, 2010 · N910AW · Boeing 7572G7 · Fuselage Miscellaneous Structure
  > CLT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FORWARD CARGO LATERAL SUPPORT ANGLE AT BS 690, LBL 14. REPLACED FORWARD CARGO LATERAL SUPPORT ANGLE AT BS 690, LBL 14 IAW B757 SRM 51-10-01 & 51-20-05.
- [SDR USAA2010111192589](https://openairdocs.org/sdr/USAA2010111192589.md): Support Angle · corroded · Oct 20, 2010 · N910AW · Boeing 7572G7 · Fuselage Main, Bulkhead
  > CLT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LOWER AFT CARGO BULKHEAD SUPPORT ANGLE AT BS 848, RBL 2. REPLACED LOWER AFT CARGO BULKHEAD SUPPORT ANGLE AT BS 848, RBL 2 IAW BOEING DRAWING 453N1814.
- [SDR USAA2010102992453](https://openairdocs.org/sdr/USAA2010102992453.md): Fitting · corroded · Oct 16, 2010 · N910AW · Boeing 7572G7 · Cargo/Baggage Doors
  > CLT - C3 - MAJOR REPAIR - NR I2D52602/007 - CORROSION ON SMALL CLIP ON AFT CARGO DOOR LOWER FORWARD CORNER INTERIOR. REPLACED SMALL CLIP ON AFT CARGO DOOR LOWER FORWARD CORNER INTERIOR IAW B757 SRM 51-10-00, 51-40-02 & BOEING DRAWING 69-47423-7.
- [SDR USAA20100604BB035](https://openairdocs.org/sdr/USAA20100604BB035.md): Slide · low pressure · Jun 1, 2010 · N910AW · Boeing 7572G7 · Escape Slide
  > PHX - R3 EMERGENCY DOOR SLIDE HAS LOW PRESSURE. REPLACED R3 DOOR SLIDE.

Next page: https://openairdocs.org/aircraft/N910AW/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 = 'N910AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N910AW/reports

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