# Service difficulty reports: N901AW, cancelled May 8, 2017

A list on [N901AW, cancelled May 8, 2017](https://openairdocs.org/deregistered/N901AW-2017-05-08.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 5 · 231 reports

- [SDR AALA201606209001](https://openairdocs.org/sdr/AALA201606209001.md): Actuator · defective · Jun 16, 2016 · N901AW · Boeing 7572S7 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED, R4 DOOR GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. REPLACED PROXIMITY SENSOR AND ACTUATOR, TARGET, AT THE R4 DOOR. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 25-66-11.
- [SDR AALA201606179008](https://openairdocs.org/sdr/AALA201606179008.md): Proximity Sensor · defective · Jun 16, 2016 · N901AW · Boeing 7572S7 · Door Warning System
  > AIRCRAFT WAS NOT GROUNDED: R4 DOOR GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. REPLACED PROXIMITY SENSOR AND ACTUATOR, TARGET, AT THE R4 DOOR. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 25-66-11.
- [SDR AALA201605289002](https://openairdocs.org/sdr/AALA201605289002.md): Reservoir · low pressure · May 27, 2016 · N901AW · Boeing 7572S7 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GNDED. L2 DOOR EMER POWER RESERVOIR PRESS IS 0. REPLACED L2 DOOR EMER POWER RESERVOIR IAW AMM 52-11-30.
- [SDR AALA201602099006](https://openairdocs.org/sdr/AALA201602099006.md): Pump · inoperative · Feb 6, 2016 · N901AW · Boeing 7572S7 · Fuel Boost Pump
  > AIRCRAFT WAS NOT GNDED. LT CTR TANK FUEL PUMP, PRESS LIGHT & CTR LT FUEL PUMP, EICAS MSG APPEARED AFTER ENG START. ASSOCIATED CB FOUND TRIPPED ON P6 3 PANEL F14. R & R LT CTR TANK FUEL PUMP MOTOR IMPELLER IAW AMM 28-22-03-401. ALL FUNCTIONAL CHECKED GOOD.
- [SDR AALA201509259001](https://openairdocs.org/sdr/AALA201509259001.md): Pump · inoperative · Sep 21, 2015 · N901AW · Boeing 7572S7 · Fuel Boost Pump
  > THE FLIGHT DIVERTED DUE TO LT CTR FUEL PUMP INOPERATIVE & ASSOCIATED PRESS EICAS MSG. R & R LT CTR FUEL BOOST PUMP IAW AMM 28-22-03.
- [SDR AALA201506229009](https://openairdocs.org/sdr/AALA201506229009.md): Slide · low pressure · Jun 21, 2015 · N901AW · Boeing 7572S7 · Escape Slide
  > L4 DOOR SLIDE PRESS LOW. REPLACED L4 DOOR SLIDE IAW 19L80025002.
- [SDR AALA201506229008](https://openairdocs.org/sdr/AALA201506229008.md): Rivet · loose · Jun 21, 2015 · N901AW · Boeing 7572S7 · Emergency Equipment
  > L4 DOOR EVACUATION SLIDE GIRT BAR SLIDER LOOSE AT RIVET. REPLACED RIVETS IAW SRM 51-42-11.
- [SDR USAA2015030100007](https://openairdocs.org/sdr/USAA2015030100007.md): Snubber · worn · Feb 27, 2015 · N901AW · Boeing 7572S7 · Passenger/Crew Doors
  > DOOR L4 ROTARY SNUBBER MINIMUM WEAR PIN EXTENSION IS NOT CORRECT. REPLACED DOOR L4 ROTARY SNUBBER.
- [SDR USAA2015021900004](https://openairdocs.org/sdr/USAA2015021900004.md): Strap · cracked · Feb 13, 2015 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C4 CHECK, STABILIZER STRAP CRACKED. FABRICATED REPAIR PARTS & INSTALLED REPAIR DOUBLER PLATES IAW EA 106499.
- [SDR USAA2015022100009](https://openairdocs.org/sdr/USAA2015022100009.md): Crease Beam · corroded · Feb 10, 2015 · N901AW · Boeing 7572S7 · Fuselage Main, Structure
  > C4 CHECK, RT CREASE BEAM INNER CHORD IS CORRODED ON UPPER & LOWER SURFACES. INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-40-02 & DWG 146N8322.
- [SDR USAA2015021900007](https://openairdocs.org/sdr/USAA2015021900007.md): Floor Support · corroded · Feb 9, 2015 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > CORROSION ON MAIN DECK SUPPORT STRUCTURE BY R1 DOOR. REMOVED, FABRICATED & INSTALLED NEW FLOOR SUPPORT IAW DWG 141N5186 & SRM 51-40-02.
- [SDR USAA2015021900005](https://openairdocs.org/sdr/USAA2015021900005.md): Angle · cracked · Feb 5, 2015 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C4 CHECK, VERTICAL ANGLE CRACKED BELOW FLOORBEAM. FABRICATED & INSTALLED NEW ANGLE IAW DWG 143N5532 & SRM 51-10-2.
- [SDR USAA2015020900019](https://openairdocs.org/sdr/USAA2015020900019.md): Tee Fitting · cracked · Feb 5, 2015 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C4 CHECK, CRACKED T CLIP AT STATION 960, STRINGER 7R. REPLACED T CLIP IAW DWG 140N2001.
- [SDR USAA2015031300008](https://openairdocs.org/sdr/USAA2015031300008.md): Floorbeam · corroded · Feb 4, 2015 · N901AW · Boeing 7572S7 · Fuselage Main, Floor Beam
  > C4 CHECK CORROSION ON FLOORBEAM AT STATION 365.25 BETWEEN RBL 38 & 50. REPLACED FLOORBEAM UPPER T CAP IAW SRM 53-00-51-2R.
- [SDR USAA2015021900006](https://openairdocs.org/sdr/USAA2015021900006.md): Panel · delaminated · Feb 4, 2015 · N901AW · Boeing 7572S7 · Vertical Stabilizer Miscellaneous Structure
  > C4 CHECK, RT SIDE OF VERTICAL STABILIZER TORQUE BOX PANEL ON INSIDE SKIN IS DELAMINATED. R & R TORQUE BOX PANEL IAW SRM 51-40 & DWG 175N2001-4.
- [SDR USAA2015022100008](https://openairdocs.org/sdr/USAA2015022100008.md): Doubler · gouged · Feb 3, 2015 · N901AW · Boeing 7572S7 · Fuselage Main, Frame
  > C4 CHECK, FUSELAGE FRAME REPAIR DOUBLER GOUGED IN TWO PLACES ABOVE FLOOR RT SIDE. THE REPAIR DOUBLER WAS REMOVED & FRAME REPAIRED IAW SRM 53-00-07-2R-1.
- [SDR USAA2015022100010](https://openairdocs.org/sdr/USAA2015022100010.md): Angle · cracked · Feb 2, 2015 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C4 CHECK, CRACKED ANGLE ON UPPER SIDE OF FWD ENTRY DOOR TOP CUT OUT WEB. R & R FABRICATED ATTACH ANGLE IAW DWG 141N8321 & SRM 51-10-02.
- [SDR USAA2015021900009](https://openairdocs.org/sdr/USAA2015021900009.md): Angle · cracked · Feb 2, 2015 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C4 CHECK, ANGLE CRACKED ON UPPER SIDE OF L1 ENTRY DOOR WEB CUT OUT. REPLACED ANGLE IAW SRM 51-10-02 & DWG 141N-8321.
- [SDR USAA2015021900008](https://openairdocs.org/sdr/USAA2015021900008.md): Intercostal · corroded · Feb 2, 2015 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous Structure
  > C4 CHECK, CORROSION ON INTERCOSTAL BY R1 DOOR FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A. INSTALLED NEW PART IAW SRM 51-10-02.
- [SDR USAA2015020200020](https://openairdocs.org/sdr/USAA2015020200020.md): Panel · cracked · Jan 28, 2015 · N901AW · Boeing 7572S7 · Leading Edge Devices
  > C4 CHECK, NR 9 SLAT COVE PANEL BETWEEN OTBD MAIN TRACK LUG & AUX TRACK IS CRACKED AROUND FASTENER THAT MEASURED 2.125 INCH CRACK FROM COVE PANEL FASTENER, 2'6 INCHES FROM OTBD END & 1'1 INCH FROM TE. FABRICATED NEW COVE PANEL IAW DWG 141N4076. COMPLETED INST
- [SDR USAA2014111700016](https://openairdocs.org/sdr/USAA2014111700016.md): Windshield · arced · Nov 15, 2014 · N901AW · Boeing 7572S7 · Flight Compartment Windows
  > ENROUTE, CAPTAIN`S FWD WINDOW WAS ARCING. R & R THE CAPTAIN'S FWD WINDSHIELD.
- [SDR USAA2014042100020](https://openairdocs.org/sdr/USAA2014042100020.md): Bottle · low pressure · Apr 18, 2014 · N901AW · Boeing 7572S7 · Service Doors
  > PHX R2 DOOR ASSIST BOTTLE LOW. SERVICED THE R2 DOOR ASSIST BOTTLE.
- [SDR USAA2013122400010](https://openairdocs.org/sdr/USAA2013122400010.md): Skin Panel · delaminated · Dec 22, 2013 · N901AW · Boeing 7572S7 · Horizontal Stabilizer, Plate/Skin
  > C3 CHECK, DELAMINATED AREA ON LT UPPER HORIZONTAL STABILIZER INBD FWD SKIN PANEL BETWEEN FSS 56.05 TO FSS 83.48, APPROXIMATELY 18 INCHES OTBD FROM FUSELAGE. REPAIRED LT UPPER HORIZONTAL STABILIZER INBD FWD SKIN PANEL BETWEEN FSS 56.05 TO FSS 83.48 IAW EA 5059
- [SDR USAA2013121700007](https://openairdocs.org/sdr/USAA2013121700007.md): Slide Raft · loose · Dec 16, 2013 · N901AW · Boeing 7572S7 · Escape Slide
  > C1 CHECK, L2 DOOR SLIDE RAFT NOT PROPERLY SECURED. INSTALLED & SECURED L2 DOOR ESCAPE SLIDE IAW JOB CARD 19C83225004.
- [SDR USAA2013121000003](https://openairdocs.org/sdr/USAA2013121000003.md): Skin · debonded · Dec 7, 2013 · N901AW · Boeing 7572S7 · Leading Edge Devices
  > C3 CHECK, DIS BONDING ON 10 SLAT UPPER TE SKIN AT OSS 791.97. REPAIRED NR 10 SLAT UPPER TE SKIN AT OSS 791.97 IAW B757 SRM 51-70-10-2R & 57-43-02.
- [SDR USAA2013091200002](https://openairdocs.org/sdr/USAA2013091200002.md): Girt Bar · worn · Sep 10, 2013 · N901AW · Boeing 7572S7 · Emergency Equipment
  > L1 FWD DOOR GIRT BAR SPRINGS WORN. MX R & R GIRT BAR ASSY.
- [SDR USAA2013091200001](https://openairdocs.org/sdr/USAA2013091200001.md): Harness · rotted · Sep 10, 2013 · N901AW · Boeing 7572S7 · Escape Slide
  > HARNESS ASSY FOR L1 DOOR SLIDE DRY ROTTED. HARNESS ASSY REQUIRES REPLACEMENT. MX INST SERV L1 DOOR SLIDE APRON HARNESS.
- [SDR USAA2013091000012](https://openairdocs.org/sdr/USAA2013091000012.md): Skin · delaminated · Sep 10, 2013 · N901AW · Boeing 7572S7 · Trailing Edge Flaps
  > DELAMINATION & SEPARATION ON RT WING INBD T/E FLAP UPPER SURFACE AT MF BS 220 APPROX 8 FT FROM AFT END. REPLACED RT WING INBD T/E FLAP IAW JC 19L50027003.
- [SDR USAA2013080800002](https://openairdocs.org/sdr/USAA2013080800002.md): Fuse · blown · Aug 7, 2013 · N901AW · Boeing 7572S7 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE ROW 8L INOPERATIVE. R & R FUSE IN POWER SUPPLY M731.
- [SDR USAA2013070300002](https://openairdocs.org/sdr/USAA2013070300002.md): Rod End Bearing · worn · Jul 2, 2013 · N901AW · Boeing 7572S7 · Emergency Equipment
  > L-1 DOOR GIRT BAR FWD & AFT ROD END BEARINGS WORN. R & R L1 DOOR GIRT BAR FWD & AFT ROD ENDS, AND INST ROD.
- [SDR USAA2013053100002](https://openairdocs.org/sdr/USAA2013053100002.md): Door · lack of lube · May 30, 2013 · N901AW · Boeing 7572S7 · Passenger/Crew Doors
  > DOOR L1 HARD TO OPEN AFTER COLD SOAKED. WILL ONLY OPEN 18" FREELY, THEN REQUIRES UNDUE FORCE. MOVES FREELY AFTER WARM UP. LUBED L1 DOOR. NO FAULT NOTED AT THIS TIME. OK FOR FLIGHT.
- [SDR USAA2013052000008](https://openairdocs.org/sdr/USAA2013052000008.md): Hinge · lack of lube · May 17, 2013 · N901AW · Boeing 7572S7 · Fuselage, Door Hinge
  > L1 DOOR WAS VERY HARD TO FULLY OPEN. APPEARS JAMMED IN HINGE AREA. LUBED DOOR HINGES. DOOR OPENS AND CLOSES NORMALLY.
- [SDR USAA2013031900023](https://openairdocs.org/sdr/USAA2013031900023.md): Skin · delaminated · Mar 19, 2013 · N901AW · Boeing 7572S7 · Leading Edge Devices
  > RON VISIT - DELAMINATION ON LOWER SURFACE OF LEFT WING 5 SLAT TRAILING EDGE WEDGE BETWEEN SLAT STA 200 TO SLAT STA 224 APPROX 26 INCHES FROM OUTBOARD END. REPLACED LEFT WING 5 SLAT ASSEMBLY IAW B757 JOB CARD 19L51027001.
- [SDR USAA2013031400001](https://openairdocs.org/sdr/USAA2013031400001.md): Cover · unsecure · Mar 13, 2013 · N901AW · Boeing 7572S7 · Emergency Lighting
  > PHX - PLASTIC COVER OVER DOOR 2L FALLS OFF. REPLACED EXIT LIGHT COVER ON L2 DOOR WAY, OPS CHECK GOOD.
- [SDR USAA2013030800013](https://openairdocs.org/sdr/USAA2013030800013.md): Bottle · activated · Mar 7, 2013 · N901AW · Boeing 7572S7 · Passenger/Crew Doors
  > KOA - DOOR 2L ASSIST BOTTLE ACTIVATED WHEN CLOSING DOOR. MAINTENANCE REMOVED AND REPLACED L-2 DOOR ASSIST BOTTLE. ALSO PERFORMED EMERGENCY POWER ACTUATION CABLE SYSTEM TEST. OPS CHECKED GOOD.
- [SDR USAA2013022800004](https://openairdocs.org/sdr/USAA2013022800004.md): Skin · delaminated · Feb 27, 2013 · N901AW · Boeing 7572S7 · Leading Edge Devices
  > RON - NR 6 SLAT HAS A 6 INCH X 6 INCH AREA OF DELAMINATED SKIN 4 INCHES INBOARD OF INBOARD END ON BOTTOM SIDE. REMOVED AND REPLACED SLAT IAW JOB CARD 19L51027001.
- [SDR USAA2012051800002](https://openairdocs.org/sdr/USAA2012051800002.md): Mechanism · out of adjust · May 17, 2012 · N901AW · Boeing 7572S7 · Emergency Equipment
  > PHX - DOOR 4L WILL NOT ARM FLIGHT ATTENDANT REPORTS. FOUND GIRT BAR MECHANISM FWD ROD ARM SAFETY LOOSE. ADJUSTED ROD ARM MECHANISM FOR GIRT BAR.
- [SDR USAA2012051700030](https://openairdocs.org/sdr/USAA2012051700030.md): Bolt · overtorqued · May 14, 2012 · N901AW · Boeing 7572S7 · Landing Gear Retraction/Extension System
  > PHX - FLT 9251 PHX TEST FLT. NO NOSE GEAR EXT WITH ALT GEAR EXTENSION. MAINTENANCE CORRECTED BINDING CONDITION OF NOSE GEAR LOCK LINK AT APEX BOLT. PERFORMED ALTERNATE GEAR EXTENSION TEST. NO FAULTS NOTED DURING THREE CYCLES.
- [SDR USAA2012043000024](https://openairdocs.org/sdr/USAA2012043000024.md): Wedge · debonded · Apr 26, 2012 · N901AW · Boeing 7572S7 · Leading Edge Devices
  > C2 CHECK - DISBONDING ON NR 5 SLAT TRAILING EDGE WEDGE APPROX 58 INCHES FROM OUTBOARD END AT WS 257. REPAIRED NR 5 SLAT TRAILING EDGE WEDGE IAW B757 SRM 51- 70-10.
- [SDR USAA2012043000023](https://openairdocs.org/sdr/USAA2012043000023.md): Wedge · debonded · Apr 19, 2012 · N901AW · Boeing 7572S7 · Leading Edge Devices
  > C2 CHECK - DISBONDING ON NR 5 SLAT TRAILING EDGE WEDGE APPROX 5 INCHES FROM OUTBOARD END BETWEEN WS 285.65. REPAIRED NR 5 SLAT TRAILING EDGE WEDGE IAW B757 SRM 51- 70-10.
- [SDR USAA2012051400003](https://openairdocs.org/sdr/USAA2012051400003.md): Stringer · corroded · Apr 18, 2012 · N901AW · Boeing 7572S7 · Fuselage Main, Longeron/Stringer
  > C2 CHECK - CORROSION ON STRINGER AT BS 1455, S28L. REPAIRED STRINGER AT BS 1455, S28L IAW EA 103875.
- [SDR USAA2012040800003](https://openairdocs.org/sdr/USAA2012040800003.md): Latch · lack of lube · Apr 6, 2012 · N901AW · Boeing 7572S7 · Flight Compartment Equipment
  > F/O SEAT DIFFICULT TO KEEP LATCHED IN J TRACK. LUBED LATCH MECHANISM, OPS CHECK GOOD.
- [SDR USAA2012022000001](https://openairdocs.org/sdr/USAA2012022000001.md): Slide · failed · Feb 18, 2012 · N901AW · Boeing 7572S7 · Escape Slide
  > EVACUATION SLIDE ARMING LEVER FAILED TO MOVE AT SERVICE DOOR 4L. SLIDE PACK AND GIRT BAR UNROLLED. INSTALLED SLIDE PACK AND GIRT BAR. INSPECTED OK.
- [SDR USAA2011121200016](https://openairdocs.org/sdr/USAA2011121200016.md): Shade · stuck · Dec 11, 2011 · N901AW · Boeing 7572S7 · Passenger Compartment Equipment
  > PHX - 27F (EXIT ROW) WINDOW SHADE WILL NOT STAY UP. MAINTENANCE UNSTUCK AND RE-SECURED WINDOW SHADE AT 27F (EXIT ROW).
- [SDR USAA2011111800011](https://openairdocs.org/sdr/USAA2011111800011.md): Fan · inoperative · Nov 14, 2011 · N901AW · Boeing 7572S7 · Air Distribution Fan
  > PHX FLT 43 EN ROUTE DCA TO PHX. EICAS MSG R RECIR FAN INOP AND INOP LIGHT ILLUMINATED WITH SWITCH POSITIONED ON. STRONG SMELL OF BURNING ELECTRICAL. MAINTENANCE REMOVED AND REPLACED RT RECIRCULATION FAN.
- [SDR USAA2011092900010](https://openairdocs.org/sdr/USAA2011092900010.md): Skin · delaminated · Sep 28, 2011 · N901AW · Boeing 7572S7 · Leading Edge Devices
  > DAILY CHECK - NR 5 SLAT HAS DELAMINATION ON TRAILING EDGE WEDGE OF UPPER SURFACE AT SLAT STATION ISS220, 51 INCHES FROM OUTBOARD END. REPAIRED NR 5 SLAT IAW B757 SRM 51-70-10.
- [SDR USAA2011092900009](https://openairdocs.org/sdr/USAA2011092900009.md): Skin · delaminated · Sep 28, 2011 · N901AW · Boeing 7572S7 · Leading Edge Devices
  > DAILY CHECK - NR 5 SLAT HAS DELAMINATION ON TRAILING EDGE WEDGE MIDDLE OF UPPER SURFACE AT SLAT STA ISS155, 42 INCHES FROM INBOARD END. REPAIRED NR 5 SLAT IAW B757 SRM 51-70-10.
- [SDR USAA2011071200003](https://openairdocs.org/sdr/USAA2011071200003.md): Pump · inoperative · Jul 11, 2011 · N901AW · Boeing 7572S7 · Fuel Boost Pump
  > HNL - FLT 31 EN ROUTE OGG TO PHX. DURING CLIMBOUT FROM MAUI, RECIEVED A FUEL CONFIG WARNING DUE TO FUEL IMBALANCE. LEFT GAUGE REPORTED 12.0 AND RIGHT GAUGE REPORTED 14.3. PROGRESSIVE FUEL LEAK IN LEFT MAIN TANK. DIVERTED TO HNL WITHOUT FURTHER INCIDENT. MA
- [SDR USAA2011070500018](https://openairdocs.org/sdr/USAA2011070500018.md): Battery Pack · discharged · Jul 4, 2011 · N901AW · Boeing 7572S7 · Emergency Lighting
  > L-4 DOOR EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK.
- [SDR USAA2011020190482](https://openairdocs.org/sdr/USAA2011020190482.md): Wire · broken · Jan 28, 2011 · N901AW · Boeing 7572S7 · Light System Wiring
  > MCN - C1 - EEL - CABIN BULLNOSE EMERGENCY LIGHT ABOVE SEAT ROW 15R DOES NOT ILLUMINATE WHEN TESTED. REPAIRED BROKEN WIRE WITH NEW TERMINAL IAW B757 SWPM 20-30-11 AT SEAT ROW 15R, OPS CHECK GOOD IAW B757 AMM 33-51-05-2.

Next page: https://openairdocs.org/deregistered/N901AW-2017-05-08/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 = 'N901AW' AND deregistration_id = 'N901AW-2017-05-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N901AW-2017-05-08/reports

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