N910AW
Service difficulty reports · 157
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA20091203BB159Pin · unsecureSEA - EMERGENCY ESCAPE PATH LIGHT AT ROW 31 IS INOP. MAINTENANCE RE-SECURED PIN.SDR USAA2009120293288Strut · damagedPHX - LINE - MAJOR REPAIR - UPON DISASSEMBLY OF RIGHT MAIN LANDING GEAR STRUT FOR REPACK FOUND DAMAGE TO INNER BARREL & BROKEN PARTS / COMPONENTS OF INNER STRUT & PISTON. REPLACED RIGHT MAIN LANDING GEAR IAW JOB CARD R4M32607.SDR USAA2009090992416Slat · debondedPHX - OVERNIGHT - MAJOR REPAIR - NR 5 WING LEADING EDGE SLAT DISBONDED AND BREAKING OFF BETWEEN WS 125 TO WS 180. REPLACED NR 5 WING LEADING EDGE SLAT IAW B737 MM 27-81-01-401.SDR USAA20090824BB128Slide · low pressurePHX - THE R2 DOOR SLIDE INDICATES LOW PRESSURE. REPLACED THE R2 SLIDE ASSEMBLY.SDR USAA20090522BB090Circuit Breaker · failedPHX FLT 24 PHX TO LAX. EICAS MESSAGE TAT PROBE DISPLAYED, AND TAT PROBE HEAT LIGHT ILLUMINATED. REPLACED TAT PROBE HEATER CIRCUIT BREAKER (C4003).SDR USAA2009042991029Pin · not seatedMCN - C2 - EEL - EMERGENCY ESCAPE LIGHT AT SEAT 11L DOES NOT ILLUMINATE. RESEATED PINS IN MOLEX CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 11L.SDR USAA2009042991030Flashlight · inoperativeMCN - C2 - EEL - FLASHLIGHTS (2 EACH) INOP AT FORWARD ATTENDANT SEAT. REPLACED FLASHLIGHTS (2 EACH) AT FORWARD ATTENDANT SEAT.SDR USAA2009042090940Strap · crackedMCN - C2 - MAJOR REPAIR - CRACK ON MAIN DECK STABILIZER FLOOR STRAP AT BS 367, BL 0. REPAIRED MAIN DECK STABILIZER FLOOR STRAP AT BS 367, BL 0 IAW B757 SRM 53-10-51.SDR USAA2009042991026Rod · bentMCN - C2 - EES - L-4 DOOR FORWARD SLIDE ENGAGE ROD BENT. REPLACED ROD ASSEMBLY ON L-4 DOOR IAW B757 AMM 52-11-25-5.SDR USAA2009042991025Intercostal · crackedMCN - C2 - MAJOR REPAIR - TWO EACH CRACKS IN FLOORBEAM INTERCOSTAL UPPER ANGLE BETWEEN BS 860 TO BS 880, BL 0. REPLACED FLOORBEAM INTERCOSTAL UPPER ANGLE BETWEEN BS 860 TO BS 880, BL 0 IAW B757 SRM 51-40-02.SDR USAA2009042490977Skin · crackedMCN - C2 - MAJOR REPAIR - NR 1 PYLON SKIN CRACKED AT AFT OUTBOARD & INBOARD THRUST REVERSER FITTING UPPER AFT HOLE. REPAIRED NR 1 PYLON SKIN AT AFT OUTBOARD & INBOARD THRUST REVERSER FITTING UPPER AFT HOLE IAW US AIRWAYS EA 130245.SDR USAA2009042090939Plate · corrodedMCN - C2 - MAJOR REPAIR - CORROSION ON AFT CABIN DECK PLATE BETWEEN BS 1681 TO BS 1690, BETWEEN LBL 14 TO LBL 50. REPAIRED AFT CABIN DECK PLATE BETWEEN BS 1681 TO BS 1690, BETWEEN LBL 14 TO LBL 50 IAW B757 SRM 53-60-51 & 51-40-02.SDR USAA2009040990846Fitting · crackedMCN - C2 - MAJOR REPAIR - 3 CRACKS ON INTERCOSTAL CLIP BETWEEN BS 663 TO BS 672, BL 0. REPAIRED INTERCOSTAL CLIP BETWEEN BS 663 TO BS 672, BL 0 IAW B757 SRM 51-40-02, 53-00-51, & BOEING DRAWING 140N2505.SDR USAA2009040990845Fitting · crackedMCN - C2 - MAJOR REPAIR - 2 CRACKS ON INTERCOSTAL CLIP BETWEEN BS 793.5 TO BS 795, WL 208, BL 0. REPAIRED INTERCOSTAL CLIP BETWEEN BS 793.5 TO BS 795, WL 208, BL 0 IAW B757 SRM 51-40-02, 53-00-51, & BOEING DRAWING 140N2505.SDR USAA20090310BB048Contact · corrodedPHX - THE SLIDE ARMED LIGHT AT DOOR L2 WAS OPERATING INTERMITTENTLY. MAINTENANCE CLEANED THE CORROSION ON THE CONTACTS AND RELAMPED THE LIGHT. OPERATIONALLY CHECKS OK.SDR USAA20090302BB043Light · inoperativePHX - THE SLIDE LIGHT FOR THE L2 DOOR WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE SENSORS AND REPLACED THE BULBS FOR THE L2 DOOR SLIDE INDICATION LIGHT.SDR USAA20090209BB031Battery Pack · dischargedPHX - THE EMERGENCY LIGHTS AT POSITIONS TWO AND THREE ON LEFT BULLNOSE WERE FOUND INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONALLY CHECKS OK.SDR BB08102Charger · inoperativePHX - THE EMERGENCY SEAT LIGHTING WAS FOUND INOPERATIVE FROM ROWS 1 - 8. MAINTENANCE REPLACED THE BATTERY CHARGER FOR SEATS AT ROWS 1 - 8. OPERATIONALLY CHECKS OK.SDR USAABB08070Pump · malfunctionedHNL FLT 47 EN ROUTE LIH TO PHX. AIRCRAFT DISPLAYED EICAS MESSAGE "L ENG LP PUMP". THE CREW DECIDED TO DIVERT BACK TO HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE LP PUMP.SDR BB08070Warning System · activatedHNL FLT 47 - EN ROUTE LIH TO PHX. AIRCRAFT DISPLAYED EICAS MESSAGE "L ENG LP PUMP". THE CREW DECIDED TO DIVERT BACK TO HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. (OPEN)SDR BB08033Pressure Switch · failedHNL - FLT 9030 OGG TO PHX. DURING CLIMB, RECEIVED EICAS MESSAGE "L ENG LP PUMP", WITH A FUEL TEMP OF +35. FLIGHT DIVERTED TO HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED, INSPECTED, THEN REPLACED THE LEFT ENGINE LOW PRESSURE FUEL FILTER. ASDR USAABB08023Densitometer · faultyPHX FLT 22 PHX - HNL. WHILE IN CRUISE FLIGHT, THE CENTER TANK FUEL QUANTITY READINGS BECAME ERRATIC. FLIGHT RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CENTER FUEL TANK FUEL DENSITOMETER. OK FOR SERVICE.SDR BB08023Indicator · erraticPHX FLT NR 22 PHX - HNL WHILE IN CRUISE FLIGHT, THE CENTER TANK FUEL QTY READINGS BECAME ERRATIC. FLIGHT RETURNED TO PHX WITHOUT FURTHER INCIDENT.SDR BB08003Fuse · blownPHX - EMERGENCY LIGHTS INOP ROW 1 THRU 8. MAINTENANCE REPLACED FUSE. OPS CHECKS NORMAL.SDR BB07104Terminal · looseMAINTENANCE FOUND ROW 12L EMERGENCY LIGHT INOPERATIVE IN OVERHEAD BIN COVE. TIGHTENED LOOSE TERMINAL. NO FURTHER FAULTS.SDR AWXA200700593Charger · inoperativePHX - EEL - SEAT ROWS 1 THRU 20 EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED AFT EMERGENCY LIGHT BATTERY CHARGER IAW B757-200 AMM 33-51.SDR AWXA200601946Skin · damagedFUSELAGE BS 800 BETWEEN S14 AND S15L HAS TWO PLUGGED HOLES THAT WERE R/R THE SHEAR TIE UNDERNEATH. COUNTER SANK THE INNER SKIN AT BS 800 BETWEEN S-14L AND S-15L TO ACCOMODATE THE RIVETS BUTTON. PLUGGED THE TWO HOLES USING BACR15CE AND DOUBLE FLUSHED THE RIVESDR AWXA200601309Control Unit · out of toleranceTHE CREW ADVANCED THE NR 2 THRUST LEVER TO TAXI AND THE NR 2 ENGINE SHUT DOWN. EGT REACHED 620C. ENGINE SHUTDOWN WAS NOT INITIATED BY THE CREW. THE NR 2 ENGINE BLEED VALVE CONTROL UNIT DISPLAYED A VOLTAGE FAULT. MX REMOVED AND REPLACED THE NR 2 BLEED VALVESDR AWXA200600887Pin · burnedOGG - EEL - LG 7250100 & 7250101 - OVERHEAD EMERGENCY LIGHTS BETWEEN SEAT ROWS 4 AND 5 DO NOT ILLUMINATE ON GROUND TEST. M731 POWER SUPPLY BAD. OGG MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK IAW MM 33-51-07. AIRCRAFT WAS FERRIED BACK TO SDR AWXA200600814Connector · damagedPHX - FLT 7832 - DURING REPO FLIGHT CREW REPORTED THAT INBOUND TO PHX RECEIVED LEADING EDGE FLAP ASYMMETRY AND DISAGREE LIGHT. QRH PROCEDURES WERE FOLLOWED. LANDED IN PHX WITHOUT FURTHER EVENT. MAINTENANCE CHECKED WIRING BETWEEN FSEU 1, FSEU 2 AND RT SLATSDR AWXA200600805Transmitter · faultyHNL - FLT 920 - CREW REPORTED THAT AFTER SELECTING FLAPS 1 ON APPROACH INTO HNL, RECEIVED "LE SLAT DISAGREE" CAUTION MSG. CREW FOLLOWED QRH CHECK LIST AND THEN RECEIVED "LE SLAT ASYMMETRY" CAUTION MSG. CREW FOLLOWED QRH AND PERFORMED ALL FLAPS/SLATS UP LANDISDR AWXA200600759Battery Pack · overheatedGYR - EEL - NR 5919942 - DURING C12 CHECK DISCOVERED THE EMERGENCY LIGHTS BATTERY PACK, JUST AFT OF FWD ENTRY LIGHT, WAS OVERHEATING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW BOEING 757-200 AMM 33-51-07-2. OPERATIONAL CHECKS WERSDR AWXA200600795Channel · crackedGYR - DURING C12 CHECK DISCOVERED CHANNEL ASSEMBLY CRACKED ON THE L4 DOOR. MAINTENANCE REMOVED AND INSTALLED NEW L4 DOOR CHANNEL ASSEMBLY IAW BOEING 757-200 SRM 51-40-02-06 PAGE 8.SDR AWXA200600790Gate · corrodedGYR - DURING C12 CHECK DISCOVERED LEVEL 2 CORROSION ON THE R2 DOOR UPPER GATE HINGE AREA, ALONG FULL LENGTH. MAINTENANCE REMOVED AND INSTALLED NEW UPPER GATE IAW MM 52-11-38-4. GATE WAS ADJUSTED IAW MM 52-11-00-5.SDR AWXA200600749Attach Fitting · galledDURING C12 CHECK DISCOVERED RT WING INBOARD STRUT ATTACH FITTING FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 248R. MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RC2SDR AWXA200600748Attach Fitting · galledDURING C12 CHECK DISCOVERED RT WING OUTBOARD STRUT ATTACH FITTING LUGS FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 263R . MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06SDR AWXA200600648Shim · migratedGYR - DURING C12 CHECK DISCOVERED NR 1 PYLON DIAGONAL BRACE FITTING SHIMS MIGRATING LEFT SHIM HORIZONTAL MOVEMENT 0.400 INCHES AND VERTICAL MOVEMENT 0.900 INCHES. MAINTENANCE REPAIRED PER AWA ER 19-5453-06060-BA1 AND BOEING SB 757-54-0035 FIG. 21, STEPS 8, 12SDR AWXA200600647Shim · migratedGYR - DURING C12 CHECK DISCOVERED NR 2 ENGINE PYLON DIAGONAL BRACE ATTACH FITTING VERTICAL SHIMS MIGRATED LT 0.200 INCHES AND R/H 0.030 INCHES. MAINTENANCE REMOVED AND REPLACED LEFT AND RIGHT DIAGONAL BRACE ATTACH FITTING SHIMS PER AWA ER 19-5453-06060-BA1.SDR AWXA200600750Attach Fitting · galledDURING C12 CHECK DISCOVERED LT WING OUTBOARD STRUT ATTACH FITTING FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 263L. MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RCSDR AWXA200600747Attach Fitting · galledDURING C12 CHECK DISCOVERED LUG SURFACES GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LEFT WING INBOARD STRUT ATTACH FITTING FOR PYLON AT WBL 248L. MAINTENANCE REMOVED INBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704SDR AWXA200600664Floorbeam · corrodedGYR - DURING C12 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE MAIN CABIN FLOORBEAM UPPER EDGE AT BS 365 FROM BL 15R TO BL 35R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 757-200 SRM 53-00-51-2A. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA IAWSDR AWXA200600616Floorbeam · corrodedGYR - DURING C12 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 740 FROM BL 45.5R TO BL 55.5R, WL 208. MAINTENANCE CUT OUT DAMAGED AREA AT BS 740 BL 45.5R IAW SRM 53-00-51-2R. CORROSION FOUND TO BE OUT OF SRM LIMITS. FABRICATED REPAIR ANGLESDR AWXA200600789Support · corrodedGYR - DURING C12 CHECK DISCOVERED LEVEL 2 CORROSION ON FASTENER HOLE AT BOTTOM SURFACE OF FLOOR PANEL SUPPORT ANGLE AT BL 60R AND BS 684.5. CORROSION WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOOR PANEL SUPPORT ANGLE AT BL 60R AND BS 684.5.SDR AWXA200600712Web · corrodedGYR - DURING C12 CHECK DISCOVERED CORROSION, LEVEL 2 INTERGRANULAR, ON R3 LOWER DOOR EMERGENCY LOWER WEB FROM BS 1340 TO BS 1360, WL 208.1, STR 17R, FROM BL 70R TO BL 79R. MAINTENANCE REMOVED CORROSION FROM WEB LOWER SIDE FROM BS 1340 TO BS 1360, WL 208.1, STSDR AWXA200600711Web · corrodedGYR - DURING C12 CHECK DISCOVERED CORROSION, LEVEL 2 INTERGRANULAR, ON L3 DOOR EMERGENCY LOWER WEB FROM BS 1340 TO BS 1360 AT STR 17L. MAINTENANCE REMOVED CORROSION FROM LOWER WEB FROM BS 1340 TO BS 1360 AT STR 176 IAW BOEING 757-200 SRM 51-10-02. CORROSION SDR AWXA200600752Floorbeam · crackedDURING C12 CHECK DISCOVERED FLOORBEAM CRACKED IN TWO PLACES AT BS 700, ONE CRACK AT BL 24R AND THE OTHER AT BL 46R. EACH CRACK WAS APPROXIMATELY 1 INCH LONG. MAINTENANCE CUT OUT DAMAGED AREA. FABRICATED SUPPORT ANGLES, REINFORCEMENT STRAPS, AND FILLER IAW ASDR AWXA200600751Skin · delaminatedDURING C12 CHECK DISCOVERED 2 SQUARE INCH AREA OF DELAMINATION ON THE UPPER SURFACE OF THE NR 8 SLAT, TRAILING EDGE WEDGE AT THE INBOARD END AT WBL 440R. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 757-200 SRM 51-70-10-2R. FABRICATED FILLER AND DOUBLER IAW BSDR AWXA200600653Wedge · delaminatedGYR - DURING C12 CHECK DISCOVERED ONE SQUARE INCH DELAMINATION AREA ON TOP SURFACE OF NR 7 L/E SLAT 28 INCHES FROM OB EDGE. MAINTENANCE CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER. BONDED FABRICATED PARTS TO TOP SURFACE OF NR 7 L/E SLAT 28 INCHES FRSDR AWXA200501375Light · inoperativeSEA - EEL - DURING OVERNIGHT INSPECTION, DISCOVERED EMERGENCY PATHWAY LIGHT AT ROW 23, LEFT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 23L. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200600252Skin · delaminatedPHX - DISCOVERED THE LT INBOARD FLAP DELAMINATING, 20.5" BY 17.5", ADJACENT TO AND UNDERNEATH THE NR 5 SPOILER PANEL. MAINTENANCE REMOVED DELAMINATED CORE AND INNER SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5753-05275-HF1. FABRICATED FILLER AND
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