N453AS
Service difficulty reports · 284
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 = 'N453AS' 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 = 'N453AS' 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 ASAA2026082668309Door · lack of lubeFA REPORTS L1 DOOR IS DIFFICULT TO OPERATE. GROUNDED - YES. L1 DOOR SYSTEM TEST FOUND CLOSE TORQUE TO BE 600 IN-LB AND WITHIN LIMITS, OPEN TORQUE FOUND TO BE 445 IN-LB AND OUT OF UPPER LIMIT REF AMM 52-11-00. LUBRICATED L-1 DOOR COMPONENTS REF AMM 12-25-11-640SDR ASAA2026081668058Door · bindingFA SAYS THE L1 DOOR IS STICKY, HARD TO OPEN AND CLOSE. GROUNDED - YES. CHECKED L1 DOOR HANDLE TORQUE REF AMM 52-11-00, WELL W/IN LIMITS, HAD INCOMING FLIGHT CREW OPERATE DOOR MULTIPLE TIMES, NO PROBLEMS, NO HISTORY 30 DAYS.SDR ASAA2026061966861Track · lack of lubeFA REPORTS L1 DOOR IS VERY STIFF TO OPEN & HAS A SQUEAK. GROUNDED - YES. LUBRICATED HINGE POINTS. TRACKS FOR L1 DOOR. OPERABILITY HAS VERY MUCH IMPROVED AND SQUEAK HAS DIMINISHED & IMPROVING WITH OPERATION OF DOOR. REF AMM 12-25-11.SDR ASAA2026042665733Door · bindingFA REPORTS L1 DOOR HANGS UP AND MAKES A GROANING NOISE DURING OPENING AND CLOSING. GROUNDED - YES. INSPECTED DOOR, SOUND APPEARS TO BE ORIGINATING FROM TOP HINGE, NO OTHER DEFECTS NOTED. LUBRICATED UPPER HINGE, ROLLERS AND TRACKS, NOISE MINIMIZED, ONLY NOTABLESDR ASAA2026032965213Handle · no discrepancyFA REPORTS L1 DOOR HANDLE STIFF TO OPEN. GROUNDED - YES. PERFORMED OPERATIONAL CHECK OF L1 DOOR REF AMM 52-11-00 OPERATIONAL CHECK NORMAL . NO DEFECTS NOTED AT THIS TIME.SDR ASAA2026021164305Door · bindingFA REPORTED THAT L1 DOOR WAS EXTREMELY HARD TO OPEN AND CLOSE. GROUNDED - YES. L1 DOOR CLOSURE AND OPENING ARTICULATION MID-SEQUENCE STIFFENS/ DRAGS HARD DOOR CLOSING AND LATCHING WITHIN LIMITS REF AMM 52-11-00-00-804. PERFORMED FORWARD ENTRY DOOR CHECK REF AMSDR ASAA2025111362362Handle · bindingL1 DOOR HANDLE IS REPORTED HARD TO MOVE. GROUNDED - YES. VERIFIED FORCE ON L1 DOOR INNER HANDLE REQUIRED TO OPEN AND CLOSE DOOR TO BE WITHIN LIMITS REF. MM. 52-11-00.SDR ASAA2025060358425Sign · detachedEXIT SIGN HANGING FROM CEILING. GROUNDED - YES. EXIT SIGN WAS MID CABIC CENTER AISLE CEILING. RESECURED SIGN - SIGN OPS CHECK GOOD. NO OTHER DEFECTS NOTED.SDR ASAA2025042558150Floor Support · corrodedIN FWD GALLEY FLOOR STRUCTURE HAS AN AREA OF CORROSION IN FLOOR PANEL SCREW HOLE, JUST AFT OF STA 294.5 & LBL 10 INCHES. MARKED IN RED. GROUNDED - YES. DISPLACED CABLES MLGEA-L AND EA-L AND EB-L IAW B737-900 AMM 20-10-91. RECONNECTED AND ADJUSTED CABLE MLGEA-LSDR ASAA2025042557896Floor Panel · delaminatedCABIN FLOOR PANEL 141A5810-155 HAS PEELING FIBERS & DAMAGED INSERTS. GROUNDED - YES. REPAIRED CABIN FLOOR PANEL 141A5810-155 BY PREFORMING A PERMANENT WET LAY UP REPAIR IAW B737-900ER SRM 53-00-50-2R-0.SDR ASAA2025042557895Floor Panel · delaminatedCABIN FLOOR PANEL 141A5810-763 HAS PEELING FIBERS & DAMAGED INSERTS. GROUNDED - YES. REPAIRED CABIN FLOOR PANEL 141A5810-763 BY PERFORMING A PERMANENT WET LAY UP REPAIR IAW B737-900ER SRM 53-00-50-2R-0.SDR ASAA2025042557836Floor Panel · delaminatedCABIN FLOOR PANEL 141A5810-236 HAS PEELING FIBERS & DAMAGED INSERTS. GROUNDED - YES. REPAIRED CABIN FLOOR PANEL 141A5810-236 BY PREFORMING A PERMANENT WET LAY UP REPAIR IAW B737-900ER SRM 53-00-50-2R-0.SDR ASAA2025042457912Transition Panel · corrodedTRANSITION PANEL STATION 500C - 500D +8 RBL 24 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM TRANSITION PNL AT STA 500C TO 500D+8 RBL 24 ORIGINAL THICKNESS IS .040 IAW B737-900 SRM 53-30-53-01-2. MAT LOSS .010 REMAINING THICKNESS .030. FOUND TO BE OUT SDR ASAA2025042457894Threshold Web · corrodedCORROSION ON THE LOWER PORTION OF THE FORWARD CARGO DOOR CUTOUT. GROUNDED - YES. EVALUATED FWD PIT DOOR WEB THRESHOLD AND FOUND TO BE 100% MAT LOSS AND FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-30-15-1A-1. RECEIVED NEW WEB THRESHOLD PN#143A8122-10 PO: 1120SDR ASAA2025042457697Floor Support · gougedFWD WET AREA INTERCOSTAL AT STA 278 TO STA 294.5 BL 0 HAS GOUGE ON LOWER SURFACE OF UPPER FLANGE. GROUNDED - YES. BLENDED AND CHECKED LIMITS @ INTERCOSTAL AREA ORI MAT .040, MAT. LOSS .021,REMAINING MAT .019 FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-10-51-SDR ASAA2025042457696Floor Support · crackedFWD WET AREA STA 312 TO STA 328 LBL 45 HAS A CRACKED INTERCOSTAL. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW B737-900 SRM 51-40-02 AND BAC DWG 141A5400.SDR ASAA2025042358151Transition Panel · corrodedAFT CARGO TRANSITION PANEL AT STA.787 TO STA.727I+9 LBL.22 CORRODED. GROUNDED - YES. REMOVED AND INSTALLED WITH NEW AFT CARGO TRANSITION PNL AND SPLICES AT STA. 727I+9 LBL.22 TO STA. 787 IAW B737-900 SRM 53-00-53. REMOVED CORR. FROM TRANS PNL AT 727I+9 LBL.22 SDR ASAA2025042358120Threshold Web · corrodedAFT CARGO DOOR THRESHOLD CORRODED. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT THRESHOLD IAW B737-900 SRM 53-60-15-01-1. ORIGINAL MAT IS .045. MAT LOSS IS .005. MAT REMAINING IS .040. FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-60-15-1A-1. RECEIVED NEW THSDR ASAA2025042358119Transition Panel · corrodedAFT CARGO TRANSITION PANEL AT STA.767 TO STA.787 RBL.22 CORRODED. GROUNDED - YES. REMOVED CORR, FROM AFT CARGO TRANSITION SHIELD AT STA 767 TO 787 RBL.22 ORIG. THICKNESS .045 I.A.W. B737-900 SRM 53-60-15 MAT. LOSSED 100% FOUND TO BE OUT OF LIMITS I.A.W. B737-9SDR ASAA2025042357917Floorbeam · corrodedSTA 947 UPPER T-CAP HAS AREAS OF CORROSION FROM LBL 15 TO RBL 4. GROUNDED - YES. REMOVED DAMAGE AND FOUND OUT OF LIMITS I.A.W. B737-900ER SRM 53-70-51-1A-1, ORIGINAL THICKNESS OF UPPER FLANGES .180, MAT REMOVED .080, MAT REMAINING .100 I.A.W. B737-900ER SRM 53SDR ASAA2025042357916Support Angle · corrodedAFT CARGO TRANSITION PANEL SUPPORT STRUCTURE AT STA. 767 TO STA. 787 RBL.22 CORRODED. GROUNDED - YES. REMOVED AND REINSTALLED WITH NEW AFT CARGO TRANSITION PNL SUPPORT ANGLE. REMOVED CORR. FROM SUPPORT ANGLE ORIG THICKNESS .040 I.A.W. B737-900 SRM 53-60-15, 10SDR ASAA2025042357915Transition Panel · corrodedAFT CARGO TRANSITION PANEL AT STA. 727I+9 TO STA. 727A LBL .22 CORRODED. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727A-727I+9 LBL 22 IAW B737-900 SRM 53-00-53-1A-2.2.D, 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW B737-900SDR ASAA2025042357914Transition Panel · corrodedAFT CARGO TRANSITION PANEL AT STA. 727I+9 TO STA. 727B RBL.22 CORRODED. GROUNDED - YES. REPAIRED AFT PIT R/H TRANSITION PANEL IAW B737-900 SRM 53-00-53-2R-5. EVALUATED IAW B737-900 SRM 53-00-53-1A-2. ORIG: .040 REMOVED:100% MAT LOSS AND IS FOUND TO BE OUT OF LSDR ASAA2025042357913Floor Support · corrodedAFT WET AREA FLOOR SUPPORT ANGLE AT STA 950 LBL 23 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE PER B737-900ER SRM 51-10-02 ORIG .080 REMOVED .035, REMAINING .045 FOUND OUT OF LIMITS PER B737-900ER SRM 53-70-51-1A-1 REMOVED FLOOR SUPPORT ANGLE IAW B737-900ER SDR ASAA2025042357911Transition Panel · corrodedAFT CARGO TRANSITION PANEL AT STA. 767 TO STA. 727I+9 RBL.22 CORRODED. GROUNDED - YES. EVALUATED AFT PIT R/H TRANSITION PANEL FROM STA 767-727I+9 ORIG:.040 REMOVED:.005 REMAINING: .035 & IS FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A & SRM 53-60-53-SDR ASAA2025021556026Lens · missingDURING CABIN INSPECTION FOUND TWO EMER CEILING LIGHT COVERS MISSING. GROUNDED - YES. REPLACED MISSING EMER CEILING LIGHT COVERS REF AMM 33-51-03.SDR ASAA2024082652128Door · bindingFWD L1 DOOR HARD TO OPEN PER 'A' FLIGHT ATTENDANT. GROUNDED - YES. PERFORMED GVI OF L1 DOOR NOT DEFECTS NOTED. GREASED DOOR HINGES, DOOR OPENS & CLOSES NORMAL. OK FOR SERVICE.SDR ASAA2024080651626Power Supply · inoperativeEMERGENCY LIGHT INOP OVER SEAT 27D. GROUNDED - YES. (RESOLVED ON W/O: 2011124 TASKCARD: N/R-00004 ) REMOVED & REPLACED EMERGENCY LIGHT POWER SUPPLY M2627 FOR E LIGHT AT 27ABC, OP TEST OK. CLEARS MEL 33-15D. PLACARD REMOVED.SDR ASAA2024050649484Sign · dislodgedMID CABIN EXIT SIGN WAS PARTIALLY DISLOGED. GROUNDED - YES. RESECURED EXIT SIGN.OP'S CKIS GOOD. REF AMM 33-51-01.SDR ASAA2024042649287Battery Pack · failedWHILE PERFORMING T/C 778233001, FOUND BATTERY PACKS FOR EMERGENCY LIGHTS REQUIRE REPLACEMENT IN: FWD ENTRY (2), MID CABIN (4), AND AFT ENTRY (1). GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS, 2 IN FWD ENTRY, 4 IN MID CABIN, 1 IN AFT ENTRSDR ASAA2024012747526Lens · brokenAFT OVERHEAD EMERGENCY EXIT LIGHT BROKEN. GROUNDED - YES. SWAPPED LENS'S ORANGE WITH PINK AND OPS CKS NORMAL PER OPS TEST AMM 33-51-00.SDR ASAA2023110846073Modulating Valve · faultyCONT CAB ZONE TEMP LIGHT ILLUMINATED UPON RECALL IT DOES RE-SET. GROUNDED - YES. (RESOLVED ON W/O: 1976139 TASKCARD: N/R-00004 ) CONFIRMED FAULT, #2 PACK/ZONE TEMP CONTROLLER SHOWS HARD FAIL "FLIGHT DECK TCV" FAULT. REMOVED & REPLACED V143 TCV REF AMM 21-61-21SDR ASAA2023110746066Unknown · unknownDURING START OF #1 ENGINE, THE ENG VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE AND DID NOT EXTINGUISH AFTER SUCCESSFUL START. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023110246024Unknown · unknownLAV WASTE SHOWED FULL AFTER LEVEL OFF IN CRUISE. NO TOILETS WOULD FLUSH. GROUNDED - YES. DIVERSION - PERFORMED WASTE TANK CONTINUOUS LEVEL SENSOR CLEANING PER AMM 38-33-02. INSPECTED BALL VALVE LINKAGE ASSEMBLY AND PROXIMITY SWITCH WITH NO DEFECTS NOTED. VERIFSDR ASAA2023103045925Indicator · leakingAPU LUBE FILTER HOUSING,FILTER INDICATOR LEAKING. GROUNDED - YES. REMOVED AND REPLACED APU INDICATOR LUBE FILTER HOUSING,OIL FILTER,INDICATOR & AND HOUSING ASSY REF MM 49-91-13-400-802.OPS,LEAK CHECK GOOD.SDR ASAA2023102645878Unknown · unknownFAULT LIGHT TRYING TO START APU. ACCOMPLISHED THE QRH AND TRIED AGAIN. BUT GOT THE FAULT LIGHT AGAIN. (ON GROUND). GROUNDED - YES. ON DEFERRAL.SDR ASAA2023102645865Unknown · unknown#2 ENGINE LONG TIME FAULT. THE VSV POSITION SIGNAL IS OUT OF RANGE. FAULT CODE 75-10392. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023102645864Unknown · unknown#2 ENGINE SHORT TIME FAULT. THE VSV POSITION SIGNALS DISAGREE. FAULT CODE 75-10402. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023102645863Unknown · unknown#2 ENGINE SHORT TIME FAULT. THE VSV POSITION SIGNALS DISAGREE. FAULT CODE 75-20402. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023102345815Unknown · unknownAPU FAULT LIGHT, 2 START ATTEMPTS. GROUNDED - YES. PERFORMED APU OPERATIONAL TEST REF AMM 49-11-00-710-801. FOUND FAULT MAINTENANCE MESSAGE 49-41012 WHILE COMPLETING FIM 49-60 TASK 801. PER MAINTENANCE MESSAGE CHART, FIM TASK 49-40 TASK 803 IS REQUIRED FOR FAUSDR ASAA2023101745708Unknown · unknownDESCENDING THROUGH 3,500' ENG VALVE CLOSED BLUE LIGHT ILLUMINATED. #1ENG. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023101745717Unknown · unknownON MASTER CAUTION RECALL CONT CAB ZONE TEMP ILLUMINATED. LIGHT EXTINGUISHED WHEN MASTER CAUTION SYATEM RESET. GROUNDED - YES. PERFORMED PZTC BITE PROC. FIM 21-62 TASK 801, R/H FLT DECK TRIM VALVE FAULT ON BIT, PREV FLIGHT AND CLEARED ON VERIFY. ACCOMPLISHED BISDR ASAA2023092445305Unknown · unknown#1 "ENGINE VALVE CLOSED" LIGHT CAME ON AFTER ROTATION. EXTINGUISHED APPROACHING 10,000 FT IN CLIMB. ALL OTHER INDICATIONS WERE NORMAL TO INCLUDE FUEL FLOW. GROUNDED - YES. PERFORMED B737-900 FIM 73-06 TASK 805, NO FAULT NOTED. START AND RAN #1 ENG, NO FAULT NOSDR ASAA2023090845017Unknown · unknownLEFT PACK LIGHT ILLUMINATES DURING RECALL. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023090444943Unknown · unknown#1 ENG PACK LIGHT ILLUMINATED WHILE TAXING OUT ON RECALL. GROUNDED - YES. (RESOLVED ON W/O: 1968004 TASKCARD: N/R-00005 ) ACCOMPLISHED PZTC BITE PROCEDURE REF. FIM 21-62 TASK 801. NO FAULTS ACTIVE OR IN HISTORY. PACK/ZONE TEMPERATURE CONTROLLER BITE TEST NORMASDR ASAA2023082944829Unknown · unknownFIRE LOOP B #2 ENG WILL NOT ILLUMINATE (TEST). GROUNDED - YES. ON DEFERRAL.SDR ASAA2023081444607Unknown · unknownHF 1 ON RADIO TUNING PANEL INDICATING FAIL - FAIL. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023081444599Unknown · unknownFORWARD LOWER COFFEE MAKER LEAKING WATER ONTO GALLEY FLOOR IN FLIGHT. LEAK UNCONTROLLABLE WITH VALVE TURNED OFF. GROUNDED - YES. DIVERSION -- REF: L/P #60571445. UPON ARRIVAL TO A/C NO LIQUID ON FLOOR. OPENED ALL FWD GALLEY CABINETS VERIFIED ALL DRY NO LIQUID SDR ASAA2023081144576Support · excess playTHE #2 ENGINE HAS SHORT TIME FAULT 75-20402, THE VSV POSITION SIGNALS DISAGREE. GROUNDED - YES. #2 ENGINE VSV "B" ACTUATOR BELL CRANK HAS EXCESSIVE PLAY. (R/H SIDE) REPLACED R/H VSV ACTUATOR BELLCRANK ASSY PER AMM 72-32-00-900-805. OPS TEST GOOD.SDR ASAA2023081144573Bellcrank · excess play#2 ENGINE HAS SHORT TIME FAULT 75-10402, THE VSV POSITION SIGNALS DISAGREE. GROUNDED - YES. #2 ENGINE VSV "B" ACTUATOR BELL CRANK HAS EXESSIVE PLAY. (L/H SIDE) REPLACED LH VSV BELL CRANK ASSY PER AMM 72-32-00-900-805. OPS TEST GOOD MIG 2C 40-0047291 COMPLETED
Back to N453AS