N1361A
Service difficulty reports · 445
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 = 'N1361A' 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 = 'N1361A' 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 ABXA20260926438Fire Warning · false activationMAIN CARGO FIRE WARNING GOING ON AND OFF. PERFORMED MAIN CARGO INSPECTION IAW AMM 26-14-00 NO FIRE OR SMOKE NOTED PERFORMED FIRE WARNING OPS CHECK IAW AMM 26-14-00, OPS CHKD GOOD ACFT REMAINS ETOPS 180. ACFT RETURNED TO SERVICE.SDR ABXA20260914403Fire Detector · false activationHAD MAIN CARGO FIRE BELL/ LIGHTS, NO SMOKE OR FIRE, QRH COMPLETED, EXTERIOR INSPECTION OPS NORM, FIRE RESCUE WILL INSPECT WITH IR CAMERA. PERFORMED CARGO COMPARTMENT INSP PER AMM 26-00-00, NO FIRE OR SMOKE NOTED, A/C OK TO CONTINUE.SDR ABXA20260810352Oxygen Bottle · low pressureDURING CREW PREDEPARTURE CHECK, EICAS PRESSURE INDICATION INOP READING 40 PSI. DEFERRED EICAS O2 PRESSOR INDICATION PER MEL 35-11-2-1 MX PROCEDURES COMPLY WITH PLACARD INSTALLED RE-INSPECT O2 PRESSURE BEFORE EA FLIGHT MUST BE COMPLY BY AUG 13, 2026. A/C RETURNSDR ABXA20260807351Elec Connector · defectiveON PREDEPARTURE CHECK EICAS OXYGEN PRESS READS 40 PSI BOTTLE 1. ACTUAL READINGS BOTTLE #1 1850 PSI BOTTLE #2 1450 PSI. DEFERRED CREW BOTTLE #1 EICAS INDICATION IAW ABX MEL 35-11-2-1 VERIFIED O2 BOTTLES OPEN MX ACTIONS C/W, PLACARD INSTALLED. VERIFY PRESSURE ABSDR ABXA20260729338Warning Message · false activationLEFT ENG BLEED OFF EICAS MSG AFTER STARTING #1 ENGINE. ACCOMPLISHED 227 NNC AND ADVANCED THRUST TO 78% N2 DID NOT RESOLVE THE ISSUE. CREW RETURNED TO THE GATE (BTB). MTC PERFORMED AIR SUPPLY BITE IAW B767 AMM 36-11-00 NO FAULTS NOTED AT THIS TIME L ENG BLEED OSDR ABXA20260622283Flap System · warning messageTRAILING EDGE FLAP DISAGREE DISPLAYED 5 TIMES DURING THE TAXI TO TAKEOFF AND THEN WENT AWAY. CREW ABORTED TAKEOFF (ATO) AND CONFERENCED WITH THE FOO AND MX. CAPTAIN OK TO CONTINUE FLIGHT SINCE MESSAGE WASN'T PRESENT BEFORE TAKING OFF. ACFT RETURNED TO SERVICE SDR ABXA20260620270Fseu · malfunctionedDURING TAXI OUT TO TAKE OFF T/E DISAGREE KEPT POPPING UP AND A/C RETURNED TO THE GATE AND MTX GROUNDED A/C . AFTER TROUBLR SHOOTING REMOVED AND REPLACED FSEU IAW AMM 27-51-01OPS CHECK GOOD NO FAULTS NOTED AT THIS TIME AND RETURNED A/C TO SERVICE.SDR ABXA20260516211Generator · inoperativeON T/O, RT GEN OFF ON THRUST ADVANCE. CREW DEFERRED IAW 24-00-1-1 AND PERFORMED AN ABORTED TAKE OFF (ATO). MTC DEFERRED PER MEL 24-00-1-1 MX PROCEDURES C/W PLACARD INSTALLED. A/C DOWNGRADED TO ETOPS 120. ACFT RETURNED TO SERVICE.SDR ABXA20260502183Smoke Detector · false activationBATHROOM SMOKE DETECTOR WENT OFF TWICE IN FLIGHT NO EICAS OR OTHER INDICATION OF FIRE.AFTER LANDING DEFERRED LAVATORY SMOKE DETECTION SYSTEM IAW ABX MEL 26-26-3-2 MX ACTIONS C/W PLACARD INSTALLED MBCB 08-30-2026. AND RETURNED A/C TO SERVICE.SDR ABXA20260404145Fire Warning · false activationMAIN CARGO FIRE MSG, MTX GROUNDED ACFT AND VERIFIED NO FIRE, PERFORMED OPS CHECK AND FOUND GOOD IAW AMM 26-14-00, ACFT REMAINS ETOPS 180. AND RETURNED ACFT TO SERVICE.SDR ABXA20260330138Altimeter · faultedON APPROACH, GEAR NOT DOWN EICAS AND BELL AT 2500 FEET FOLLOWED BY LAND 2 NO LAND 3 ON ASA. ACCOMPLISHED LAST FLIGHT FAULTS ON MCDP AND RADIO ALTIMETER TESTS IAW B767 AMM 22-00-02 AND 34-33 FAULT TREE 810, NO DEFECTS NOTED AT THIS TIME, AC DOWNGRADED TO CATI SDR ABXA20260327134Radio Altimeter · faultedDURING DESCENT, GEAR NOT DOWN RED EICAS MESSAGE CAME ON AROUND 5000FT ON THE ARRIVAL WITH FLAPS SET AT 1 SEVERAL TIMES WITH THROTTLES AT IDLE. C/W 30/40 TEST NO FAULTS NOTED, MCDP FLIGHT REPORT FLAGGED L-RADIO ALTIMETER DEFERRED PER MEL 34-33-01-2A-1. MAINTENASDR ABXA20260318113Starter · defectiveDURING ENGINE START, L ENG STARTER EICAS MESSAGE, UNABLE TO START NO. 1 ENGINE, NO N2. AIRCRAFT RETURNED TO BLOCKS (BTB). T/S #1 ENG STARTER IAW B767 FIM 80-11 FT 805. REMOVED AND REPLACED #1 ENG STARTER IAW B767 AMM 80-11-02. OPS CHECK #1 ENG IAW B767 AMM 7SDR ABXA20251231364Anti-Ice Valve · faultedDURING TAXI OUT, AFTER L ENG START EICAS MESSAGE L ENG ANTI-ICE VALVE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED AND REPLACED L ENG TAI VALVE IAW AMM 30-21-03. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. A/C REMAINS ETOPS 180. AIRCRAFT RETURSDR ABXA20250918232A/C Pack · warning messageON TAXI OUT, L PACK TEMP EICAS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED L PACK PER MEL 21-51-1-1. MTX PROCEDURES CW. PLACARD INSTALLED. AC RELEASED NO ETOPS. A/C RETURNED TO SERVICE.SDR ABXA2025622134Pitot Head · defectiveDURING TAXI, F/O'S PITOT LIGHT PROBE NOT WORKING. AIRCRAFT RETURNED TO BLOCKS. (BTB). REMOVED AND REPLACED THE F/O'S PITOT PROBE IAW B767 AMM 54-11-01. OPS CHECK GOOD. PERFORMED LEAK CHECK OF SYS IAW B767 AMM 34-11-00. OPS AND LEAK CHECK GOOD. AIRCRAFT RSDR ABXA20250407071Module · malfunctionedON TAKEOFF, RIGHT N1 DID NOT ADVANCE MORE THAN 60%. RH ENG NOT MAKING TAKEOFF PWR. ABORTED TAKEOFF, RETURNED TO BLOCKS (BTB). PERFORMED B767 FIM 71-01 FT 810 (R) PIMU BITE, PIMU FLAGGED EEC/PIMU MODE DISAGREE FAULT. PERFORMED CONTINUITY CHECK FROM EEC TO (RSDR ABXA20250116013Warning Message · false activationAFTER BLOCKOUT AND BOTH ENGINES RUNNING AFT CABIN TEMP FWD CABIN TEMP, FLT DECK TEMP EICAS MESSAGES DISPLAYED WITH DISCRETE LIGHTS ILLUMINATE.AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC MTX EXECUTED BITE TEST OF ZONE TEMP CONTROLLER IAW FIM 21-61 FAULT TREE SDR ABXA20241207246Iru · failedAFTER PUSHBACK R IRS ALIGN EICAS AND DISCRETE LIGHT ILLUMINATED. PERFORMED QUICK ALIGN AND STATUS DID NOT CHANGE. AIIRCRAFT RETURNED TO GATE. MAINTENANCE GROUNDED AIRCRAFT. TRIED NEW CENTER IRU, NO HELP. WAPPED RIGHT & CENTER SYMBOL GENERATOR, NO HELP. ALL UNISDR ABXA20241102211Steering Sys · no discrepancyTUG DRIVER OVERTORQUED NOSE GEAR ON PUSH BACK AC RETURNED TO THE GATE AND MTX GROUNDED AC . MTX EXECUTED A PHASE 1 CONDITIONAL INSPECTION OF THE NLG STEERING SYSTEM IAW B767 AMM 05-51-29 NO DEFECTS NOTED @ THIS TIME. AND MTX RETURNED AC TO SERVICE.SDR UIEA2024072200713Hydraulic Line · tornTORN HYDRAULIC LINE TRUCK POSITIONER LEFT MAIN LANDING GEAR(<P>HYDRAULIC LINE TRUCK POSITIONER LEFT MAIN LANDING GEAR WAS REPLACED IAW AMM 32-32-18-404-024 REV 142 22-APR- -2024 TORQUE 170 LB IN S/N 224110689 DATE 02-FEB-2025. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072200714Rod · wornLH WING, INNER ACCESS PANEL 521QB, OUTBD REFUEL COUPLING, BEARING ROD ASSY WITH WORN(<P>LH WING INNER ACCESS PANEL 521QB OUTBD REFUEL COUPLING ROD WAS REPLACED IAW AMM 28-21-01-404-010 REV 142 22APR2024 TORQUE APPLIED 100LB-IN TORQUE N/S=0524121894EB-2025. NO SDR UIEA2024072200715Chain · missingLH WING, INNER ACCESS PANEL 521QB, ON BOTH REFUEL COUPLINGS, CHAINS MISSING(<P>THE CAPS ASSY OF REFUEL COUPLINGS WERE REPLACED IAW AMM 28-21-01-404-010 REV:142 22/APR/2024. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072200716Brake Pads · wornNOSE LANDING GEAR WHEEL WELL, WEAR ON LEFT AND RIGHT SPIN BRAKES (PADS).(<P>NOSE LANDING GEAR WHEEL WELL, LEFT AND RIGHT SPIN BRAKES (PADS) WERE REPLACED IAW AMM 32-45-05-422-007 REV 142 DATE 22 APR 24. TORQUE APPLIED 35 LBIN S/N 0423902837 DATE 24 OCT 24. GOOSDR UIEA2024072200717Placard · damagedLOWER FUSELAGE EXTERNAL SKIN, ILLEGIBLE LABELS ON EMERGENCY ACCESS HANDLE OF RH COCKPIT WINDOW #2.(<P>LOWER FUSELAGE EXTERNAL SKIN, ON EMERGENCY ACCESS HANDLE OF RH COCKPIT WINDOW #2. LABELS WAS INSTALLED CORRECTLY IAW AMM 20-10-12-404-004 REV. 142 DATE 22 APRSDR UIEA2024072300732Access Panel · leakingRH WING, ACCESS PANEL 641BB, BASE OF FUEL STICK WITH LEAK(<P>RH WING, ACCESS PANEL 641BB, BASE OF FUEL STICK WAS REPLACED IAW AMM 28-44-01-404-033 REV 142 22-APR-24 ,</P> / <P>BONDING: 01 MILLIOHMS / SERIAL BONDING: 1534 / DATE EXP: 22-ENE-25, INSTALATION OF PSDR UIEA2024072300733Skin · delaminatedLH WING, SLAT #1, EXTERNAL SURFACE, MIDDLE SIDE WITH DELAMINATION(<P>LH WING, SLAT #1, EXTERNAL SURFACE WAS REPAIRED IAW SRM 57-43-02-2R-1 PAG 1-2 AND SRM 51-70-10-2R-4 FIG 201 SHEET PAG 8,16 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072300734Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 185(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 185 WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 PAG 1-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 4 REV 49 APSDR UIEA2024072300735Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 169(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 169 WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 PAG 1-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 4 PAG 6-7 RSDR UIEA2024072300736Shim · migratedFUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR.(<P>FUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR. AREA ON LH WISDR UIEA2024072400740Position Unit · wornWORN ON FITTING OF TRUCK POSITIONER, LEFT MAIN LANDING GEAR(<P>LH MLG SUPORT OF TRUCK POSITIONER WAS REPLACED IAW AMM 32-32-18-404-027 REV. 142 DATE 22 APR 24. TORQUE TO BOLTS WAS APPLIED 650 LB-IN AND 200 LB-IN WITH TOOL N/S 0823114442 DATE: 15-NOV-24. GOOD FSDR UIEA2024072400741Fuel Tank · leakingRH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK(<P>RH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK. THE FUEL LEAK WAS EVALUATED, SEALANT REMOVED AND REPAIRED IAW AMM 28-11-00-308-013 REV 142 22APR24. THE TEST WAS SATISFACTORY.</P>)SDR UIEA2024072400742Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN BETWEEN FSS 183.3 AND FSS 230.91.(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, PANEL SKIN BETWEEN FSS 183.3 AND AND FSS 230.91 WAS REPAIRED IAW TRE 6755078 REV 1 ISSUE DATE 18 JUL 2024, FSDR UIEA2024072500746Hydraulic Line · chafedCHAFING IN HYDRAULICS LINES RH LANDING GEAR, IN THE MIDDLE OF THE BACK(<P>RH LANDING GEAR, IN THE MIDDLE OF THE BACK. HYDRAULICS LINES WAS REPLACED IAW AMM 20-11-00-910-801 REV. 142 DATE 22 APR 24 AND AMM 20-11-00-910-802 REV. 142 DATE 22 APR 24. TORQUE APPLIESDR UIEA2024072500747Indicator · malfunctionedLH WING, INNER ACCESS PANEL 521QB, RH FUEL QUANTITY INDICATION IN 888.8(<P>RH FUEL QUANTITY INDICATOR WAS REPLACED IAW AMM 28-21-13-404-016 REV. 142 DATE 22 APR 24. OPERATIONAL TEST FUELING QUANTITY INDICATION WAS SATISFACTORY. GOOD FOR SERVICE.</P>)SDR UIEA2024072500748Indicator · malfunctionedLH WING, INNER ACCESS PANEL 521QB, CENTER FUEL QUANTITY INDICATION, FLASHING INDICATION(<P>CENTER FUEL QUANTITY INDICATION WAS REPLACED IAW AMM 28-21-13-404-016 REV. 142 DATE 22 APR 24. OPERATIONAL TEST FOR PRESSURE FUELING SYSTEM QUANTITY INDICATION WAS SATISSDR UIEA2024072500749Valve · failedFWD TRIM VALVE FAIL.(<P>FWD TRIM VALVE WAS REPLACED IAW AMM 21-61-07-404-011-003 REV. 142 DATE 22 APR 24. TORQUE APPLIED 45 LB-IN S/N 0823900243 DATE 15 NOV 24. BONDING TEST WAS SATISFACTORY 2.2 MILLIOMHMS S/N DC- 005040 DATE 12 DEC 24. OPERATIONAL TEST WAS SASDR UIEA2024072500750Relay · faultedAUTO SPEEDBRAKE DEPLOY INOPERATIVE WHEN T/R PULLED(<P>SYSTEM AUTO SPEED BRAKE. ACTUATOR WAS REPLACED IAW AMM 27-62-04-422-023 REV- 142 DATE 22 APR 24. TORQUE APPLIED 80 LB-IN S/N 12995 DATE 11 JUN 25. GEAR TILT PRESSURE SWITCHES LH AND RH WERE REPLACED IAW AMMSDR UIEA2024061200514Lamp · inoperativeEMERGENCY LIGHTS "UNARMED" LIGHT HALF BURNT OUT(<P>RELAMPED EMERGENCY LIGHTS "UNARMED" LIGHT IAW AMM 33-11-00. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024022100098Tape · brokenTAPE ON ELT BROKEN/TORN(<P>TRANSFERRED TO MDDR # 203295 PER MEL 25-63-10-01, CAT D. DUE DATE 19JUN24. PLACARDS INSTALLED.</P> / <P>PART ON HAND NOT CORRECT, TAPE REQUIRED PART OF ELT ASSY. MCC NOTIFIED. NEW ELT ON ORDER. DMI #203295 REMAINS OPEN.</P> / <P>RSDR UIEA2024013100056Fmc · faultedWHILE TAXIING ON GROUND IN MHT, A TURN SHOWED 26 KTS, WHICH I BELIEVE TO BE INCORRECT ON GROUND IN MHT. DURING CRUISE, ATC ADVISED WE WERE OFF COURSE AND LNAV SHOWED ON COURSE TO JWH, FIX WERE GIVEN A HEADING TO FLY. RECEIVED AN IRS NAV ONLY FLAG ON SCRATCH PASDR UIEA2023100300862Trim Switch · unknownUPON ROLL AT THRUST SET TO MASTER WARNING/CAUTION SIREN, EICAS MSG CONFIG / STABLIZER LOW SPEED REJECT(<P>T./S PER FIM TASK 31-51 FAULT TREE 807. R/R CONTORL "STAB TRIM POSITION SWITCH ASSY" IAW AMM 27-48-01.OPS CK GOOD NO MSG. </P>)SDR UIEA2024031500152Altimeter · failedCAPT ALTIMETER FAILED AND DISPLAYED OFF FLAG AT CRUISE. ACCOMPLISED QRH. NO CHANGE(<P>CAPTAIN ALTIMETER REMOVED AND REPLACED PER AMM 34-13-01/404. PERFOMRED OPS CHECK TO THE SYSTEM, ALL OPS CHECKED NORMAL. PITOT STATIC LEAK TEST PERFORMED, NO DEFECTS NOTED.</PSDR UIEA2023091400830Fitting · unknown#1 PYLON FAN COWL SUPPORT BEAM FITTING CRACKED.(<P>R/R #1 ENG PYLON FAN COWL SUPPORT STRUCTURE AFT FITTING P/N 311T2114-7 PO 4842022 AS PER B767 SRM 51-40-02 & DWG 311T2110. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023091400831Fitting · unknown#2Â PYLON FAN COWL SUPPORT FITTING CRACKED(<P>R/R #2 ENG PYLON FAN COWL SUPPORT STRUCTURE AFT FITTING P/N 311T2114-7 PO #4743771 AS PER BOEING DWG #311T2110 AND B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023091400832Angle · unknown#1 PYLON FAN COWL SUPPORT BEAM ANGLE P/N: 311U2510-113 IS CRACKED(<P>R/R CRACKED ANGLE R/N 311U2510-113. FABRICATED NEW ANGLE AND INSTALLED AS PER BOEING 767 SRM 51-40-02 AND DRAWING #311U2510 REV AL.</P>)SDR UIEA2023062000654Medical Kit · unknownFIRST AID KIT ON OVHD BIN HAS SAFETY SEAL BROKEN(<P>REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-04-01. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023011200017Panel · misinstalledEMERGENCY EGRESS WINDOW CAPT SIDE WILL NOT OPEN. REMOVED CAPTS WINDOW EMERGENCY EGRESS PANEL AND REINSTALLED / ADJUSTED PANEL IAW B767 AMM 20-11-00. NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2022120301204Fseu · faultedCLIMBING THROUGH 10,000FT FLAPS UP & IN VNAV, NOTICED THE AIRPLANE SPEED BUG WAS AT 250KTS & THAT THE OVERSPEED TAPE WAS DOWN TO 250KTS. GIVEN A CLIMB TO FL230, BUT ELECTED TO STAY BELOW FL200 AND LEVELED OFF AT FL190 250KTS OF NOTE AT APPROX 14000FT, SLOWED SDR UIEA2022051500480Switch · failedBARBER POLE WOULD NOT ADVANCE AFTER PASSING 10,000FT. INVESTIGATED AND FOUND VMO SWITCH TO BE IN THE ALT POSITION. SWITCHED VMO LIMITING SWITCH TO NORM POSITION IAW AMM 22-00-02</P>)
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