N1439A
Service difficulty reports · 179
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 = 'N1439A' 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 = 'N1439A' 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 IXXA20250918053Power Supply · inoperativeFOUND INTERIOR EMERGENCY LIGHTS RIGHT CEILING, DOOR EXIT SIGN AND DOOR THRESHOLD LIGHT INOPERATIVE DURING EMERGENCY LIGHT TEST. PLACED ON DEFERRAL 66237. MINIMUM EQUIPMENT LIST ATI-33-51-01-01 CATEGORY D. TROUBLESHOT IN ACCORDANCE WITH B767 IAI WIRING DIAGRAMSDR IXXA20250908001Tube · dentedA DENT WAS FOUND DURING C-CHECK MAINTENANCE VISIT LOCATED INSIDE 532BB BETWEEN LOWER STRINGER L-6 AND L-7. THE DENT WAS MEASURED AS L=0.400" W=0.700" D=0.129". DENT TO BE RE INSPECTED AT NEXT C-CHECK TO BE CONSIDERED PERMANENTSDR IXX2025F00019Beam · corrodedFLC DOOR CUTOUT LWR SILL BEAM EXFOLIATED STA622SDR IXXA2025090300018Tube · dentedLEFT WING FUEL DISTRIBUTION TUBE HAS A DENT, LOCATED INSIDE 532BB BETWEEN LOWER STRINGER L-6 AND L-7SDR IXXA20250831002Skin · corrodedRIGHT WING TOP EXTERNAL SKIN CORRODED AT SKIN SPICE AT WING STA 383.5-395SDR IXX2025F00016Skin · delaminatedVERTICAL STAB PANEL LEFT SIDE DELAMINATEDSDR IXXA2025082801Skin · delaminatedRHS VERTICAL STAB SKIN PANEL DELAMINATED AT FSS 270SDR IXXA2023090801Skin · crackedLH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED.SDR IXXA2023090101Support Angle · crackedFLC DOOR CUTOUT UPPER TRANSITION AND CEILING PANEL CRACKED AT CENTER AND GOUGES AT FWD CORNER. REPLACED FLC DOOR CUTOUT CENTER AND FWD CORNER SUPPORT ANGLES IAW B767-300 SRM 51-40-02 PARA 7. P/N 453T1654-28 AND P/N 453T1654-18.SDR IXXA2023082800001Longeron Clip · cracked#1 PYLON HAS TWO CRACKED LONGERON CLIPS ON THE O/B AND I/B SIDE OF WEB LOCATED JUST AFT OF HYD BAY DOORS . REMOVED AND REPLACED LONGERON CLIPS IN #1 PYLON . IAW B767 SRM 51-40-02 PARA 7SDR IXXA2023082802Roller Tray · corrodedROLLER TRAY CORRODED AT STA 654+88 RBL 20 AT LOCK. COMPLETED ROLLER TRAY SPLICE REPAIR IAW B767 SRM 53-00-53 REPAIR 1 DETAIL 4 REF. AMES DOC 47574REA01.SDR IXXA2023090401Roller Tray · corrodedROLLER TRAY CORRODED AT STA. 478 RBL44SDR IXXA20230619037Window · unknownSUPPLEMENTAL-5 JULY 2023-KILN DUE TO SYSTEM OUTAGE, REPORT PREVIOUSLY SUBMITTED VIA ALTERNATE EMAIL PROCEDURES. LEFT FORWARD WINDOW EICAS DISPLAYED. NO OTHER INDICATIONS NOTED. CAPTAIN'S WINDOW SHATTERED AT 35,000 FEET. DIVERSION TO KSMF WITH AN EMERGENCY DSDR IXXA2022103101Skin · crackedLH LE WING STA 616.2 CRACKEDSDR IXXA2023090601Roller Tray · corrodedROLLER TRAY CORRODED AT STA 478, RBL44SDR IXXA20211018078Stiffener · crackedWEB ON STIFFENER AT STATION 971 LBL 90 HAS DAMAGED HOLE. REMOVED, FABRICATED AND REPLACED NEW STIFFNER AT STATION 971 LBL 90 IAW ENGINEERING ORDER 74783FAB01.SDR IXXA20211018077Failsafe · crackedRIGHT FAILSAFE STRAP AT STA 955 HAS A CRACK INDICATION ON ULTRASOUND NDT INSPECTION. REPAIRED FAILSAFE STRAP AT STATION 955 IAW AMES ENGINEERING ORDER 472070RD04.SDR IXXA20211018075Flap · delaminatedLEFT WING TRAILING EDGE INBOUND TRAILING EDGE PLAP HAS DELAM AREA ON INBOUND EDGE. LAYED UP AND CURED IAW B767 SRM 51-70-10.SDR IXXA20211018074Beam · crackedINBOUND HYD BAY LATCH CHANNEL IS CRACKED AT #3 LATCH MOUNT AREA. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-02.SDR IXXA20211018069Skin · delaminatedRIGHT SIDE VERTICAL BETWEEN THE AUX SPAR AND FRONT SPAR THE COMPOSITE SKIN PANEL IS DELAMINATED. REPAIRED RIGHT SIDE VERT STAB PANEL BETWEEN THE AUX SPAR AND FT SPAR IAW B767 SRM 51-70-10 R4.SDR IXXA20211018067Web · crackedFWD DOUBLER ON FAIRING SUPPORT WEB AT TA 1081 CRACKED, FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02.SDR IXXA20211017066Doubler · crackedAFT DOUBLER ON FAIRING SUPPORT WEB AT STA 1081 CRACKED. FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02.SDR IXXA20211017068None · crackedRIGHT STUB BEAM CRACKED AT STATION 903.5 RBL89.REPAIRED RIGHT CRACKED STUB BEAM AT STATION 903.5 RBL 89 IAW
ENGINEERING ORDER 53-767-7702.SDR IXXA20211018076Former · crackedNOSE FORMER IS CRACKED BY #9 SLAT INBOUND AUX TRACK AT WING LEADING STATION 562. REMOVED AND REPLACED DAMAGE NOSE FORMER IAW B767 SRM 51-40-02.SDR IXXA2021100018075Rib · crackedLEFT WING LEADING EDGE AT APPROXIMATELY LES 563.0 HAS CRACKED NOSE RIB. REMOVED AND REPLACED NOSE RIB ON LEFT WING LEADING EDGE AT WS STA 565.9 IAW B767 51-40-02.SDR IXXA20211018073None · cracked#2 AFT STRUT FAIRING SMALL ANGLE ON BACK SIDE OF HYD COMPT OUTBOARD SIDE CRACKED. REMOVED AND REPLACED SMALL "C" ANGLE ON #2 AFT STRUT FAIRING FWD SIDE JUST AFT OF HYD COMPT IAW B767 SRM 51-40-02SDR IXXA20211018071Channel · cracked#2 AFT STRUT FAIRING WEB OUTBOARD "U" CHANNEL CRACKED AT BOTTOM IN RADIUS. REMOVED CHANNEL AND MATCH DRILLED NEW "U" CHANNEL IAW B767 SRM 51-40-05 AND INSTALLED IAW B767 SRM 51-40-02. IN #2 PYLON AFT OF FAIRING WEB.SDR IXXA20211018072Stiffener · cracked#2 AFT STRUT FAIRING ANGLE ON INBOUND FORWARD SIDE OF AFT WEB RUNNING FORE AND AFT IS CRACKED. REMOVED AND REPLACED STRUT FAIRING ANGLE IAW B767 SRM 51-40-02.SDR IXXA20211018070Bulkhead · cracked#1 PYLON PANEL 437DB V FRAME CRACKED. REMOVED DAMAGED V FRAME AND INBD CHANNEL MATCH DRILLED HOLES IAW B767 1-40-05 AND REINSTALLED CHANNELS AND V FRAME IAW B767 SRM 51-40-02 PARA 4 AND PARA 7.SDR IXXA20200920036Flashlight · inoperativeRIGHT FLIGHT DECK EMERGENCY FLASHLIGHT IS INOPERATIVE. CENTER FLASHLIGHT IS OPERATIONAL. INITIATED DEFERRAL MAINTENANCE ITEM-17342. REMOVED AND REPLACED RIGHT FLIGHT DECK EMERGENCY FLASHLIGHT AND BATTERY, IAW B767 AMM 25-05-03. OPERATIONAL CHECK SATISFACTOSDR UIEA2019091605511Clamp · not seated"LEFT BLEED DUCT LEAK" CAUTION EICAS MSG. COMPLETED ASSOCIATED QRH PROCEDURE. INSPECTED LEFT PACK CROSS OVER DUCT, ISO VALVE, AND ACM AREA CLAMPS WITH BAY DOORS OPEN AND CLOSED. NO EICAS MSG NOTED. OK FOR SVC REF AMM 21-50-00. LP 1069086 - ITEM 1: DEFERRED TO SDR UIEA2019090805459Unknown · malfunctionedLP 1100481 (MIA) - SPAR VALVE CHECK FAILS DURING ENG START - RT ENG - RETURN TO BLOCKS. LP 1100482 (CVG) - INFO ONLY - DURING RT ENG START SPAR VALVE CYCLES NORMALLY. THIS AFTER RETURN TO BLOCKS DUE TO NO CYCLING . INDICATION AND LATER DEFERRAL. LP 1100481 (MISDR UIEA2019082875308Oil System · underserviced"APU FAULT" EICAS, 2 ATTEMPTS UNSUCCESSFUL. SERVICED APU OIL IAW AMM 12-13-04. OPS CHECK OK, START ON FIRST ATTEMPT PER AMM 49-11-00.SDR UIEA2019082955285Pressure Switch · failedAPU FAULT, SHUTDOWN DURING POWER TRANSFER. BIT CHECKED THE APU ECU AND FOUND IT WAS FLAGGING LOW OIL PRESSURE IAW FIM 49-11 FT 987. REMOVED AND REPLACED APU LOW OIL PRESSURE SWITCH, IAW AMM 49-94-02. OPS CHECKED OK. CLEARED APU FAULT AND DOOR STATUS FAULT.SDR UIEA2019082755280Warning Message · false activationAFT EQ EXH FAN 2 STATUS MESSAGE. T/S PER FIM 21-26 FAULT TREE 808. MESSAGE CLEARED, OPS CHECK NORMAL.SDR UIEA2019080984972Display · malfunctionedRADAR DISPLAYS SCATTERED RETURNS ACROSS ENTIRE DISPLAY WITH NO PRECIP IN VICINITY. PERFORMED WX RADAR OPERATIONAL TEST IAW AMM 34-43-00. OPS TEST OK, NO DEFECTS NOTED AT THIS TIME.SDR UIEA2019080534938Shutoff Valve · unknownEICAS AND STATUS MSG: R ENG HPSOV. PERFORMED RIGHT ENGINE RUN, NO MESSAGE DISPLAYED AT THIS TIME. PACK PRESSURE HOLDS GOOD. THERE ARE NO DEFECTS FOUND AT THIS TIME, OPS CHECK PERFORMED IAW 71-00-00. REMOVED AND REPLACED R ENGINE HPSOV IAW AMM 36-11-02. LEAK SDR UIEA2019080204931Warning Message · false activationRIGHT ENGINE HPSOV DISPLAYED ON STATUS PAGE. PERFORMED A BITE TEST, NO FAULTS FOUND. SYSTEM OPS CHECKED GOOD IAW AMM 36-00-00.SDR UIEA2019080134899Warning Message · false activationRIGHT ENGINE HPSOV MESSAGE DISPLAYED ON EICAS, IN FLIGHT. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/101. FOUND RH SYS PRV LIGHT ILLUMINATED. PERFORMED MX ACTIONS IAW DDG VOL. 2 36-11-08-01-01A. REACTIVATED R HPSOV. PERFORMED BITE AIR SUPPLY MODULSDR UIEA2019072704868Switch · faultyFWD CARGO FIRE SWITCH LIGHT ON THE P-8 PANEL WOULD NOT TEST DURING SYSTEM OR BRIGHT LIGHT TEST. (BULB GOOD) FWD CARGO FIRE SYSTEM PLACED ON MEL DEFERRAL IAW DDG 26-23-01. MDDR 115416. LP 1053596 - M7: REMOVED AND REPLACED FWD LOWER CARGO FIRE SWITCH IAW SWPM 2SDR UIEA2019072604864Control Valve · malfunctionedL BLEED DUCT LEAK. (<P>TRANSFERRED TO DMI 115382 PER MEL 21-51-01-01, CAT 'C', DUE DATE: 05-AUG-19. PLACARDS INSTALLED AND MX ACTION C/W. </P><P>LP 1053595 - M5: REMOVED AND REPLACED LEFT PACK TEMP CONTROL VALVE REF AMM 21-51-12. OPS CHECK NORMAL. THIS CLEARS SDR UIEA2019072104800Oil System · lowAPU WOULD NOT START. (<P>PERFORMED B767 FIM 49-11 FT 987 APU BITE PROCEDURES. SERVICED OIL, CLEARED FAULTS. OPS CHECK GOOD. </P>)SDR UIEA2019071604763Brake · fireON EXITING RW, TWR ADVISED SMOKE & FIRE EMANATING FROM LEFT MAIN GEAR. EMERGENCY VEHICLES RESPONDED & SPRAYED GEAR.(<P>REMOVED AND REPLACED #6 BRAKE ASSY IAW AMM 32-41-08, OPS CHECK GOOD. PERFORMED ANTI-SKID OPERATIONAL TEST AND BITE TEST IAW AMM 32-42-00, NO SDR UIEA2019071204738Bleed Air Sys · malfunctionedNO DUCT PRESSURE DURING APU OPERATION.(<P>TRANSFERRED TO MDDR 114602 PER 49-11-01-01 CAT C DUE 21JUL19 VALVE LOCKED OUT PER DDG 36-11-01.</P><P>LP 1080383 - M2: PUT THE AIRPLANE BACK IN ITS USUAL CONFIGURATION. PERFORMED FIM 36-10 FAULT TREE 839. NO FAULTS NOTSDR UIEA2019071204739Unknown · malfunctionedNO APU DUCT PRESSURE ON STARTUP AFTER LANDING. (<P><SPAN>RE-STARTED APU DUCT PRESSURE NORMAL, NO FAULTS FOUND REF AMM 49-11-00 DUCT PRESSURE REF 49-52-00.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)SDR UIEA2019070404670Eec · malfunctionedNO LIGHT OFF ON RIGHT ENGINE START. SELECTED BOTH, SECOND ATTEMPT SUCCESSFUL. (<P>RT ENGINE IGN. 1(A) INOP, DEFERRED IGN 1(A) PER MEL 74-00-01B CAT 'C'. THIS OPENS DMI # 114171, PLACARD INSTALLED AND MCC NOTIFIED.</P><P>LP 1054226 - M5: T/S PER SRM 74-31-01. SDR UIEA2019062864592Light · intermittentRIGHT ENG BLEED OFF BACKLIGHTING, NO ILLUMINATION WITH ENG SHUT DOWN. FOUND DURING COCKPIT PRE-FLIGHT. RESET RT ENG BLEED SWITCH IAW AMM 36-20-00. OFF LIGHT CAME BACK ON. OPS CHECKED GOOD.SDR UIEA2019062404564Exciter · malfunctionedITEM 1 - INFO, FIRST START ATTEMPT ON RIGHT ENGINE NO LIGHT OFF. ITEM 2 - STATUS MESSAGE: R ENG IGNITER 1(<P>RT ENG #1 IGNITION INOP. PLACED ON MEL 74-00-01B DMI #113663, SELECT BOTH TO START ENGINE. </P><P>LP 1080536 - M2: REMOVED AND REPLACED RT ENG #1 IGNITSDR UIEA2019062104551Switch · brokenCAPTAIN`S OXYGEN TEST RESET SWITCH BROKEN. REMOVED AND REPLACED CAPT OXYGEN STOWAGE PER ASSY AS REQ, LEAK CHECKED GOOD IAW AMM 35-11-51.SDR UIEA2019061874510Exciter · malfunctioned# 2 ENGINE DID NOT START WITH SINGLE IGNITER , SWITCHED TO BOTH FOR BOTH ENGINE STARTS. PERFORMED NO.2 SYS IGNITION AUDIBLE TEST. CONFIRMED ONLY ONE IGNITER IS OPERATING WITH SWITCH SET TO 'BOTH'. A/C DOWNGRADED TO ER 60. PLACARDS INSTALLED. REMOVED AND REPLA
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