Boeing 767-300
Service difficulty reports · 2,148
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '767300' 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 aircraft_model_key = '767300' 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 IPXA2025050244800Skin · dented*** MAJOR REPAIR *** RIGHT SIDE FUSELAGE SKIN DENT AND CREASE REPAIR AT STA 139 ABOVE S-21R REVIEW COMPLETE.SDR IPXA2024102340525Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA (REPLACE). I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.143 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.SDR IPXA2024102342031Floor Panel · crackedFOUND FLOOR PANEL WITH CRACK DAMAGE IN MAIN DECK, PANEL NO: 251XFF, P/N: 146T5869-135. (REPAIR). I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 25-57-02-404-016 AND AMM 25-58-04-404-015 REV.143 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORSDR IPXA2024092851725Skin · damagedFOLLOW ON ACTION, ON FUSELAGE SKIN DAMAGE AND STRINGER DAMAGE STA 1417 TO STA 1439 S-38R TO S-38L AFTER ADDITIONAL CUTOUT PERFORMED, FOUND SKIN AT AFT SIDE OF CUTOUT TO BE .063" THICK. OPENSDR IPXA2024090373368Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO: 231BFF , P/N: 143T5876-104 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. EO-91289-REQ1 REV.1. CONDITION CHECK IS SATISFACTORY. I.A.W AMM 25-57-02-404-016 AND AMM 25-57-03-404-005 AND AMM 25-57-05-404-006 AND AMM 25-57SDR IPXA2024090671665Drain · no discrepancyFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO 82173. COMPLETED.SDR IPXA2024083171665None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.SDR IPXA2024082998832Warning Message · false activationLH FWD ENTRY DOOR EICAS MSG OK TO CLOSE IN REF TO FIM 52-90-17-41 AND AMM 52-12-00/201 CONFIG 1, UNABLE TO DUPLICATE ISSUE. DOOR OPEN MSG IS PRESENT WHEN DOOR IS OPEN AND MSG IS EXTINGUISHED WHEN DOOR IS CLOSED. OPEND AND CLOSED DOOR SEVERAL TIMES AS WELL AS PSDR FDEA202408141122Floorboard · delaminatedMAIN DECK COMP. AT APROX STA 412 TO STA 490 & LBL 11 TO RBL 11 FLOORBOARD 231AFF HAS SURFACE AREA INDENTATION (MARKED) FABRICATED NEW FLOORBOARD PNL# 231AFF AT STA. 412-490, LBL 11-RBL11 IN REF TO FEDEX DRW# SRZ-25-005. SEE JPF FOR OTHER WORK ACOMPLISHEDSDR FDEA202408081092Slat System · fault messageAFTER SELECTING FLAPS FROM 20 TO 30 FOR APPROACH LE SLAT DISAGREE EICAS WITH ASSOCIATED LEADING EDGE DISCRETE LIGHT ANNUNCIATED. EXECUTED MISSED APPROACH, RAN QRH, DECLARED EMERGENCY WITH SPOKANE APPROACH CONTROL AND LANDED. EMERGENCY DECLARED. TROUBLESSDR IPXA2024073078169Switch · malfunctionedTOGGLE SWITCH ON EMER LIGHTS DOES NOT WORK CORRECTLY R/R EMERGENCY LIGHT CONTROL PANEL PER AMM 33-51-00SDR IPXA2024073078959Switch · malfunctionedTOGGLE SWITCH ON EMER LIGHTS DOES NOT WORK CORRECTLY. R/R EMERGENCY LIGHT PANEL PER B767 AMM 33-51-00SDR IPXA2024073075528Transformer · faultedGROUND SERVICE 28 V AC BUS TRANSFORMER 2 LOW VOLTAGE WIRE DAMAGED. REMOVED AND REPLACED 28 VAC BUS TRANSFORMER 2 IN REFERENCE TO SWPM 20-30-00, 20-30-11 AND WDM 24-53-51-1. OPS NORMAL AT THIS TIME.SDR IXXA2024060202Bracket · crackedFLOOR SUPPORT BRACKET CRACKED IN HALF AT STA 1562 RBL-79 IAW B767 SRM 51-40-02-8, RBL79, STR 21RSDR IXXA2024060201Floor Support · crackedFLOOR SUPPORT BRACKET IS CRACKED IN HALF, AT STA.1562, LBL79, JUST BELOW THE CABIN FLOOR, CLOSE TO STR 20LSDR FDEA202404240284Sensor · damagedON DESCENT RECEIVED EQUIP OVHT EICAS. COMPLIED WITH CHECKLIST. RECEIVED AGAIN ON LANDING. COMPLIED WITH CHECKLIST ALL WAY THROUGH ON GRID AND INFLICT. SWITCH LEFT IN STBY DURING SHUTDOWN. COMPLIED WITH ALL CHECKLIST. INSATLLED NEW EQUIPMENT COOLING LOW FLSDR IPXA2024041735963Guard · malfunctionedEMER LIGHTS SWITCH GUARD CAUSING SWITCH TO TURN OFF FROM ARMED POSITION INTERMITTENTLY. REPLACED EMERGENCY LIGHTS CONTROL PANEL. OPS OK REF AMM 33-51-08.SDR FDEA202404020433Former · crackedFOUND FORMER CRACKED AT RH WING STATION 441 0000704471 : FLEEHEARTY, AARON T - 02-APR-2024 21:46 INSTALLED NEW FORMER AND L-ANGLE FROM WING STA 441 REF B767 SRM 51-40-02, B767 SRM 57-41-09-2R AND FDX DWG SR67-57-002SDR IPXA2024032194772Valve · warning message*DIVERSION* R ENG PRV STATUS MESSAGE ON TAKEOFF #2 ENG PRV MANUAL WRENCHING ACCOMPLISHED AND VERIFIED TO BE HARD TO WRENCH AND WITH STUCK POSITION IN THE MIDDLE. THEREFORE #2 ENG PRV REPLACED AS PER AMM 36-11-18/401 REV.141 OPS AND LEAK TEST FOUND SATIS.SDR IPXA2024032691538Wire · damagedLDG GEAR MONITOR MSG T/S AS PER B767 FIM 32-61- FAULT TREE 812 AND WDM 32-61-13. FOUND PROX. BOX BITE DISPLAYED FAILURE OF S233 NOSE SYS1 NOSE GEAR LOCKED PROX SENSOR-AMM 32-61-03-722-043/32-09-04-704-013. ISOLATED PROBLEM TO WIRE 207R-22 IN P36 PNL. BETWEEN SDR IPXA2024031591538Sensor · faultedLDG GEAR MONITOR MSG T/S LDG GEAR MSG IAW FIM 32-61 FAULT TREE 812 FOUND NLG DOWN SENSOR 233 FAULTED SWAPPED LH/RH PROBLEM DIDNT FOLLOW. OPENSDR IPXA2024031439522Window · crackedLH #1 WINDOW CRACKSDR 2DYA202403130070Skin · corrodedBLEND REPAIR TO LH INSPAR WING PANEL NO.1 LOWER SURFACE AT REAR OF SPAR AND WS 1055.0SDR 2024F00069Skin · corrodedBLEND REPAIR TO LH SPAR WING PANEL NO.1 LOWER SURFACE AT STINGER NO.7 AND WS 1089.0SDR 2DYA202403130068Skin · corrodedBLEND REPAIR LH WING LOWER SKIN AT WS 1040.0SDR IXXA2024022101Precooler · cracked# 1 ENGINE CORE COWL PRE-COOLER EXHAUST DUCT MATING FLANGE CHAFED AND CRACKEDSDR IXXA2024021904Stringer · damagedF/S 429 STR11L DRILL STARTSDR IPXA2024020697266Drain · damagedFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36RSDR FDEA202401220100Flap · delaminatedLH WING OUTBOARD FLAP BETWEEN INBOARD SIDE AND INBOARD FLAP TRACK AREA LEADING EDGE WITH DELAMINATE. LH WING OUTBOARD FLAP AT OTEF 345.75 WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG 3-9 FIG 201 AND SRM 51-70-17-0G PAR 4.A PAG 24,25,48 FIG 10 REV 88 DEC 15/2SDR FDEA202401170084Spoiler · delaminatedLH WING SPOILER #1 UPPER SKIN WITH DELAMINATED. LH WING SPOILER #1 UPPER SKIN WAS REPAIRED IAW B767 SRM 57-70-01-2R REP 1 PAG 1-4 AND SRM 51-70-17-06 PAR 4.A FIG 10 PAG 24,48 REV 88 DEC 25/2023.SDR FDEA202401170083Skin · dentedUPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1480/1510.5 AND STG 3 / 4 LH WITH DENT. UPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1461/1480 AND STGR 3/4 LH WAS REPAIRED I.A.W. SRM 53-00-01-212 REPAIR 14 FIG. 201 AND INSPECTION REQUIREMENTS SEE TABLE V ZONE A - SDR FDEA202401170082Skin · dentedUPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1480/1510.5 AND STG 3 / 4 LH WITH DENT. UPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1461/1480 AND STGR 3/4 LH WAS REPAIRED I.A.W. SRM 53-00-01-212 REPAIR 14 FIG. 201 AND INSPECTION REQUIREMENTS SEE TABLE V ZONE A - SDR FDEA202401130076Unknown · unknownWEIGHT CHECK DUE FOR THE FLIGHT DECK PORTABLE FIRE EXTINGUISHER MOUNTED IN FRONT OF RAFT STOWAGE. GMM: 9-4-404 AMM: 26-26-02-4-1 COMPLETED WEIGHT CHECK PROCEDURE PER ABOVE REFS. OK FOR SERVICE.SDR FDEA202401120081Skin · dentedDURING BIRD STRIKE INSPECTION FOUND DENTS LOCATED FWD OF CAPTAINS WINDHIELD AFT OF RADOME. REPLACED FUSELAGE SKIN PANEL 141T3830-18 REF E.A. H-5330-T0377384 REV. C PT2 AND SRM STANDARD PRACTICES. SEE JPF FOR WORK ACCOMPLISHED,SDR FDEA202401050041Beam · crackedLEFT WING, UPPER SURFACE PANEL, FORWARD OF OUTBOARD AILERON IS MISSING MULTIPLE FASTENERS. MARKED WITH TAPE. REPLACED CRACKED BEAM PER EA H-5720-T0377649 P1.SDR IPXA2023122648565Unknown · unknown*SDR FILED OPEN* FAULT - FUSELAGE SKIN AT STA 1050.25 BETWEEN S21L AND S22L FOUND WITH BLEND MARK RECOMMENDED ACTION TO MEASURE BLEND OUT MARKSDR IXXA20240103Skin · damagedLH FUSELAGE LIGHTNING STRIKE DAMAGE AT STATION 387 STRINGER33LSDR IPXA2023122624315Unknown · unknown*SDR FILED OPEN* FAULT - SCRATCH MARK FOUND AT FUSELAGE EXTERNAL SKIN STA 368 TO STA 390, S-10L OK TO WORKSDR FDEA202312231952Brake Assy · making metalON WALK AROUND METAL SHAVINGS COMING FROM #5 BRAKE. AMM: 32-11-18-4 COMPLETED INSTALLATION OF LMLG BOGIE BEAM ASSY, IAW AMM 32-11-18-4. PLS SEE W/O 87633, SEQ. 5 FOR ALL WORK ACCOMPLISHED AND PARTS INFORMATION.
SERVICABLE MLG BRAKE INSTALLED IN # 5 POSITSDR FDEA202312191948Fseu · failedON FINAL APPROACH INTO CAN WHEN SELECTING FLAPS 25 RECEIVED A LEADING EDGE, SLAT DISAGREE EICAS MESSAGE. EXECUTED MISSED APPROACH AND PERFORMED QRH PROCEDURE. UNEVENTFUL FLAPS 20 VREF 20 LANDING. LEFT FLIGHT CONTROLS, EXTENDED AND DEBRIEFED MAINTENANCE. SDR FDEA202312111933Linkage · damagedRH WING INBD TRALING EDGE FLAP LINKAGE (113T770-52G) FAIRNIG AT WS 671. HAS A HOLE PUNCTURE REPAIRED RH WING TRAILING EDGE FLAP LINKAGE FAIRING (PNL# 671FB) AT WS 671. IN REF. TO EA#: H-5750-T03773386 767 SRM 57-53-70-2R FIG. 201 SHEET 2, 767 SRM 51-70-03-SDR IPXA2023121009987Unknown · unknownMAJOR REPAIR, EXISTING FRAME REPAIR AT STA 1219 AND S-18L MODIFICATION FOR BCF MOD BRACKET ASSEMBLY INSTALLATION (CATEGORY B REPAIR) OK TO WORKSDR FDEA202312091934Skin · damagedPER WRI 53-30/0922, DURING BIRD STRIKE INSPECTION, FOUND DENTS LOCATED FWD OF CAPTAINS WINDSHIELD AFT OF RADOME. REPLACED SKIN PANEL 141T3830-18REF E.A. H-5330-T0377384 REV. C PT 2 AND SRM STANDARD PRACTICES. REF W.O. 87715 NR 52 FOR WORK ACCOMPLISHED.SDR FDEA202311301901Switch · failedCABIN PRESSURE FLUCTUATIONS OF /- 500FPM DURING FLIGHT. REPEAT WRITE-UP. REF: WRI 22-30/0868 REMOVED AND REPLACED AY AUTOTHROTTLE MICROSW PER AMM. ALL ADJ/ TESTS GOOD AT THIS TIME. A/C OK FOR SDR CALA2023120103512Processor · faultyRIGHT WING FUEL QTY AND TOTALIZER DISPLAY BLANK FOUR TIMES FOR U P TO 5 MINUTES AT A TIME CREW VERBAL REPORT, THE RIGHT WING TANK AND FUEL TOTAL QTY INDICATION RECOVERED AND REMINED ON DURING APPRACH AND LANDING.(CENTER TANK PUMPS SELECTED OFF) BITE CHECKED FUSDR FDEA202311251896Access Door · crackedLOWER HALF OF FUSELAGE, ACCESS DOOR 113AL WITH A BIRD STRIKE ON EXTERNAL SURFACE. THE DAMAGE AT EXTERNAL SURFACE IN ACCESS DOOR 113AL WAS REPAIRED. I.A.W. DRAWING 141T6401 REV.L I.A.W. SRM 51-40-02-0G REV.87 AUG 15,2023.SDR FDEA202311241891Skin · dentedLOWER HALF OF FUSELAGE, BETWEEN STA 135.5 AND STA 148.5, AND BETWEEN STGR 21R AND STGR 30R, BIRD STRIKE. DAMAGE AT LOWER HALF OF FUSELAGE, BETWEEN STA 135.5 AND STA 148.5, AND BETWEEN STGR 21R AND STGR 30R WAS REPAIRED. I.A.W. E.A.#: H-5330-T0377079 PART: SDR FDEA202311241890Skin · crackedUPPER HALF OF FUSELAGE, BETWEEN STA 132.5 AND STA 143.5, AND BETWEEN STGR 14-L AND STGR 18-L, BIRD STRIKE. DAMAGE AT UPPER HALF OF FUSELAGE, BETWEEN STA 132.5 AND STA 143.5, AND BETWEEN STGR 14-L AND STGR 18-L WAS REPAIRED. I.A.W. E.A.#: H-5330- T0377062 PSDR FDEA202311241889Skin · damagedLOWER HALF OF FUSELAGE, BETWEEN STA 132.5 AND 143.5, AND BETWEEN STGR 30-L AND STGR 31-L, BIRD STRIKE. DAMAGE AT LOWER HALF OF FUSELAGE, BETWEEN STA 132.5 AND BETWEEN STGR 50-L AND STGR 31-L, WAS REPAIRED I.A.W. E.A.:# H-5330-T0377078 PART: 1(P1) RELEASESDR FDEA202311231887Orifice · failedTHE DOOR TO THE CRM IS EXTREMELY HARD TO OPEN - THE CRM IS HOLDING TOO MUCH PRESSURE. DID NOTICE THE EYEBALL VENT DOES NOT EMIT MUCH AIR - SUSPECT MAYBE THE CRM IS NOT VENTING CORRECTLY. WE ARE PUSHING THE BLACK RELIEF BUTTON AND CAN HEAR IT RELIEVING PRE
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