Boeing 767-34AF
Service difficulty reports · 6,303
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 = '76734AF' 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 = '76734AF' 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 IPXA2025082141090Stiffener · crackedCRACK - ANGLE, FWD MEC AT STA 246 LBL 40 FLOOR STRUCTURE. .ACCOMPLISHED REPAIR I.A.W SRM 53-10-51-2R-4 REV.92 AND EGAT WORK SHEET NO.50647SDR IPXA2025081621930Web · crackedCRACKED WEB, AFT LOWER CARGO COMPT ENTRYWAY AT STA 1329 LBL 2.2. .I.A.W AMM 20-11-00-910-802 REV.145 REMOVED BALL PANEL SUPPORT FITTING.FABRICATE P/N: 451T2603-65 PER BOEING DWG NO: 451T2603 SH. 11 REV."-"; PL REV."AP"; PSDL REV."-" AND ORIGINAL PART AS A SASDR IPXA2025081107546Seal · brokenFOUND THE CREW ENTRY DOOR AFT DOORWAY LINING SEAL BROKEN. OK TO WORK. OPENSDR IPXA2025081104151Sensor · out of adjustBTD DUE TO FWD ENTRY DOOR EICAS L FWD ENTRY DOOR ON PUSH BACK. ADJUSTED SENSOR AND TESTED SATIS PER AMM TASK 52-12-00-715-119 REV 137.SDR IPXA2025081102208Pump · no discrepancyAIR TURN BACK, CENTER TANK RIGHT FUEL PUMP PRESSURE IS LOW PERFORMED QRH PROCEDURE DID NOT RETURN A/C TO NORMAL OPERATION RESULTED IN AN ATB IAW AMM 28-31-01. REPLACE RH CTR TANK JETT PUMP. BONDING RESISTANCE CHECK AND PUMP FUNCTIONAL/OPERATION CHECK NORMAL.SDR IPXA2025080729838Fce · faultedAIR TURN BACK, LE SLAT DISAGREE. PERFORMED FSEU BITE PER FIM 27-51 FT 809. FOUND EXISTING FAULT MSG: LVR RVDT 2 MISRIG WITH FAULT CODE 27-51023. ALSO PREVIOUS LEG FAULT 0. FOUND MSG: LE SLATS SEE FIM WITH FAULT CODE: 27-81045. PERFORMED POSITION RVDT #2 (MSDR IPXA2028080700149Strut · corrodedSUSPECTED CORROSION RH MLG UPPER STRUT BODY - APPROX 14€? X 0.75€? TOTAL AREA BLENDED CORROSION AREAS IAW CMM 20-10-01 STEP 2.F AND 2.H. PITTING STILL REMAINS. MAPPED AND SENT DAMAGE PHOTOS TO ENGINEERING OF PITTED AREAS AND ATTACHED TO FAULT. PITTED AREAS SDR IPXA2025080476560Lever · malfunctionedMAIN ENTRY DOOR - YELLOW PUSH TO, SECURE LEVER WILL NOT ENGAGE TO THE LOCK/SECURE POSITION WITH THE ENTRY DOOR CLOSED. PERFORMED ADJUSTMENT OPS CHECK OF ENTRY/SERVICE DOOR INTERLOCK PAWL. OPS CHECK GOOD AT THIS TIME REF AMM 52-11-26-710-801SDR IPXA2025080237986Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-105 PANEL NO : 231AFF. I.A.W AMM 25-57-02-004-029 AND AMM 25-57-05-004-001 REV.145. FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PSDR IPXA2025080451310Adc · inoperative***AIR TURN BACK*** AIRCRAFT DISPLAYED FLAP LIM & SPD LIM AT 255 KTS AND 3000 FT ON CLIMBOUT. FLAP LEVER WAS IN UP POSITION AND INDICATED UP ON FLAP INDICATOR. ++REPLACED R ADC IAW AMM 34-12-01. OPS CHECK SATISFACTORY PER AMM 34-12-00. RESEATED R SWC PER AMM SDR IPXA2025080518981Angle · crackedFOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 INBD SIDE. .I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL , G.V.I AND CONDITION CHECK NORMAL. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 92. INSTALLED NEW ANGLE I.A.SDR IPXA2025080519135Angle · crackedFOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 OUTBD SIDE. I.A.W AMM 25-59-01-004-001 REV.145. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 92. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 92. AND BOEING DWG NO. 146T5650 SH. 5 REV. C. SDR IPXA2025080126694Lever · bindingUPON CREW ENTRY DOOR CLOSURE, CAPTURE LEVER DIFFICULT TO MOVE OUTBOARD. INSPECTED CREW ENTRY DOOR HANDLE CAPTURE LEVER AND FOUND NO DEFECTS. OPERATED DOOR AND TESTED PER AMM 52-12-00-715-119. NO FAULT, DEFECTS OR EXCESSIVE FORCE WAS NOTED AT THIS TIME. OK FOR SDR IPXA2025080870685Skin · corrodedCORROSION, FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-94636-REQ1 REV1.SDR IPXA2025080670685Skin · corrodedCORROSION, FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. RESPECTIVELY PART MARK THE REPAIR PART(S) PER BAC5307 CODE M AS BELOW. REPAIR FILLER: F2025A53M-1650-1, REPAIR DOUBLER: F2025A53M-1650-2; REPAIR TRIPLER: F2025A53M-1650-3. INSTALL THE REPAIR PARTS WSDR IPXA2025073083108Window · crackedDIVERSION, L1 WINDOW CRACKED. REPLACED WINDSHIELD IAW AMM 56-11-01-404-017 REV 145. LEAK AND OPS CHECKED SATIS.SDR IPXA2025081456371Acoustic Liner · damagedBROKEN-ACOUSTIC LINER, NO.2 ENG FAN CASE MIDDLE 7:00 AREA . I.A.W AMM 72-33-01-004-001-H00 AND 72-33-01-404-011-H00 REV.145, REPLACED THE ACOUSTIC LINER SEGMENT OF NO.2 ENGINE.SDR IPXA2025072856371Acoustic Liner · brokenBROKEN ACOUSTIC LINER, NR 2 ENG FAN CASE MIDDLE 7:00 AREA. OK TO WORK.SDR IPXA2025080644382Filler · corrodedFOUND FILLER WITH CORROSION DAMAGE AT STA 1602 LBL 62 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92. REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92. FABRICATE FILLER (P/N: 146T5609-67) PER BOEING DRAWING 146T5609 SH 7 REV.SDR IPXA2025080734467Fitting · crackedFAULT- FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1197 BL0. (FLOOR PANEL NO. 251AFF). I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT , G.V.I AND CONDITION CHECK NORMAL. REMOVED DAMAGSDR IPXA2025072734622Floor Panel · crackedFOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, P/N: 146T5869-89 PANEL NO: 251XFF STA 1400~ STA 1520 LBL 55~ LBL 77. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT AND PERFORM G.V.I CHECK RESULT WAS NORMAL. 1.FABRICATE A NEW SDR IPXA2025080634499Filler · corrodedETOPS, FOUND FILLER WITH CORROSION DAMAGE AT STA 1602 RBL 62 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92. FABRICATE FILLER (P/N: 146T5609-67) PER BOEING DRAWING 146T5609 SH 7 REV."-"; PL REV."AA" AS A SAMPLE I.A.W GMM-MTX SDR IPXA2025080633038Floorbeam · corrodedFOUND FLOOR BEAM CLIP WITH CORROSION DAMAGE AT STA 1596.5 RBL 55 IN BULK CARGO COMPARTMENT. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT , G.V.I AND CONDITION CHECK NORMAL. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.92. SDR IPXA2025080633067Floorbeam · corrodedFOUND FLOOR BEAM CLIP WITH CORROSION DAMAGE AT STA 1596 LBL 57 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.92 FABRICATE CLIP (P/N: 146T5619-358) PER BOEING DRAWING 146T5619 SH 8 REV."-"; PL REV."BY"; PSDL REV."-" AS A SAMPLE I.A.WSDR IPXA2025080633177Support Strap · corrodedCORROSION - STRAP, FWD CARGO CEILING LINER SUPPORT AT STA 478-610 RBL 39. REMOVED DAMAGE STRAP I.A.W SRM 51-40-02-0G REV.92. I.A.W. UPS EO NO.:EO-94540-REQ1 REV 1 STEP 1 , COMPLETED MACHINING THE CEILING SUPPORT STRAP. ACCOMPLISHED JOB I.A.W UPS EO-94540-REQ1SDR IPXA2025080534497Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) 1. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.92 INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO. 146T5650 SHEET 5 REV C.SDR IPXA2025080533093Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. .I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT , G.V.I AND CONDITION CHECK NORMAL. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.92. I.SDR IPXA2025080534499Filler · corrodedFOUND FILLER WITH CORROSION DAMAGE AT STA 1602 RBL 62 IN BULK CARGO COMPARTMENT. (REPLACE) 1. REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92 FABRICATE FILLER (P/N: 146T5609-67) PER BOEING DRAWING 146T5609 SH 7 REV."-"; PL REV."AA" AS A SAMPLE I.A.W GMM-MTSDR IPXA2025072734706Floor Panel · crackedFOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, P/N: 146T5869-88 PANEL NO: 252UFF STA 1400~ STA 1520 RBL 55~ RBL 77. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT AND PERFORM G.V.I CHECK. RESULT WAS NORMAL. FABRICATE A NEW SDR IPXA2025072256161Pump · inoperativeDURING CRUISE, RECEIVED CTR R FUEL PUMP (EICAS C). RAN CHECKLIST AND OPERATED REMAINDER OF FLIGHT WITH CTR R FUEL PUMP INOP. I.A.W. AMM 28-22-05-004-057-002 REV.145 AND AMM 28-22-05-404-078-002 REV.145 REPLACE THE CTR R FUEL PUMP. I.A.W. AMM 28-22-00-715-001 SDR IPXA2025072555740Floor Panel · crackedFOUND BULK CARGO FLOOR PANEL DAMAGE , STA 1518 LBL 24. (REPAIR) 1.ACCOMPLISHED REPAIR I.A.W SREO-34806-REQ002 REV.1.SDR IPXA2025072555713Floor Panel · crackedFOUND BULK CARGO FLOOR PANEL DAMAGE , STA 1480 , LBL 5. (REPAIR) 1.ACCOMPLISHED REPAIR I.A.W SREO-34806-REQ002 REV.1.SDR IPXA2025072230582Liner · brokenFOUND MAIN DECK DOORWAY LINING BROKEN TTL: 2 AREA. (REPAIR) I.A.W AMM 52-12-02-004-001 REV.145 REMOVED DOORWAY LINING.SDR IPXA2025072008272Floor Panel · damagedFOUND MAIN DECK FLOOR DAMAGE, P/N : 145T5876-85 PANEL NO : 241FFF. I.A.W AMM 25-57-05-004-001, AMM 25-58-01-004-001 AND AMM 25-58-03-004-001 REV.145 REMOVED MAIN DECK CARGO HANDLING AND G.V.I CONDITION CHECK NORMAL. .FABRICATE A NEW FLOOR PANEL I.A.W. SREO-969SDR IPXA2025072210407Window · warning messageETOPS, L WINDOW MSG QRH ACTIONED MSG REMAINS DISPLAYED REPLACED L2 WINDOW IAW MM 56-11-02-404-026 OPS CHECK NORMALSDR IPXA2025071410407Warning Message · illuminatedLEFT WINDOW MSG QRH ACTIONED MSG REMAINS DISPLAYED. DEFERRED THE L2 WINDOW AS PER MEL 30-41-1-2. DMP C/W AND PLACARD INSTALLEDSDR IPXA2025072727420Skin Panel · gougedGROUND CREW REPORTS GOUGE ON DOUBLER OF PREVIOUSLY REPAIRED AREA OF DAMAGE ON THE LOWER FORWARD CARGO DOOR FRAME. FUSELAGE STATION 478, WL 121. INSTALLED LINER ON RIGHT SIDE FWD CARGO COMPARTMENT REF AMM 25-52-01.SDR IPXA2025070814759Weu · faulted**ATB** FIRE BELL SOUNDED ON ROTATION NO MASTER WARNING LIGHTS OR ANY OTHER FIRE INDICATIONS RTB AS A PRECAUTION. R&R BELL CHIME WARNING CARD PER 31-51-04. OPS CHECK GOODSDR IPXA2025071295380Bear Strap · crackedCRACK, FWD ENTRY DOOR AFT LOWER CORNER BEAR STRAP. INSTALLED INSULATION BLANKET IAW AMM 25-80-00-400-803 REV. 145, JOB COMPLETED AND CONDITION CHECK NORMAL. IAW AMM 20-11-00-910-802 REV 145 INSTALLED THE E/E COOLING DUCT AT MEC P31. IAW AMM 24-22-00-862-001 RESDR IPXA2025072374238Link · damagedWORN OUT - SUPPORT LINK, NO.2 ENG R/H HPT CASE COOLING FWD DUCT UPPER SIDE, NEAR FUEL SUPPLY LINE. I.A.W AMM 70-50-00-912-001-H00 REV.145, REPLACED THE LINK OF NO.2 ENGINE. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR IPXA2025072374286Link · damagedWORN OUT - SUPPORT LINK, NO.2 ENG L/H LPT CASE COOLING FWD DUCT LOWER SIDE, NEAR EGT. I.A.W. AMM 70-50-00-912-001-H00, REV.145, REPLACED THE LINK OF NO.2 ENGINE. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR IPXA2025071272165Rib · crackedNUMBER 10 SPOILER ACTUATOR SUPPORT HINGE RIB CRACK WS 640. INSTALL NEW FITTING I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG 112T1000 SH 14 REV: B, 113T1422 SH 1 REV: D, 112T1001 SH 43 REV: -, 113T1653 SH 1 REV: J. I.A.W AMM 27-61-01-424-019 REV 145 STEP 3A TSDR IPXA2025071173048Strap · crackedCRACK - STRAP, FWD LOWER CARGO MAIN DECK FLOOR STRUCTURE STA 610 RBL 64.5. INSTALL THE REPAIR PARTS WET WITH BMS 5-95 FAYING SURFACE SEALANT. REFER TO FIGURE 2. INSTALL ALL HI-LOKS WET WITH BMS 5-95 SEALANT IN TRANSITION FIT HOLES PER 767-300F SRM 51-40-05. SHSDR IPXA2025070774321Hinge Fitting · crackedCRACK - FITTING, INBD SIDE OF L/H WING T/E INBD MAIN FLAP T/E MID LINK FITTING, WBL 174. PERFORM SRM 57-53-02-2R-1 REV.92 AND EGAT WORK SHEET NO. 50533 STEP 14 TO 15 14.ASSEMBLE THE REPAIR PARTS WITH BMS 5-95 SEALANT BETWEEN MATING SURFACES. REFER TO 767-300F SDR IPXA202507074238Link · wornWORN OUT SUPPORT LINK, NO.2 ENG R/H HPT CASE COOLING FWD DUCT UPPER SIDE, NEAR FUEL SUPPLY LINE. (REPLACE) OK TO WORKSDR IPXA2025072362233Fan · damagedFOUND SUPPLY FAN JOINT SLEEVE WORN OUT. I.A.W AMM 21-58-06-004-283 REV.145 AND AMM 21-58-06-404-284 REV.145 REPLACED THE SLEEVE.SDR IPXA2025072363772Valve · damagedCRACK - FLANGE, NO. 2 PYLON FAN AIR VALVE INLET. I.A.W. AMM 36-11-16-004-001-006, AND 36-11-16-404-015-006, REV.145, REPLACED THE FAN AIR VALVE OF NO.2 ENGINE. I.A.W AMM 36-11-16-404-015-006 REV.145, DID THE OPERATIONAL TEST, RESULT: NO LEAK WAS FOUND AND TESTSDR IPXA2025070762233Sleeve · wornFOUND SUPPLY FAN JOINT SLEEVE WORN OUT.SDR IPXA2025070763772Inlet · crackedCRACK - FLANGE, NO. 2 PYLON FAN AIR VALVE INLET. (REPLACE) OK TO WORKSDR IPXA2025070762480Manifold · brokenBROKEN - MANIFOLD, NO.2 ENG LPT CASE COOLING, NEAR 11:00 AREA. I.A.W. AMM 75-24-03-004-050-H00 AND 75-24-03-404-037-H00, REV.145, REPLACED THE LPT COOLING MANIFOLD OF NO.2 ENGINE. JOB COMPLETED AND CONDITION CHECK NORMAL.
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