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 FDEA202309161608Panel · damagedCREATED THIS NR TO DO A RDR & SDR FOR REPAIR OF 149T7760-89 PANEL BOND ASSY. (REPAIR OF PANEL DONE ON EA H-2750-T0376188 P1 PAGE 7. TITLE: FLAPS/CNTRL/IND - LH INBD FLAP MECHANISM, TRACK LINK BOLT FAILED, TEAR DOWN AND INVESTIGATION. ***SDR ENTERED IN ESDR FDEA202309151629Panel · damagedPANEL 195GL PN 113T1740-275 DAMAGED. REPAIRED PANEL IN REF. TO EA# H-5350-T0376218 P1SDR IPXA2023091847718Unknown · unknownFAULT - BROKEN - JUMPER ASSY, FWD CARGO DOOR CUTOUT STA 618 S-21R AREA. (REPLACE) 1. I.A.W AMM TASK 52-33-01-404-061 REV.139 AND AMM TASK 52-33-01-004-060 REV.139 REPLACE THE JUMPER AT FWD CARGO DOOR FWD CUTOUT CORNER. 2. JOB COMPLETED AND CONDITION CHECK NORMSDR IPXA2023091851421Unknown · unknownFAULT - TORN - JUMPER, AFT CARGO DOOR AFT CUTOUT UP CORNER STRUT AT STA 1304 (REPLACE) 1. I.A.W AMM TASK 52-37-01-004-001 REV.139 AND AMM TASK 52-37-01-404-021 REV.139 REPLACE THE JUMPER AT AFT CARGO DOOR AFT CUTOUT UP CORNER. 2.JOB COMPLETED AND CONDITION CHESDR IPXA2023091851359Unknown · unknownFAULT - TORN - JUMPER, AFT CARGO DOOR FWD CUTOUT UP CORNER STRUT AT STA 1204 (REPLACE) 1. I.A.W AMM TASK 52-37-01-004-001 REV.139 AND AMM TASK 52-37-01-404-021 REV.139 REPLACE THE JUMPER AT AFT CARGO DOOR FWD CUTOUT UP CORNER. 2.JOB COMPLETED AND CONDITION CHESDR FDEA202309141615Bolt · shearedFOUND LEFT WING INBD FLAP, INBD FLAP TRACK TRAILING EDGE UPPER LINK BOLT SHEARED. BACB30US14K31 REPAIR COMPLETED ON WO 86959, SEQ 19 AND E.A. H-2750-T0376213 A; BY REPLACING BOLT AND ALL DAMAGE WITHIN THE AREASDR FDEA202309131635Fairing · delaminatedDURING POST FLIGHT WALK AROUND, FOUND L/H INBD FLAP AFT PIVOT FAIRING BUCKLED. REF. IPC 27-51-03-21A, ITEM 275. REPLACED DAMAGED LEFT HAND AFT PIVOT FAIRING REF. B767 AMM 27-51-07-4-3 REPLACED DAMAGED LEFT HAND AFT PIVOT FAIRING REF. AMM 27-51-07-4-3SDR FDEA202309121583Floor Panel · delaminatedMAIN DECK FLOOR PANEL 241FFF REQUIRES PERMANENT REPAIR FROM RAMP REPORTED PUNCTURE. REF WRI 53211480 / EA# H-5321-T0375485. COMPLETED CORE PLUG AND LAY UP REPAIR ON MAIN DECK FLOOR PANEL 241FFF IAW B767 SRM 53-00-50-2R PARA GRAPH 4.DSDR FDEA202309081562Skin · delaminatedR/H ELEVATOR UPPER SKIN L/E IS DELAMINATED APPROX 16" OTBD OF THE INBD EDGE REPAIRED DAMAGE IAW FEDEX EA H-5520-T0376055-P1, RELEASED SEP 07, 2023, TITLED "STABILIZERS - ELEVATORS - RH ELEVATOR, UPPER SKIN ELEV STA 93, EDGE DELAMINAITON"SDR FDEA202309081560Unknown · unknownL/H ELEVATOR UPPER SURFACE IS GOUGED APPROX 9.5' O/B OF THE I/B HINGE. REPAIRED L/H ELEVATOR UPPER SURFACE NOTED DAMAGE BY PERFORMING PERMANENT WET LAY UP REPAIR IAW B767 SRM 55-20-01-1A , SRM 55- 20-01-2R , SRM 51-70-17-06 , FEDEX EA# H-5520-T0376037 NEW RESDR NACA2023090300001Unknown · unknownAPU FUEL FILTER POP OUT INDICATOR EXTENDED. REMOVED AND REPLACED APU FUEL FILTER ELEMENT IAW AMM 49-31-04 NO LEAKS NOTED.SDR NACA2023090100001Unknown · unknownFL350 EICAS CABIN ALTITUDE OVERHEAD PANEL - CABIN ALTITUDE PILOT'S CENTER PANEL, CABIN ALT LIGHT ILLUMINATED, YES. TROUBLESHOT CABIN ALTITUDE IAW B767 FIM 21-31 FAULT TREE 803, SYSTEM OK NO FAULTS FOUND.SDR FDEA202308311532Floor Panel · gougedMAIN DECK CARGO FLOOR PANEL DAMAGED AT STA. 1137 AND 3 INCHES LEFT OF CENTER. REF WRI 25-50 5384 AND SEQ 150 OF WORK ORDER 86663. FABRICATED AND INSTALLED NEW FLOOR PANEL. REF SRZ -25-005 REV. R AND B767 AMM 53-01-06-4. ALSO SEE WRI # 25-50/5384 AND SEQSDR NACA202308300001Outflow Valve · failedMI 0330Z FL 350 DIVERT TO KIN FOR CABIN ALTITUDE LIGHT ON EICAS. CABIN ALTITUDE/OUTFLOW VALVE UNCONTROLLABLE. CABIN ALTITUDE REACHED 14000 FEET. BELOW 18000 FEET AUTOMATIC CONTROLLER APPEARED TO WORK NORMALLY. OUTFLOW VALVE TESTED ON THE GROUND IN MANUAL, WORKSDR FDEA202308301539Wedge · dentedL/H WING OB FLAP HAS 2 EACH DENTS AT LOWER SURFACE BETWEEN 132" AND 152" FROM O/B END OF THE FLAP AND BETWEEN THE TRAILING EDGE TO 12" FWD. MARKED REPAIRED LH WING OB FLAP 2EA DENTS LOWER SURFACE 132" FROM OB EDGE TO 152" FROM OB EDGE AND BETWEEN TE EDGE TSDR IXXA2023082801Pylon · cracked#2 PYLON AFT OF BULKHEAD UPPER CLOSEOUT ANGLE IS CRACKED. REPLACED #2 PYLON AFT BULKHEAD UPPER CLOSEOUT ANGLE IAW BOEING DWG#311T1157-6,REA 47573FABO1 AND IAW B767-300 SRM 51-40-02 PARA 7D.SDR FDEA202308251492Floorbeam · cracked1EA FLOORBEAM ATTACH ANGLE IS CRACKED, INSIDE E&E COMPARTMENT ON LH SIDE AT STA 246, APPROX LBL 44 ON AFT SIDE OF THE FLOORBEAM REMOVED AND REPLACED FLOORBEAM ATTACH ANGLE IAW B767 SRM 51-40-02-0G, BAC DWG 141T5146 REV F, AND BAC DWG 141T5600, SHEET 4, REVSDR NACA202308284001Unknown · unknownDURING POST FLIGHT WALK AROUND #1 ENGINE #15 BLADE HAD A NICK ON LEADING EDGE. BLENDED #1 ENG FAN BLADE #15 WHICH IS 18" FROM BLADE TIP .015" WITHIN SERVICEABLE LIMITS AS PER PW AMM 72-31-02. NDT INSPECTION COMLETED.SDR FDEA202308241491Skin · delaminatedR/H I/B AILERON, LOWER SURFACE HAS SMALL AREA OF SKIN DELAMINATION NEAR I/B AFT CORNER. M.W.T. 0000553921 : DAVIES, ANDREW M - 24-AUG-2023 23:10 INSTALLED BONDED REPAIR ON RH IB AILERON LOWER SURFACE IN REF. TO 767 SRM: 57-60-01-2R AND 51-70-04. COMPLIED WSDR FDEA202308241490Wedge · wornRH WING #8 L/E SLAT, T/E WEDGE, LOWER SURFACE IS WORN JUST OUTBD OF THE INBD AUX TRACK REPAIRED DAMAGE ON THE RH WING #8 SLAT, T/E WEDGE, LOWER SURFACE IAW B767 SRM 57-43- 02-2R AND B767 SRM 51-70-10-2RSDR FDEA202308241489Wedge · wornRH WING #8 L/E SLAT T/E WEDGE LOWER SURFACE IS WORN JUST OUTBD OF THE OUTBD ROTARY ACTUATOR CONTROL ROD REPAIRED RH WING #8 SLAT, T/E WEDGE IAW B767 SRM 57-43-02-2R AND B767 SRM 51-70-10-2RSDR FDEA202308231483Former · crackedL/H WING L/E FORMER AT WS OSS 499 FOUND CRACKED. 0000553921 : DAVIES, ANDREW M - 23-AUG-2023 21:02 REMOVED AND REPLACED CRACKED FORMER REF E.A H-5720-T0368947 B PT3.SDR FDEA202308231482Former · crackedL/H WING L/E FORMER AT WS OSS 441 FOUND CRACKED. 0000392280 : BILLMAN, CRAIG B - 23-AUG-2023 21:09 REPLACED L.E. FORMER WS 441 AS REQUIRED PER SR67-57-002. AND EA H5720-T0368947 B PT3.SDR FDEA202308231481Slat · wornRH WING #9 L/E SLAT WEDGE LOWER SURFACE IS WORN JUST INBD OF THE INBD ROTARY ACTUATOR TIE ROD. ACCOMPLISHED PERMANENT REPAIR OF RIGHT WING #9 L/E SLAT T/E WEDGE LOWER SURFACE WORN AREA IAW B767 SRM 57-43-02-0I,B767 SRM 51-70-10 AND 57-43-02-2R FIG 201 SHEESDR IPXA2023082302235Door · dented*** SDR FILED OPEN *** DENT ON BULK CARGO DOOR DENT ON BULK CARGO DOOR FWD EDGE LOCATED 10€? FROM TOP AND 1.75€? FROM FWD EDGE. DENT IS 4.0€? / 1.75€? AND A/Y= 33.33.<BR>FOUND TO BE WITHIN LIMITS REF SRM 52-30-01-1A-1 FIG 101 SHEET 4, DETAIL 6SDR FDEA202308221477Floor Panel · crackedAFT CARGO FLOOR PANEL 154GF BROKEN. AFT CARGO FLOOR PANEL 154GF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.87 AUG 15/2023SDR NACA2023081900004Unknown · unknown#2 ENG #17 BLADE HAS NICK. REMOVED NICK AT #2 ENG BLADE #17. DISTANCE 2 3/8, LENGTH 0.591 DEPTH IS .073 IS WITHIN LIMITS IAW B767-300 AMM 72-31-02SDR NACA2023081900003Unknown · unknown#2 ENG #8 BLADE HAS NICK. REMOVED NICK AT #2 ENG BLADE #8. DISTANCE 11 1/8, DEPTH 0.65, LEGTH 0.458 IS WITHIN LIMITS. IAW B767-300 AMM 72-31-02SDR NACA2023081900001Unknown · unknown#2 ENGINE BLADE #2 HAS NICK. REMOVED NICK AT #2 ENG #2 BLADE DISTANCE 3/4 LENGTH =-204 DEPTH .054, IS WITHIN LIMITS IAW B767-300 AMM 72-31-02SDR NACA2023081700002Unknown · unknownNICK AT BLADE 2B 5 7/16 INCHES FROM ROOT 1/32 DEP 1/8 WIDTH. BLENDED NICK PER AMM B767 72-31-02 NDT GOODSDR NACA2023081700001Unknown · unknownCIRCULAR BEND AT BLADE 14B 2 INCHES FROM ROOT 1/32 DEEP 1/8 WIDTH #2 ENGINE. BLENDED BLADE BEND PER AMM 72-31-02, NDT GOOD.SDR NACA2023081600001Unknown · unknownON POST FLIGHT FOUND L ENGINE BLADE #15 DINGED AT TIP OF LEADING EDGE OUTWARD. REPAIRED BLADE #15 IAW B767 AMM 72-31-02. NDT GOOD.SDR FDEA202308161451Panel · crackedPANEL PN 146T5869-152 CRACKED FABRICATE NEW PANEL 146T5869-152 (252YFF) REF FEDEX DWG SRZ-25-005 REV R.SDR FDEA202308151440Transmitter · unknownGO AROUND FOR FLAP INDICATION. RIGHT FLAPS INDICATED 20 WHILE LEFT FLAPS INDICATED 25. NO MESSAGES OR ALERTS. SECOND APPROACH BOTH FLAPS WERE SET TO AND INDICATED 30 AS SELECTED. REMOVED AND REPLACED FLAP POSITION TRANSMITTER #8 PER AMM 27-51-45-2. SDR IXXA2023083101Panel · delaminatedL/H VERTICAL STAB BONDED SKIN PANEL IS DELAMINATED BETWEEN AUX SPAR AND FRONT SPAR RIB 10SDR NACA2023081400001Unknown · unknownLEFT PACK LIGHT OFF ILLUMINATED AFTER TURNING PACK ON AND PACK RUNNING. PERFORMED FIM 21-51 FT 803 BLOCK 1-8 SYSTEM SATISFACTORYSDR IPXA2023081468869Escape Reel · inoperativeEMERGENCY DESCENT DEVICE **OII 2** INSTALLED EMERGENCY DECENT DEVICE PER AM 25-60-00SDR NACA2023081100001Unknown · unknownCABIN ALT 2. CONTINUITY CHECKS/WIRE SHAKE TESTED OK. SWAPPED CABIN CONTROLLERS FOR TROUBLESHOOTING IAW AMM 21-31-02SDR FDEA202308111399Transmitter · failedON FINAL APPROACH, CONFIGURED FLAPS 20 TO 25 WITH GEAR DOWN. LEFT FLAP INDICATOR NEEDLE WENT TO 25, RIGHT FLAP NEEDLE INDICATOR REMAINED AT 20. ELECTED TO GO ROUND. NORMAL GO AROUND, RAN QRH FOR ASYMMETRY AND RETURNED FOR LANDING. NO ABNORMAL FLIGHT CHARASDR FDEA202308111398Pseu · failedGEAR DOOR LIGHT AND EICAS WARNING WITH GEAR INDICATING SAFE. UPON GO AROUND, GEAR DOOR LIGHT EXTINGUISHED. NEXT LANDING ATTEMPT THE GEAR DOOR LIGHT WAS ILLUMINATED AGAIN. LANDED UNEVENTFULLY. QRH PROCEDURE COMPLIED WITH AFTER GO AROUND. VERIFIED WITH SDR FDEA202308111397Former · failedNOSE FORMER ANGLE AT OSS 499.6 ON THE LEFT WING FIXED LEADING EDGE IS CRACKED. REMOVED THE BROKEN NOSE FORMER ANGLE AT OSS 499.6 ON THE LEFT WING FIXED LEADING EDGE. INSTALLED A 114T251U13 ANGLE. FEDEX DRAWING B67-57-002.SDR NACA2023081000001Unknown · unknownFLIGHT CREW REPORTING OIL COMING OUT OF APU AREA. OPENED APU AND CHECK OIL LEVEL, FOUND FULL. NO OIL LEAKS NOTED PER AMM 49-16-00SDR NACA2023080900001Unknown · unknownL ENG A/O VALVE EICAS MSG. DEFERRED PER MEL 75-21-02A CAT C ON 8/10/2023SDR 2023F00251Unknown · unknownDURING STARTING PREPARATION AND DEPARTURE FOR FLIGHT LCO542 (ASU -QSC), THERE WAS A FAILURE OF THE RIGHT ENGINE STARTER DURING IGNITION; MAINTENANCE PERSONNEL EVIDENCED THE PRESENCE OF SPARKS IN THE LOWER AREA OF THE COWLINGS CLOSE TO THE ENGINE STARTER LOCATISDR NACA2023080700001Unknown · unknownCABIN AUTO INOP LIGHT ON DESCENT @ 24800 FEET ABOUT 274 KNOTS. PERFORMED FIM TASK 21-31 FAULT TREE ON 803 ON CABIN CONTROLLER AND CABIN ALT IS ALREADY ON DMI # 21-31-01A CABIN CONTROLLER #1 NO FAULTS FOUND.SDR NACA2023080600001Controller · failedRIGHT PACK LIGHT SHOWED UP AT LANDING. DEFERRED RIGHT PACK IAW EL 21-51-01-01 CAT C. REPLACED RIGHT PACK CONTROLLER IAW AMM 21-51-14/401 POST INSTALLATION TEST OK. PACK TEMP CONTROLLER OPS CHECK GOOD IAW AMM 21-51-00SDR NACA2023080950002Unknown · unknownCABIN ALT EICAS MSG ON DESCENT INTO MIA. ASSOCIATED STATUS MESSAGE CABIN ALT AUTO 1 & 2. DEFERRED CABIN ALT 2 IAW MEL 21-31-01A CAT CSDR FDEA202308041358Aileron · dentedLH WING, OUTBOARD AILERON, LOWER SURFACE WITH DENT LH WING, OUTBOARD AILERON, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-60-02-2R DETAIL II AND B767 SRM 51-70-03-0G PAR 5.L FIG 16 (SHEET 1) REV 86 APR 15/2023SDR FDEA202308041357Aileron · damagedLH WING, OUTBOARD AILERON, TRAILING EDGE, OUTBOARD END WITH LIGHTNING STRIKE LH WING, OUTBOARD AILERON TRAILING EDGE OUTBOARD END WAS REPAIRED IAW E.A.#: H-2710- T0375526 RELEASE DATE: AUG 01, 2023SDR NACA2023080300002Unknown · unknownCABIN AUTO INOP EICAS LIGHT ON DESCENT. PERFORMED BITE PROCEDURES ON CABIN PRESSURE CONTROLLERS, NO FAULTS FOUND AT THIS TIME. IAW FIM 21-31 FT 803
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