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 FDEA202305220912Flap · damagedRH WING INBD MAIN FLAP UPPER SURFACE HAS EDGE DAMAGE ON OUTBD END. REPAIRED RH WING INBD MAIN FLAP UPPER SURFACE ON OUTBD END IAW FED EX EA H-5750- T0374487-P1-WING-FLIGHT SURFACES-RH INBD MAIN FLAP, FRANGIBLE STRUCTURE ASSY UPPER SKIN NICK.SDR FDEA202305200911Slat · gougedRIGHT WING #8 SLAT TRAILING EDGE LOWER SKIN HAS 2 GOUGES. REPAIRED RIGHT WING #8 SLAT LOWER SKIN IAW B767 SRM 57-43-02-1A AND 51-70-10-2R.SDR FDEA202305190910Flap · chafedRIGHT WING INBOARD FLAP LOWER SURFACE HAS CHAFFING WEAR MARKS ON EACH SIDE OF #6 FLAP FAIRING REPAIRED RIGHT WING INBOARD FLAP LOWER SKIN IAW B767 SRM 57-53-01-2R AND 51-70-03-0G.SDR FDEA202305190909Flap · gougedRIGHT WING INBOARD AFT FLAP HAS EDGE DAMAGE ON TRAILING EDGE UPPER SURFACE. REPAIRED RIGHT WING INBOARD AFT FLAP IAW B767 SRM 57-53-01-2R AND 51-70-10-2R.SDR FDEA202305190908Flap · gougedRIGHT WING INBOARD AFT FLAP HAS EDGE DAMAGE ON TRAILING EDGE UPPER SURFACE. REPAIRED RIGHT WING INBOARD AFT FLAP IAW B767 SRM 57-53-01-2R AND 51-70-10-2R.SDR FDEA202305190907Slat · chafed#5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF INBOARD AUX. TRACK. REPAIRED #5 SLAT WEDGE LOWER SKIN IAW B767 SRM 57-43-02-2R AND 51-70-10-2R.SDR FDEA202305190906Slat · chafed#4 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF INBOARD ACTUATOR CONTROL ROD. REPAIRED #4 SLAT WEDGE LOWER SKIN IAW B767 SRM 57-43-02-2R AND 51-70-10-2R.SDR FDEA202305180896Flap · delaminatedRIGHT WING, OUTBOARD FLAP, WITH DENT ON LOWER INTERNAL PART. RH WING OUTBOARD TRAILING EDGE FLAP, WEDGE ON LOWER SKIN AT POSITION OTEF 12.36: DAMAGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG. 201 PAG. 1-2 AND SRM 51-70-17- 0G PAG. 26, 49 FIG. 11 PASDR FDEA202305180895Slat · delaminatedRH WING SLAT N8 WITH DENT ON WEDGE AREA UPPER SURFACE OSS 448. RH WING SLAT N. 8 ON WEDGE AREA UPPER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R PAG. 1-2 AND B767 SRM 51-70-10-2R REP. 4 PAG. 150-151 FIG. 201 REV. 85 DEC15/2022SDR IXXA2023051702Skin Panel · delaminatedRH SKIN ON VERT STAB DELAMINATEDSDR IXXA2023051701Skin Panel · delaminatedRH UPPER HORIZONTAL SKIN PANEL DELAMINATED.SDR FDEA202305160879Display · failedR FMC WENT BLANK UPON ENGINE START. ACCOMPANIED BY SQUEAL OVER THE RADIOS, NOTICEABLE ELECTRIC SMOKE ODOR AND CIRCUIT BREAKER FMCS CDU POPPED. (E11) RETURNED TO GATE. R/R'D FO'S CDU PER AMM 34-61-02-4. CHECKS GOOD. ALL RADIOS CHECK GOOD IAW AMM 23-12-SDR IPXA2023052535629Flap · dentedLT I/B MAIN T/E FLAP HAS DENT EO 86959 REQ 2 PREVIOUSLY C/W ON T3F18E001TM9H, PLS SEE NEW FAULT T3F18E001TNY5SDR IPXA2023051535629Unknown · unknown**SDR FILED OPEN**LT I/B MAIN T/E FLAP HAS DENT COMPLIED WITH STEPS 1-5 OF EO 86959-PRELIM1SDR FDEA202305120861Skin · burnedFUSELAGE SKIN EXTERNAL SURFACE FOUND 4EA LIGHTNING STRIKES AT STA544- STA566 STGR38L- STGR39R REPAIRED THE FUSELAGE SKIN EXTERNAL SURFACE 4EA LIGHTNING STRIKES AT STA544- STA566 STGR38L- STGR39R PER B767 SRM51-40-02 & B767 SRM53-00-01-2R REPAIR.14. THE RESDR IPXA2026100479934Skin · damagedMAJOR REPAIR, NR 8 SLAT HAIL DAMAGE. ALL STEPS OF EO-98803-REQ1 COMPLETED.SDR IPXA2026100576324Slat · damagedMAJOR REPAIR, LEFT WING LEADING EDGE SLAT #3 DAMAGE ITEM HAS BEEN ADDRESSED REF T3F18E009S7KH. C/W EO-98774-REQ1.SDR IPXA2023100273411Unknown · unknownRT WING OUTBRD AILERON DAMAGE. PROVIDED EO-88303-REQ1. THE NEW MOMENT FOR THE AILERON IS -107.635LB-IN. OPENSDR FDEA202305090836Skin · dentedR/H WING INBD FWD FLAP LOWER SURFACE IS DENTED IN LINE WITH THE #8 MLG WHEEL ASSY. ACCOMPLISHED PERMANENT REPAIR OF DENT ON LOWER SURACE OF R/H WING INBRD MAIN FLAP IAW B767 SRM 57-53-01-2R FIG 201 DETAIL 1 SHEET 1 AND SRM 51-70-10-2R, 51-70-03-OGSDR FDEA202305050820Floorbeam · crackedCRACK IN ANGLE OF COCKPIT FLOOR BEAM AT BS 246 AND LBL 50, LEFT SIDE OF MAIN EQUIPMENT CENTER, ACCESS 119AL ANGLE OF FLOOR BEAM AT BS 246 AND LBL 50 WAS REPLACED I.A.W. SRM 51-10-02-0G PARAG. 9 AND FLOOR BEAM UPPER WEB WAS REPAIRED I.A.W. E. A. #: H-5310-TSDR FDEA202305050819Panel · dentedMDC SECTION 41 FLOOR PANEL 221DFF WITH DENTS. MDC, SECTION 41 FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305050818Panel · dentedMDC SECTION 41 FLOOR PANEL 221CFF WITH DENTS. MDC, SECTION 41 FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305050817Panel · dentedMDC SECTION 41 FLOOR PANEL 222AFF WITH DENTS. MDC SECTION 41 FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305050816Panel · dentedMDC SECTION 41 FLOOR PANEL 222BFF WITH DENTS. MDC SECTION 41, FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305050815Panel · dentedMDC SECTION 41 FLOOR PANEL 222CFF WITH DENTS. MDC SECTION 41, FLOOR PANEL 222 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305040811Flap · dentedDENTS ON INBOARD FLAP UPPER SURFACE NEXT TO INBOARD EDGE. RH WING AFT FLAP-INBOARD TRAILING EDGE FLAP, UPPER SURFACE, DENTS 1,6 WERE FOUND WITHIN ALLOWABLE DAMAGE LIMITS AND DENTS 2,3,4,5 OUT OF LIMITS WERE REPAIRED IAW SRM B767 57-53-01-1A FIG. 101 TABLESDR FDEA202305040810Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENTS AT 4-3" FROM LOWER EDGE AND 25" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SURFACE AT 3-4" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PASDR FDEA202305040809Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 9.5" FROM LOWER EDGE AND 11" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SURFACE AT 9.5" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PARSDR FDEA202305040808Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 12" FROM LOWER EDGE AND 39" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SURFACE AT 12" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PAR. SDR FDEA202305040807Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 8-10" FROM LOWER EDGE AND 55" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SURFACE AT 8-10" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PSDR FDEA202305040806Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 7" FROM LOWER EDGE AND 77" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PAR. 4.A. REV. 85 DEC15/2022SDR FDEA202305040805Flap · dentedRIGHT WING OUTBOARD FLAP LOWER SURFACE WITH DENT AT 11" FROM LOWER EDGE AND 71" FROM OUTBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SKIN AT 11" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PAR. 4.ASDR FDEA202305030802Bracket · damagedON CLIMBOUT LE FLAPS ASYM EICAS WHEN RETRACTING FLAPS FROM 1 TO UP, QRH COMPLIED, PAN PAN DECLARED. RETURN TO CRK RUNWAY 20, FLAPS 20 APPROACH. EMERGENCY DECLARED. UPON TROUBLESHOOTING LE SLATS ASYM, PERFORMED BITE TEST PSEU FOUND MESSAGE 286 LH SLAT #5 INBSDR IXXA2023050301Spoiler Panel · crackedNO 1 SPOILER IS CRACKED AND SEPARATED, FOUND OUT OF LIMITSSDR FDEA202305020796Bracket · crackedRIGHT WING I/B FIXED L/E CAVITY SUPPORT BRACKET IS CRACKED AT IFSS 283 REMOVED AND REPLACED RIGHT WING INBOARD LEADING EDGE TORQUE TUBE GUIDE BRACKET IAW B767 SRM 51-40-02 AND BAC DWG 114T1240, SHEET 6SDR FDEA202305010793Fuel Nozzle · failedAFTER TAKEOFF, HAD R ENG OVHT EICAS WITH ASSOCIATED R ENG OVHT CAUTION LIGHT COMPLIED WITH QRH RETURNED TO MEMPHIS MOMENTARY STATUS MESSAGE R ENG OVHT LP2 WE NEVER HAD EGT OVHT ON PRIMARY FLT INSTRUMENT PANEL. EMERGENCY DECLARED. TESTED LOOP RESISTANCE SDR FDEA202304290780Unknown · unknownPDIS 132 26-10 7156 28APR23 MEM OPEN U RIGHT ENG OVERHEAT INDICATION. ON CLIMB OUT. NO EXCEEDANCE NOTED. NO FIRE ALERT. ECAM MESSAGE OF RIGHT ENGINE OVERHEAT. RAN QRH. RETURNED TO KMEM. ***EMERGENCY DECLARED*** TROUBLESHOT PER FIM 36-10 SDR FDEA202304280779Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 222AFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 222 AFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304280778Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 222CFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 222 CFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304280777Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 222BFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 222 BFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304280776Access Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 221CFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 221 CFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304280775Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 221DFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 221 DFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2. REV. 85 DEC15/2022SDR FDEA202304270770Unknown · unknownON APP RECEIVED LEADING EDGE LIGHT, AIRPLANE WAS FULLY CONFIGURED WITH FLAPS 25. RAN THE QRH FOR LE SLAT DISAGREE AND FOLLOWED THE CHECK LIST TO THE LEADING EDGE SLAT ASYMMETRY CHECK LIST. THE AIRPLANE FLEW NORMALLY WITH NO ASYMMETRIC INPUTS. NO ASSOCISDR IXXA2023042701Seat Track · crackedFIRST OFFICERS FORWARD O/B SEAT TRACK IS CRACKED.SDR IXXA2023042604Roller Tray · corrodedROLLER TRAY CORRODEDSDR IXXA2023042603Web · corrodedFLOOR SUPPORT WEB CORRODEDSDR IXXA2023042602Failsafe · crackedLH STA. 955 FAIL SAFE STRAP CRACKEDSDR IXXA2023042601Panel · crackedPANEL 521BB CRACKED.SDR FDEA202304250764Transcowl · cracked#1 ENGINE LH THRUST REVERSER HAS SMALL FILLER PANEL ADJACENT TO TOP BLOCKER DOOR THAT IS CRACKED AND MISSING SOME MATERIAL. 0000392280 : BILLMAN, CRAIG B - 26-APR-2023 22:53 COMPLIED WITH EA T H-7830-T0374199 P1. (REPAIRED #1 ENG LH TRANS COWL INNNER UPPER SDR IXXA2023042404Skin · delaminatedVERTICAL AUX SPAR SKIN DELAMINATED
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