Boeing 767-432ER
Service difficulty reports · 3,098
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 = '767432ER' 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 = '767432ER' 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 DALA2025102007645Skin · corrodedSHIP 1812 AFT CARGO COMPARTMENT FOUND DRAIN HOLE AREA CORROSION AT BS 1087 BETWEEN S39R AND 39L. THE PRI629503-14 REV.0 COMPARED AND COMPLIED WITH (1253239)SDR DALA2025102007644Skin · crackedNUMBER 2 NACELLE STRUT FWD TORQUE BOX UPPER SPAR INBD FWD WIRING OPEN HOLE CUT-OUT FOUND CRACK AT ABOUT NAC STA 229. CORRECTIVE ACTION: REPAIRED AS PER PRI629501-14 (1253202)SDR DALA2025102007652Pca · leakingMISC/DE- RT HYD SYS QTY DECREASED AFTER TAKEOFF FROM GIG. QRH C/W. CREW DECLARED EMERGENCY INTO ATL FOR LONGER RUNWAY LANDING. R/R RT HYD SYS PCA FOR THE RT ELEV. (7621290)SDR DALA2025102007643Light · out of positionSHIP 1809 EMERGENCY EXIT LIGHTS AT 1R AISLE HAVE WHITE AND RED LIGHT ASSY'S SWITCHED. CORRECTIVE ACTION: REINSTALLED LIGHT ASSY'S IN CORRECT POSITION PER B767 MM 33-51 AND SERVICE CHECK PAPERWORK (6831644)SDR DALA2025101507552Spar Web · crackedDURING H CHECK AT STAG, A CRACK WAS NOTED ON THE NR 2 PYLON FWD UPPER SPAR WEB. A REPAIR WAS INSTALLED PER ER/A 629501-14 SECT. I. ACCOMPLISH ER/A 629501-14 SECT. II INSPECTION NOT TO EXCEED 25,783 TOTAL A/C FLIGHT CYCLES, THEN AT 12,000 FLIGHT CYCLE INTERSDR DALA2025101507551Light · looseL3 EMERGENCY LIGHT LOOSE. RESECURED THE L3 EMERGENCY LIGHT. (7359290)SDR DALA2025101507550Spar · crackedNR 2 NACELLE STRUT FWD TORQUE BOX UPPER SPAR HYD TUBE CLAMP FASTENER HOLE FOUND CRACKED. REPAIRED AS PER PRI629500-14 REV.0. THE PRI629500- 14 REV.0 COMPARED AND COMPLIED WITH ER/A629500-14. (1251312)SDR DALA2025101507547Seat Track · corrodedFOUND CABIN SEAT TRACKS SURFACE CORROSION AT STA 1373 LBL 88.5. REMOVED THE CORROSION AND MEASURED THE REWORKED AREA: THE DEPTH OF CLEANUP ON TOP OF TRACK IS 0.036">0.020". FOUND OUT OF LIMITS AS PER B767-400 SRM 53-00-52. (1245738)SDR DALA2025101507546Seat Track · corrodedFOUND CABIN SEAT TRACKS SURFACE CORROSION BETWEEN STA 402 AND STA 447 RBL 88. DVI CARRIED OUT AND FOUND A CRACK CAUSED BY CORROSION. TRIMMED OUT THE SEAT TRACK AT STA 511 RBL 88. ACCOMPLISHED THE REPAIR AS PER B767-400 SRM 53-00-52 (1245714)SDR DALA2025101507545Skin · crackedOPEN HOLE HFEC INSPECTION PERFORMED ON THE ALL FASTENNER HOLE(5 EA) AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER, FOUND CRACK ON THE NO.4 HOLE,THE CRACK AT 12:00 O'CLOCK DIRECTION. REPAIRED IAW B767-400 SRM53-10-01 (1244345)SDR DALA2025100707314Sign · dislodgedSHIP 1821 3L EXIT SIGN DISLODGED FROM CEILING. CORRECTIVE ACTION: EXIT SIGN RESECURED AS REQUIRED. OK FOR SERVICE. (7591112)SDR DALA2025100707312Light · inoperativeL1 SLIDE LIGHT INOP ON FAP. R/R L1 SLIDE LIGHT PER B767-400 AMM 33-51. OPS CHK GOOD. OK FOR SVC. (7377265)SDR DALA2025092907048Lens · damagedEMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: SWAPPED EXIT SIGN LENS AS REQUIRED. OK FOR SVC. (1216500)SDR DALA2025092907043Window · arcedSHIP 1809 FLT DECK LH NO.1 WINDOW FOUND ARCING. CORRECTIVE ACTION: REMOVED AND REPLACED FLT DECK LH NO.1 WINDOW AS PER B767-400, AMM 56-11-01 (1217262)SDR DALA2025092406969Light · detachedL3 DOOR OVERHEAD EMERGENCY LIGHT HANGING FROM CEILING. REATTACHED 3L DOOR EMERG SIGN (6967488)SDR DALA2025092406968Cover · looseEMERGENCY EXIT SIGN COVER LOOSE. SECURED HARDWARE ON EMERGENCY EXIT SIGN COVER. OPS CHECK GOOD. OK FOR SVC. (1214008)SDR DALA2025092406966Stiffener · crackedMFEC INSPECTION PERFORMED ON THE NOSE WHEEL WELL,RH VERTICAL STIFFENER, FOUND 01 EA CRACK,THE CRACK LOCATIONED AT WL177,THE LENGTH OF CRACK IS 0.15 INCH,AS MARKED. CORRECTIVE ACTION: ACCOMPLISHED W/C 5312-01186-02B FOR REPAIRING THE NOSE WHEEL, RH VERTICAL STISDR DALA2025091706835Skin · dentedRIGHT WING INBD AFT FLAP LOWER SURFACE AT 30" FROM OTBD FAIRING INBD SIDE FOUND DENTED. RT WING INBD AFT FLAP LOWER SURFACE AT 30" FROM OTBD FAIRING INBD SIDE DENT REPAIRED IAW SRM 51-70-10-2R-3, SRM 57- 53-01-2R-1, AND SRM 51-70-10-2R. (1201666)SDR DALA2025091706834Skin · chafedFOUND RT WING NR 9 SLAT LOWER SURFACE AT INBD AUX TRACK AREA CHAFED. RT WING NR 9 SLAT LOWER SURFACE AT INBB AUX TRACK AREA REPAIRED IAW SRM 57-43-02-2R-1, SRM 51-70-10-2R-4 & SRM 51-70- 10-2R (1201654)SDR DALA2025091706833Skin · wornNUMBER 5 SLAT LOWER SURFACE AFT EDGE FOUND WEAR, 40 IN FROM INBD EDGE. NR 5 SLAT LOWER SURFACE AFT EDGE REPAIRED IAW SRM 57- 43-02-2R-1 & SRM 70-10-2R-4 & SRM 51-70-10-2R (1201639)SDR DALA2025091706837None · noneCOMPLETE PRI ERA629252-14 ORIGINAL PRI REV O. COMPLETED ALL STEPS OF PRI ERA 629252-14 ORIGINAL PRI REV O (1199866)SDR DALA2025091506768Door Frame · crackedPERFORMED OPEN HOLE HFEC INSPECTION OF ALL FASTENER HOLES (5 EA) AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER ,FOUND 01 EA CRACK ON THE FASELAGE SKIN OF THE NO.4 FASTENER HOLE, THE CRACK LOCATIONED AT 2 O'CLOCK,THE LENGTH OF CRACK IS ABOUT 0.12 INCH, SDR DALA2025091506767Spar · crackedPERFORMED OPEN HOLE INSPECTION ON THE FORWARD UPPER SPAR HIDDEN PORTION OF CHORD,FOUND 01 EA CRACK ON THE FASTENER HOLE ON THE INBORD UPPER SPAR AT NSTA221.25, THE CRACK FASTENER HOLE ON LH PYLON UPPER SPAR AT NSTA 221.25 REPAIRED AS PER PRI 582037-14 REV 0 (SDR DALA2025091506766Seat Track · corrodedSEAT TRACK FOUND CORROSION AT STA 1263 AND STA 1324, RBL 88.5. THE CORROSION ON SEAT TRACK AT STA1263 AND STA1324 RBL 88.5 REPAIRED AS PER PRI 628835-14 REV 0 (1192827)SDR DALA2025091506765Battery Pack · inoperativeEMERGENCY PATH LIGHTS INOP AT RIGHT AISLE ROWS 41-49. R & R EMERGENCY BATTERY PACK (M6760) PER AMM 33-51. OPS GOOD. (7600524)SDR DALA2025091006684Cover · detachedSHIP 1819 EXIT SIGN COVER MISSING AT 3L. FOUND AND INSTALLED EXIT SIGN COVER. OK FOR SVC (7625268)SDR DALA2025091006685Skin · crackedFUSELAGE SKIN CRACKED AND RIVETS POPPED AT LAVATORY VACUUM BLOWER FORWARD EXHAUST PORT. REPAIRED PER ER/A 628936-14 REV. (1185817)SDR DALA2025090806619Skin · corrodedER/A 628936-14 REV ORIGINAL, REPAIR FWD VACUUM OUTLET CUTOUT CORROSION. C/W ERA 628936-14. (1185225)SDR DALA2025090806618Shear Tie · corrodedAFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1197+253,BETWEEN S-39L AND S-38L,REF CPCP TASK NO:53-558- 00. CORRECTIVE ACTION: DAMAGED SHEAR TIE REMOVED AND REPLACED AS PER B767- 400 SRM 51-40-02 (1182496)SDR DALA2025090806622Girt Bar · fodUPON ARRIVAL, FA'S DISARMED ALL DOORS, 4L DOOR WAS ACTUALLY PHYSICALLY DISARMED ACCORDING TO LEVER POSITION BUT THE LIGHT " ARMED" ON THE DOOR HANDLE AND AT THE 1L FA PANEL BOTH SHOW 4L STILL ARMED. CORRECTIVE ACTION: CLEANED THE DEBRIS FROM GIRT BAR AND LATCHSDR DALA2025083106424Computer · faultedDIV- TO KEF DUE TO INTERMITTENT VIBRATION WITH L DPC MESSAGE DISPLAYED. REPLACED LEFT DPC. OPS NORMAL.SDR DALA2025083106420Control Panel · inoperativeCREW DECISION TO RETURN TO JFK DUE TO REPORTED HEADING SELECT MODE INOP ON AFDS MODE CONTROL PANEL. LNAV AND VNAV FUNCTIONAL. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSP. REPLACED AFDS MCP.(7600056)SDR DALA2025090206512Light · malfunctionedEMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:601. GREEN RUNNING MAN SIGN PART OF EMERGENCY LIGHTS. NORMAL OPERATION. OPS CHECKED NORMAL IAW FIM 33-51. (1166256)SDR DALA2025090206510Switch · faultedR1 DOOR SLIDE ARMED LIGHT AT FWD F/A PANEL INOPERATIVE. R & R R1 DOOR ARMED STATUS LIGHT SWITCH ASSY AT FOWARD FAP PANEL. (1168017)SDR DALA2025083106423Computer · faultedDIV- TO LHR DUE TO INTERMITTENT VIBRATIONS FELT BY CREW. REPLACED ELEVATOR FEEL COMPUTER DUE TO ONE CHANNEL INOP.(7600378)SDR DALA2025081906207Interlock · brokenATB, RETURN TO JFK DUE TO GEAR DISAGREE AND GEAR DOOR MESSAGES AFTER GEAR RETRACT. C/W OW LANDING INSP. FOUND LMLG DOOR MTC ACCESS PANEL INTERLOCK MECHANISM OUT OF ADJ AND LT MAIN LANDING GEAR DOOR SAFETY PIN INSTALLED. REPAIRED AND ADJUSTED INTERLOCK MECHANSDR DALA2025081506111None · noneSHIP 1817 ROBBED PORTABLE EXIT SIGN AS SERVICABLE FOR A/C 1604. CORRECTIVE ACTION: INSTALLED PORTABLE EXIT SIGN REF B767 AMM 33-51 (7547804)SDR DALA2025081506110Wedge · wornNUMBER 8 SLAT T/E WEDGE LOWER SURFACE FOUND WORN 18" TO OB EDGE. CORRECTIVE ACTION: NO.8 SLAT T/E WEDGE LOWER SURFACE WORN REPAIRED 18" TO OB EDGE AS PER B767-400 SRM 57-43-02-2R-1 & SRM51-70-10 (1138882)SDR DALA2025081306041Engine · fireATB- -IFSD- LEFT ENGINE FIRE ON TAKEOFF, PERFORMED ENGINE IFSD. FOUND SEVERE DAMAGE TO THRUST REVERES AND CORE COWLS. REPLACED LEFT ENGINE.SDR DALA2025081306040Light · looseCABIN CREW REPORTS EMERGENCY EXIT BY 3L WAS LOOSE. RESECURED AS REQUIRED. LIGHTED SIGN OPS NML OK FOR SVC.SDR DALA2025081306036Battery Pack · inoperativeON SVC CHK, FOUND SEATS 20,21,22 FE & 30,31,32 GF EMERGENCY AISLE LIGHTS INOP. R&R BATTERY PACK FOR SEATS 20,21,22 FE & 30,31,32 GF PER B767- 400 AMM 33-51.SDR DALA2025081105960Structure · debondedRIGHT WING O/B FLAP INTERNAL STRUCTURE HONEYCOMB DISBONDING AT OTEF STA 190+5 UNDER FLAP PANEL 666MT IB AREA. RT WING O/B FLAP INTERNAL STRUCTURE HONEYCOMB REPAIRED AT OTEF STA 190+5 UNDER FLAP PANEL 666MT IB AREA IAW SRM 57- 53-01-2R-1, SRM51-70-10-2R-4, ANDSDR DALA2025081105959Spar · crackedPERFORMED OHEC INSPECTION OF THE FORWARD UPPER SPAR HIDDEN PORTIONS OF CHORD-CF6-80C STRUT,FOUND 01EA CRACK ON THE INBOARD FASTENER HOLE OF THE WEB AT NSTA221.25. REPAIRED AS PER PRI 581786-14.SDR DALA2025081105962Torque Box · damagedLEFT PYLON FWD TORQUE BOX UPPER SKIN FOUND EXISTING REPAIR AT NAC STA 221.25 TO NAC STA 237.5. REPAIR DESCRIPTION IN ER/A 581828-14.SDR DALA2025080505852Wedge · wornNUMBER 5 SLAT T/E WEDGE LOWER SURFACE FOUND WORN AT O/B EDGE TO 31.4 INCH. NR 5 SLAT T/E WEDGE LOWER SURFACE WORN REPAIRED AT O/B EDGE TO 31.4 INCH IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R.SDR DALA2025080505851Spar · crackedRIGHT PYLON UPPER SPAR BETWEEN NAC STA221.25 AND NAC STA237.5 FOUND CRACKED AROUND WIRE CUTOUT. THE R/H PYLON UPPER SPAR BETWEEN NAC STA221.25 AND NAC STA237.5 POWER FEEDER CABLE CUTOUT CRACK AREA REPAIRED IAW PRI 628061-14 REV 0, .COMPARED AND COMPLIED WITHSDR DALA2025080105781Spar · crackedRIGHT PYLON UPPER SPAR BETWEEN NAC STA221.25 AND NAC STA237.5 FOUND CRACK AROUND HYD CASE DRAIN LINE CUTOUT. DAMAGED AREA REPAIRED PER ER/A 00-628062-14.SDR DALA2025080105782Spar Web · damagedERA 628061-14 SECTION I ISSUED FOR REPAIR TO #2 PYLON FWD UPPER SPAR WEB AT POWER FEEDER CABLE CUTOUT. DAMAGED AREA REPAIRED PER ER/A 00-628061.SDR DALA2025080105780Tail Cone · damagedTAILCONE LT FUSELAGE SKIN AT STA1783 UNDER SEAL PANEL 313CLX FOUND ABRASION. DAMAGED AREA REPAIRED PER SRM 53-80-70.SDR DALA2025080105779Skin · damagedTAIL SECTION RH FUSELAGE SKIN AT STA 1730 UNDER SEAL PANEL 314CRX FOUND ABRASION. DAMAGED AREA REPAIRED PER SRM 53-80-01.
Back to Boeing 767-432ER