Boeing 767-32LF
Service difficulty reports · 74
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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 = '76732LF' 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 = '76732LF' 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 FDEA202607160937Transmitter · failedON APPROACH INTO LAS, SELECTED FLAPS 25 & CAPTAIN NOTICED FLAPS BECAME ASYMMETRICAL LEAVING 20. NEVER RECEIVED ANY INDICATION ON ICAS. VERIFIED DETENT OF 25. ELECTED TO GO BACK TO 20. TRIED TO CYCLE FROM 20-25 AGAIN, STILL SHOWED A FLAP ASSYM, DECLARED AN SDR FDEA202607100885Floor Panel · puncturedTWO PUNCTURES ON FLOOR PANEL 231QFF AT MDCC FLOOR PANEL 231QFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV.94 DEC 15/ 2025SDR FDEA202607090878Floor Panel · puncturedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232MFF HAS PUNCTURE DAMAGE. JM25 REPAIRED FLOOR PANEL 232MFF (P/N:143T5876-128) AT APPROXIMATELY AT STA 654 22 THRU 654 88 BETWEEN RBL-55 AND RBL 77. USING B767 SRM 53-00-50-2R FIG. 201. REPAIR 1. SH 1. THIS IS A MAJSDR FDEA202607090876Floor Panel · puncturedFIVE PUNCTURES ON FLOOR PANEL 231AFF AT MDCC. THE FLOOR PANEL 231AFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2, PAR 4.B, FIG 201, SHEET 2, REV 94. DEC 15/2025.SDR FDEA202607090875Floor Panel · puncturedMAIN DECK CARGO COMPARTMENT, 232NFF HAS PUNCTURE DAMAGE.JM24. REPAIRD FLOOR PANEL 232NFF, RBL77-TO RBL 88 BS 654.22 TO 676 IAW SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 2. MAJOR REPAIR. THIS FLOOR PANEL WAS REPAIRED ON AIRCRAFT.SDR FDEA202607090874Floor Panel · puncturedTHREE PUNCTURES ON FLOOR PANEL 232NFF AT MDCC FLOOR PANEL 232 NFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R, PAR. 4-B, FIG. 201, SHEET 2, REV 94 DEC 15/2025SDR FDEA202607090873Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231LFF AT MDCC FLOOR PANEL 231 LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607090872Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 242CFF AT MDCC FLOOR PANEL 242CFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201, SHEET 2, REV 94, DEC 15/2025.SDR FDEA202607090871Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231KFF AT MDCC FLOOR PANEL 231KFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202607090870Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 231LFF AT MDCC FLOOR PANEL 231LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202607070861Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231EFF AT MDCC FLOOR PANEL 231 EFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG.201 SHEET 2 REV.94 DEC 15/2025SDR FDEA202607070860Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231CFF AT MDCC FLOOR PANEL 231CFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607070859Floor Panel · damagedTWO PUNCTURES ON FLOOR PANEL 231DFF AT MDCC FLOOR PANEL 231DFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV.94 DEC 15/2025SDR FDEA202607070858Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 251KFF AT MDCC FLOOR PANEL 251KFF AT MDCC WAS REPAIRED IAW B767 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607070856Floor Panel · damaged2 PUNCTURE ON FLOOR PANEL 251KFF AT MDCC FLOOR PANEL 251KFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202607070855Floor Panel · dentedTHREE DENTS WITH DELAMINATION ON FLOOR PANEL 241AFF AT MDCC, THE FLOOR PANEL 241AFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607070853Floor Panel · damagedPUNTURE ON FLOOR PANEL 241KFF AT MDCC FLOOR PANEL 241KFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 94 DEC 15/2025SDR FDEA202607070850Floor Panel · damagedTWO PUNCTURES ON FLOOR PANEL 251PFF AT MDCC FLOOR PANEL 251PFF AT MDCC. REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2, REV. 94 DEC 15/2025SDR FDEA202607070849Floor Panel · damagedPUNCTURED FLOOR PANEL 232HFF AT MDCC FLOOR PANEL 232HFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV. 94 DEC 15/2025SDR FDEA202602090148Skin · wornRH WING, T/E MAIN FLAP, OTBD EDGE UPPER SURFACE HAS AREA THAT IS WORN INTO COMPOSITE. REPAIRED RT WING INBD MAIN FLAP OTBD EDGE UPPER SURFACE 23 INCHES FROM T/E IAW DRAWING 113T2204 AND SRM 51-70-05-0G. MAJOR REPAIR.SDR FDEA202602080146Floorboard · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252HFF DENTED. FABRCATED FLOORPANEL (252HFF) IAW DRAWING SR67-53-009 AND DRAWING 146T5869-10, RBL 77.50-12.85 BS 1197-1285 AND SR67-53-009.SEE JPF FOR ALL THE WORK PERFORMED. (THIS IS MAJOR REPAIR) INSTALLATION OF THISSDR FDEA202602070145Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 252GFF IS DENTED IN TWO LOCATIONS. FABRICATED NEW FLOOR PANEL 252GFF, RBL 54.75- RBL 77.5, STA 1197 22-1197 132 IAW DWG 146T5868-49, & SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. REMOVAL /SDR FDEA202602060139Floor Panel · delaminatedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222AFF HAS AREA OF DELAMINATION FABRICATED NEW FLOOR PANEL 222AFF, MPN 141T5856-107, RBL11 - RBL 33, STATION 285 - 412 IN REF TO BOEING DWG 141T5856-107 AND SR67-53-009. SEE JPF FOR ALL WORK PERFORMED. THIS IS A MAJSDR FDEA202602050134Floorboard · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF DENTED. FABRICATED NEW FLOOR PANEL MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF DENTED 222BFF, MPN 141T5856- 106,RBL33 - RBL 54.75, STATION 285 - 412 IN REF TO BOEING DWG 141T5856-106 AND SR67-53- 009.SESDR FDEA202602050131Floorboard · delaminatedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232MFF HAS AREA OF DELAMINATION. FABRICATED NEW FLOOR PANEL 232MFF, MPN: 148T5875-19 RBL 54.75- RB L 77.5, STA 654-784.5 IN REF. TO BOEING DWG 148T5875-19, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS SDR FDEA202602050130Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF HAS PUNCTURE DAMAGE. JM39. (INCORRECT REF. AND REWORK PROCEDURE USED FOR DAMAGED AREAS.) FABRICATED NEW FLOOR PANEL 251KFF, MPN: 146T5869-9, LBL 77.50- LBL 86.75, STA 1087-1207 IN REF. TO BOEING DWG 146T586SDR FDEA202601290098Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242VFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 242VFF, MPN: 145T5874-32, RBL 84.25 - RBL 74.25, STA 984.95-1087 IAW DWG 145T5874-32, AND SR67-53-009. PERFORMED. MAJOR REPAIR.SDR FDEA202601280096Floorboard · dentedFLOORBOARD 242VFF IS DAMAGED VFF SHOULD BE 242UFF. FABRICATED FLOOR PANEL 242UFF (MPN: 145T5874-34) AT STA 980.95 - STA1114.82, RBL 54.75 - RBL 74.25 IN REF TO BOEING DRAWING 145T5874-34., AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJORSDR FDEA202407141000Floor Support · crackedSTA. 266, APROX RT BL 20 FLOOR SUPPORT "V" BRACKET CRACKED. REMOVED AND REPLACED SUPPORT V BRACKET 141T5602-8 REF BOEING DRAWING 141T5601 REV C & B767 SRM 51-40-03-0G. THIS IS A MINOR REPAIRSDR FDEA202404120457Skin · damagedDURING HMV 1 AT INDY, A PRIOR LIGHTNING STRIKE WAS DISCOVERED AND ONE FASTENER LOCATION AT STA 452, ON STRINGER 30L WAS BLENDED TO 0.040 THICK FROM A 0.063 MATERIAL THICKNESS AT THIS LOCATION. THIS AREA WILL BE REPAIRED WITH A SRM 53-00-01-2R REPAIR 29 DOUSDR FDEA202403290445Skin · dentedRH OUTBD WING, #11 SLAT HAS SMALL DENT ON UPPER SURFACE. MARKED MK8 REPAIRED RH WING L/E # 11 SLAT TRAILING EDGE WEDGE TOP SURFACE AT WS OSS 856 IN REF TO 767 SRM 57-43-02-2R, PG 1-2 DETAIL I & III, FIG.201 SHEETS 1 & 2, 767 SRM 51-70-10-2R, THIS IS A MAJOSDR FDEA202403290442Former · mismanufacturedR/H L/E NOSE FORMER ANGLE MALFORMED AND HAS MORE THAN .037" GAP TO LEADING EDGE SKIN. ENGINEERING CONTACTED PER SEQUENCE 708 AND RECOMMENDS REPLACEMENT.SDR FDEA202403290440Former · misalignedR/H L/E NOSE FORMER ANGLE MALFORMED AND HAS MORE THAN .037" GAP TO LEADING EDGE SKIN. ENGINEERING CONTACTED PER SEQUENCE 708 AND RECOMMENDS REPLACEMENT. REF. SEQ 708 ON SAME WO FOR REPLACEMENT OF FORMER AT OSS 441 IAW FDX E.O.#:H-5720-E0368563C, WING-SECONSDR FDEA202209242364Switch · failedEMERGENCY EXIT UNARMED PUSH BUTTON LIGHT FELL APART DURNG RELAMPING ON PREFLIGHT. REPLACED ANNUNCIATOR I/A W M/M 33-16-02-2 OPS CHECKS GOOD REF M/M 33-51-08-4SDR FDEA202108011918Line · leakingAFTER BLOCK IN, MX REPORTED A HYDRAULIC MIST/DRIP FROM LEFT MAIN WHEEL WELL. CRASH FIRE AND RESCUE WAS CALLED. TRACED HYDRAULIC LEAK TO BRAKE PRESSURE TUBE ASSY, P/N 373T1200-375. REF IPC 32-41-65-01 ITEM 305. FOUND TUBE WAS KINKED, WITH LEAK LOCATED ASDR FDEA202106301624Controller · malfunctionedCABIN ALTITUDE EICAS WARNING CLIMBING THROUGH 10,000 FEET OUT OF KGSO. LEVELED THE AIRCRAFT AT 10,000, RAN QRH, CONSULTED GOC AND GSO MAINTENANCE. TRIED BOTH AUTO 1 AND AUTO 2. THEN MOVED THE CONTROLLER TO MAN. WERE STILL UNABLE TO CONTROL THE PRESSURIZATSDR FDEA202105201320Warning Message · false activationFWD CARGO DOOR CAUTION ON CLIMB OUT. CHECKED FWD CARGO DOOR PROX SENSORS 150,151,152,153, AND 154 WITH BREAKOUT BOX, ALL SENSORS CHECK GOOD, READING 4.8 MH ON150,151 AND 153(FAR) AND 5.4 MH ON 152, AND 5.8MH ON 154 (NEAR) WITH DOOR CLOSED. ALL SENSORS ALSO SDR FDEA202105201315Warning Light · false activationFWD CARGO DOOR CAUTION ON CLIMB OUT. RAN QRH. DECLARED EMERGENCY. RELEASED FOR SERVICE PER MEL : 52-71-01-01-B CATEGORY C. INSPECTED FWD LOWER CARGO DOOR. IT WAS CLOSED, LOCKED, VENT DOORS CLOSED AND VERIFIED CLOSED IN THE VIEWING WINDOWS. DEBRIEFED CREW SDR FDEA202104130909Angle · crackedMAIN DECK FLOOR SPLICE IS CRACKED REMOVED & REPLACED FLOOR SPLICE ANGLE IAW BAC DWG 146T5650SDR FDEA202104130908Angle · crackedMAIN DECK FLOOR SPLICE ANGLE IS CRACKED REMOVED & REPLACED ANGLE IAW BAC DWG 146T5650SDR FDEA202104130907Angle · crackedLH NOSE TUNNEL @ STA 246, LBL 50, FLOOR SUPPORT ANGLE IS CRACKED REMOVED & REPLACED ANGLE IAW BAC DWG 141T5600 SHEET 4 REV - & BAC DWG 141T5146 REV FSDR FDEA202104110887Angle · crackedAFT CARGO COMPARTMENT, FWD END-WALL, @ STA 1087 HAS CRACKED ATTACH ANGLE REMOVED & REPLACED ANGLE IAW BAC DWG 140T0130SDR FDEA2020091412173Cabin Pressure · malfunctionedPDIS 298 21-30 4361 1SEP20 MEM. NO PRESSURIZATION ON TAKEOFF MODE SELECTORS 1 OR 2 WOULD NOT WORK, USED MANUAL MODE REMAINDER OF FLIGHT, STAYED 20,000 AND BELOW. FACT 11SEP20 21:14 MEM, REF AMM 21-31-00-5 AND FIM 21-31 FAULT TREE 803. PERFORMED BITE TEST ONSDR FDEA2020090982145Skin · chafedRT WING NR 8 SLAT T/E LOWER SURFACE CHAFED AT INBOARD AUX TRACK. REPAIRED RT WING NR 8 SLAT T/E LOWER SURFACE, IAW B767 SRM 57-43-02-2R REPAIR 1, 51-70-10-2R FIG. 202.SDR FDEA2020090962136Skin · dentedLT WING INBOARD AFT FLAP LOWER SURFACE IS DENTED 10.5 INCHES AFT OF THE LEADING EDGE AND 31.5 INCHES FROM INBOARD SIDE. REPAIRED LT WING INBOARD AFT FLAP LOWER SURFACE IAW B767-300 SRM 57-53-01-0I, SRM 57-53-01-1A, SRM 57-53-01-2R, SRM 51-70-03 PARA 5 FIG 5 ASDR FDEA2020090962135Skin · dentedLT WING INBOARD AFT FLAP LOWER SURFACE IS DENTED AT TRAILING EDGE AND 64 INCHES FROM INBOARD SIDE. REPAIRED LT WING INBOARD AFT FLAP LOWER SURFACE, IAW B767-300 SRM: 57-53-01-1A, SRM 57-53-01-2R REPAIR 1, SRM 51-70-10-2R REPAIR 4. MAJOR REPAIR.SDR FDEA202009032088Skin · chafedLEFT WING #5 SLAT WING STATION OSS 441 IS CHAFFED ON LOWER SURFACE DUE TO WORKING RIVETS REPAIRED LEFT WING #5 SLAT IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4.SDR FDEA202009032087Skin · chafedLEFT WING #5 SLAT AT WING STATION OSS 499 IS CHAFFED ON LOWER SURFACE DUE TO WORKING RIVETS REPAIRED LEFT WING #5 SLAT IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4SDR FDEA202007171555Unknown · odorDURING DECENT, BELOW 16000 FT, THERE WAS A STRONG CIGARETTE LIKE SMELL EMITTING FROM AN UNKNOWN SOURCE. NO SMOKE WAS VISIBLE. THE ODOR DISSIPATED AFTER TAXI-IN. DURING DEBRIEF, CREW NOTED APU WAS NOT OPERATION DURING EVENT. INSPECTED THE FWD EQUIPMENT BASDR FDEA2020021430335Bearing · failedBRAKE TEMP LT ILLUMINATED ON BLOCK IN BRAKE TEMPS WERE 23/44/22/54 FOUND THAT THE #7 BRAKE OUTER BEARING FAILED AND IMPACTING THE WHEEL/ TIRE, REPLACED THE #7 BRAKE PER M/M 32-41-08-4-4 AND THE #7 WHEEL/ TIRE PER M/M 32-45-0-4. BRAKE TEMP TEST OK. WHE
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