Boeing 767-332
Service difficulty reports · 11,959
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 = '767332' 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 = '767332' 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 HALA2011120400565Warning Message · multiple failFLAP ASSY MESSAGE ON GROUND. ON GEAR RETRACTION, RECEIVED A GEAR UN-SAFE LIGHT. OPEN.SDR DALA1166900176Charger · inoperativeDURING DRC FOUND OVERHEAD EMERGENCY LIGHTS AT 23GF-28GF INOP. MAINTENANCE REPLACE THE BATTERY CHARGER FORM M732 BATTERY PACK. SYSTEM OPERATION IS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPSSDR HALA2011120300563Controller · malfunctionedETOPS SIGNIFICANT SYS - ATB - RT ENG BLEED LIGHT ON AT TOP OF CLIMB. COMPLIED WITH TSI IAW FIM 36-10-00 FIG 111 AND WD 36-11-62, WIRING BETWEEN BLEED CONTROL CARD AND HPC CONNECTOR, CHECKED GOOD. LEAK CHECKED ALL SENSE LINES, NO LEAKS FOUND. R & R HPC IAW MM 3SDR HALA2011120100558Filter · failedETOPS SIGNIFICANT SYS - AFTER ENGINE START, EICAS STATUS PAGE RT OIL FILTER. INSPECTED NR 2 ENGINE CHIP DETECTOR, NO DEFECTS. R & R RT ENGINE OIL FILTER ELEMENT, LEAK CHECKED NORMAL IAW AMM 79-21-04, OK FOR CONT SERVICE.SDR DALA1166421607Wedge · bulgedLT WING NR 2 SLAT T/E WEDGE UPPER SURFACE HAS A BULGE AND IS REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.SDR DALA1166411607Flap · dentedLT WING I/B MAIN FLAP LWR MID AREA IS DENTED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.SDR DALA1255770183Tee Fitting · damagedRT WING UPPER PITCH LOAD FITTING INBD TEE FITTING HAS SHORT EDGE MARGIN ON FASTENERS AND HAS BEEN REPLACED IAW ERA 507545-14AD, REV ORG NR 52474.SDR DALA1169141704Skin Panel · wornEMPENNAGE- RT HORIZONTAL STAB LWR AIR GATE FAIRING FWD CUTOUT LWR SKIN PANEL CHAFING WORN. REPAIRED PER B767-300 SRM 53-80-01 FIG 201 REPAIR 3 ITEM 3 DETAIL VI.SDR DALA1169131704Skin Panel · wornEMPENNAGE RT HORIZONTAL STAB LWR AIR GATE FAIRING FWD CUTOUT FWD SKIN PANAL CHAFING/WORN. DEFECTIVE SKIN PANEL REPLACED PER B767-300 SRM 53-80-01 FIG 201 REPAIR 3 ITEM 3 DETAIL VI.SDR HALA2011112800544Control Unit · malfunctionedFLAPS WOULD NOT EXTEND BEYOND 15DEG ACCOMPANIED BY T/E FLAP ASSYMETRY ANNOUNCIATION. USED ALTERNATE FLAPS TO EXTEND TO 30 DEG, NORMAL LANDING. ACFT ARRIVED WITH NO ASSYM MSG. HOWEVER T/E FLAP SHUTDOWN MESSAGE ON EICAS, ACCMO FIM 27-58-00/101 FIG 104 AND AMM SDR DALA1165011704Attach Fitting · crackedFS 927 RT AT STR 21R FRAME ATTACH FITTING CRACKED.SDR DALA1165001704Frame · crackedFS 903 LT AT STR 20L-21L FRAME INNER CHORD IS CRACKED.SDR DALA1164991704Frame · crackedFS 903 RT AT STR 20R-21R FRAME INNER CHORD IS CRACKED.SDR DALA1255330185Floor Support · corrodedBS 287 RBL 21 FLOOR SUPPORT SURFACE CORRODED. REPAIR IAW SRM 53-00-51, FIG 201, REPAIR 1.SDR DALA1171270130Power Supply · inoperativeEMERGENCY LIGHTS AT SEATS 25-34FG AND ROWS 35-44ABC ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY PER AMM. SYSTEM OPERATION IS GOOD.SDR HALA2011112500545Counterbalance · brokenL4 DOOR HARD TO CLOSE. FOUND COUNTERBALANCE BROKEN. R & R L4 DOOR COUNTERBALANCE ASSY IAW AMM 52-11-16. OPS CHECKED OK.SDR DALA1164731607Fairing · delaminatedLT WING I/B MAIN FLAP LEADING EDGE O/B FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND 51-70-05 PAR 5A(1) FIG 5.SDR DALA1164720179Wedge · delaminatedLT WING NR 5 SLAT T/E WEDGE IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202.SDR DALA1164710179Wedge · delaminatedLT WING NR 6 SLAT T/E WEDGE IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202.SDR DALA1164700179Wedge · delaminatedRT WING NR 11 SLAT T/E WEDGE IS DELAMINATED AND A HOT BOND REPAIR WAS INSTALLED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202.SDR DALA1306060127Sill · corrodedFUSELAGE AFT CARGO DOOR LOWER SILL FS 1270 UPPER CHORD. REPAIR IAW ERA 497875-14.SDR DALA1164770196Skin · damagedDURING LIGHTNING STRIKE INSP FOUND STRIKE AT STA 654+22 AT STR 32R TO BE OUT OF LIMITS. REPAIRED PER SRM 53-00-01 REPAIR NR 1. REPAIR WORKED ON NR 70. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPSSDR DALA1164620179Rib · crackedRT WING NR 12 SLAT I/B RIB FOUND CRACKED.SDR DALA1164601602Slat · crackedRT WING NR 7 SLAT FROM I/B 61 INCHES AND FROM T/E 4 INCHES FOUND A 0.375 INCH CRACK. METAL HOT BOND REPAIR PERFORMED AS PER B767-300 SRM 51-70-10 REPAIR 2 FIG 203.SDR DALA1164581602Skin · chafedLT WING NR 4 SLAT O/B EDGE RIB O/B SURFACE WAS FOUND CHAFED.SDR DALA1165050194Wire Harness · defectiveEMERGENCY LIGHT AT SEAT 23GF ARE INOPERATIVE. MAINTENANCE REPLACED THE HARNESS AT SEAT 23GF. SYSTEM OPERATION IS NORMAL.SDR HALA2011112300540Fan · malfunctionedETOPS SIGNIFICANT SYS - AFT EQUIPMENT EXHAUST FAN 1 LIGHT ON. RESET AFT EQUIPMENT EXHAUST FAN & OPS CHECKED OK.SDR DALA1165040130Charger · inoperativeSEAT MOUNTED EMERGENCY LIGHTS ROWS 25-34FG AND 34-46AB ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER M9010 SYSTEM OPERATION IS NORMAL.SDR DALA1164021602Flap · delaminatedRIGHT WING - O/B AFT FLAP T/E FOUND DAMAGE AT APPROXIMATELY 30" FROM I/B EDGE. RIGHT WING O/B AFT FLAP T/E AT APPROX 30" FROM I/B EDGE AREA COMPOSITE REPAIR CARRIED OUT AS PER B767-300 SRM 51-70-06 PAR 5D FIG 7 AND REF HX PROCESS CARD SEQ NO.GJX512057-1 FOR DSDR HALA2011112000533Isolation Valve · failedETOPS SIGNIFICANT SYS - LEFT ISOLATION VALVE LIGHT REMAINED ON AFTER ENGINE SHUTDOWN. REMOVED & INSTALLED NEW ISOLATION VALVE, OPS CHECKED OK IAW AMM 36-11-04-004-001.SDR HALA2011111800538Connector · dirtyETOPS SIGNIFICANT SYS - ATB - EICAS MESSAGE RT ENGINE BLEED VALVE. T/S IAW FIM 36-11-00 FIG 111, CLEANED CONNECTOR TO HPC, RECONNECTED CONNECTOR AND UNLOCKED VALVE, RAN ENGINE. RT ENGINE HPSOV OPS NORMAL, OK FOR SERVICE.SDR DALA1164170128Light · inoperativeEMERGENCY PATH LIGHTS AT R2 DOOR IN LAV WALL IS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.SDR DALA1164030192Light · inoperativeCEILING EMERGENCY LIGHT ABOVE SEAT 2B INOPERATIVE. REPLACED CEILING LIGHT ASSEMBLY PER AMM 33-51-05. OPS CHECKS NORMAL.SDR HALA2011111600527Warning Light · false activationETOPS SIGNIFICANT SYS - BTB EICAS RUDDER RATIO LIGHT ON AFTER ENGINE START. RESET LT AND RT RRCM PERFORMED FIM 27-21-00, FIG 104. NO FAULTS NOTED. OK FOR SERVICE.SDR DALA1501040192Fairing · crackedNR 3 AFT FLAP LINKAGE FAIRING CRACKED, AT 4 O'CLOCK POS .75 L/E. CARRIED OUT PERMANENT REPAIR SRM 51-70-17, PARA 4A, REV 91-03 AND PAINTED IAW SRM 51-2-01, REV 91.03.SDR HALA2011114000518Bulb · missingON OVERNIGHT CHECK, FOUND SEAT 1H FWD AISLE EMERGENCY LIGHT MISSING LENS & BULBS AND SEAT 2H BOTH AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED LENS AND BULBS. OPS CHECKED OK IAW AMM 33-51-00.SDR HALA2011114000517Blade · damagedETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK, FOUND NR 2 ENGINE, NR 33 BLADE FR. INDEX ON SPINNER HAS FOD DAMAGE. ACCOMPLISHED AMM 72-31-02, NR 2 ENGINE NR 33 BLADE FROM INDEX ON SPINNER.SDR HALA2011112000515Warning Message · false activationETOPS SIGNIFICANT SYS - APU ISOLATION VALVE STATUS MESSAGE. PERFORMED FIM 28-25-00/101, FIG 104, NO FAULTS NOTED, MESSAGE CLEARED OK FOR SERVICE.SDR HALA2011111100516Blade · damagedETOPS SIGNIFICANT SYS - FOUND .2500 X .2500 BLADE DAMAGE ON NR 2 ENGINE FAN. IAW AMM 72-31-02-801 WITHIN LIMITS AREA B, 4" BELOW BLADE SHROUD. BLENDED IAW AMM 72-31-02-801. OK FOR SERVICE.SDR HALA2011111000511Flap System · malfunctionedON APPROACH, SELECTED FLAPS 15 DEGREE, GOT EICAS FLAP DISAGREE MSG HANDLE IN DETENT AND FLAP GAUGE SHOWED APPROX 10 DEGREE. FOLLOWED PROCEDURE AND LANDED WITHOUT INCIDENT, ON FINAL ALL ALERTS OFF AND SEL FLAP 25 DEGREE, FLAPS MOVED TO 25 DEGREE NORMALLY. TROSDR HALA2011110900508Warning Message · false activationETOPS SIGNIFICANT SYS - RA DISPLAYED ON THE F/O ADI. RESET F/O RADIO ALTIMETER CIRCUIT BREAKER, BITE CHECKED OK, TEST 30 OK. LMP REMAINS IN LAND 3.SDR DALA1162860181Skin · damagedLIGHTNING STRIKE AT STA 1543 BL 0. REPAIRED PER ERA 497575-14. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPSSDR DALA1161941708Connector · not seatedEMERGENCY LIGHTS AT SEATS 21A-31A ARE INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR ON THE EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPERATION IS NORMAL.SDR DALA1161751703Flap · dentedTWO DENTS ON THE RIGHT I/B TRAILING EDGE FLAP UNDERNEATH. DENTS MEASURE ARE 4 INCH WIDTH AND 0.05 DEEP. SECOND DENT 3 INCH WIDTH AND 0.04 DEEP. PERFORMED METAL HOT BOND REPAIR PER B767-300 SRM 51-70-10 REPAIR 4 FIG 201 AND SRM 57-53-01 REPAIR 1 FIG 201.SDR DALA1161701703Panel · damagedNR 2 PYLON PNL 446CR HAS ELONGATED HOLES AND IS BEING REPAIRED ON A PRI WHICH IS LISTED AS A MAJOR REPAIR.SDR DALA1161401703Skin · dentedC2 DOOR REAR LWR EDGE IS DENTED AND IS MAJOR REPAIR AS PER PRI. REPAIRED IAW ER/A 496350-14 REV O.SDR DALA1161411703Door Frame · crackedFS 478 STR 23R FWD CARGO DOOR CUT OUT FRAME WEB IS CRACKED AND REPAIR IS LISTED AS MAJOR ON PRI. REPAIRED IAW ER/A 496355-14 REV O.SDR DALA1160891703Frame · crackedFS 903 RT AT STR 21R FRAME INNER CHORD IS CRACKED. REPAIRED IAW ER/A 496354-14AD REV O.SDR DALA1160901703Frame · crackedFS 903 LT AT STR 21L FRAME INNER CHORD IS CRACKED. REPAIRED IAW ER/A 496353-14AD REV 0.SDR DALA1160921703Access Panel · wornNR 1 ENG RT C-DUCT LWR REAR ACCESS PNL INTERIOR REAR EDGE WORN. LISTED AS MAJOR REPAIR ON PRI.
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