Boeing 767-232
Service difficulty reports · 2,991
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 = '767232' 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 = '767232' 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 DL767002134Skin · corrodedCORROSION FOUND ON CENTER SECTION WING SKIN. THE DAMAGE WAS ON THE OUTER SURFACE OF THE UPPER SKIN AT STRINGER U-17 AT LBL 88. ER/A 334963-14 REPAIRED DAMAGE.SDR DL767002132Pressure Panel · corrodedCORROSION FOUND ON THE RT MLG WHEEL WELL CANTED PRESSURE WEB. CORROSION LOCATED AT STA 960 BETWEEN RBL 85 AND RBL 90. ER/A 334987-14 REMOVED CORROSION.SDR DL767002096Skin · corrodedCORROSION DAMAGE FOUND ON THE UPPER SURFACE OF THE CENTER WING SKIN AND IN THE UPPER SPAR CAP AT STA 955, RBL 70 - 90. IN NORDER TO VERIFY REMOVAL AND FACILITRATE A REPAIR THE LOWER CHORD OF THE RBL 74.81 FLOORBEAM WAS CUT FWD TO THE DAMAGE AND THE AFT SECTIOSDR DL767002097Bulkhead · wornHOLE FOUND ELONGATED IN THE AFT BULKHEAD OF THE NR 1 PYLON ON THE LOWER FWD GSE HOLE (6TH FROM THE TOP). THE RIVET HOLES INSTALLED PER BOEING S/B 767-54-0010 WERE DOUBLE DRILLED. ADDITIONAL WEAR DAMAGE FOUND JUST BENEATH THE GSE HOLE. ER/A 396279-14.SDR DL767001900Outflow Valve · failedAT FL240 GOT CABIN PRESS AUTO CTL 2 EICAS MSG AND CABIN ALT EICAS MSG. BITE FAULTED NR 2 AC MOTOR. REPLACED OUTFLOW VALVE.SDR DL767001894Skin · dentedGROUND DAMAGE AT STA 1250 STR 30R. SKIN AND STRINGER DENTED LOCALLY. SKIN AND STRINGER ARE TRIMMED OUT AND REPAIRED. ER/A 369288-14 REV A.SDR DL767001859Skin · corrodedCORROSION WAS FOUND ON THE FUSELAGE SKIN AT THE FOLLOWING LOCATIONS; FS 1175 AND S-39L, FS 1197 AND S-39L, AND FS 1197AND S-39R. THE CORROSION WAS CUT OUT AND EXTERNAL REPAIR DOUBLERS AND TRIPLERS WERE INSTALLED PER ERA 334950-14 AT MV2.SDR DL767001797Fitting · tool damageTOOLING DAMAGE OCCURRED IN THE LT AND RT WING O/B PITCH LOAD FITTINGS. THE DAMAGE WAS LOCATED ON THE THIRD FROM BOTTOM HOLE ON THE VERTICAL LEGS OF THE BACK-UP FITTINGS. REWORK CONSISTED OF OS AND RE-COLD WORKING HOLES. ER/A 334916-14.SDR DL767001781Skin · gougedOUTER SKIN OF THE L-1 DOOR HAS BEEN GOUGED. REPAIR PER ER/A 388030-14.SDR DL767001798Bulkhead · damagedFOUR HOLES FOUND ELONGATED IN THE AFT BULKHEAD OF BOTH PYLONS. ON THE NR 1 PYLON I/B FLANGE, THE UPPER HOLE, THE SECOND FROM THE TOP, AND THE 5TH GSE FASTENER HOLE FROM THE TOP WERE DAMAGED. ON THE NR 2 PYLON, THE UPPER GSE HOLE ON THE I/B FLANGE WAS FOUND WSDR DL767001726Skin · wornPERFORMED SRM REPAIR 53-80-01-2-203. REF NR 336. REPAIR OF DAMAGE ON FUSELAGE SKIN ABOVE RT HORIZ STAB AT STA 1809.5.SDR DL767001704Fitting · damagedTHE O/B HOLE IN THE I/B SIDE OF THE LT KICKLOAD FITTING FOUND DAMAGED. THE HOLE WAS SLIGHTLY ELONGATED AND WORN UNDER THE NUT. THE HOLE WAS OVERSIZED AND SPOTFACED TO REMOVE DAMAGE. ER/A 334858-14AD.SDR DL767001674Skin · dentedA DENT WAS FOUND IN THE FUSELAGE SKIN AT STRINGER 28R, BETWEEN BS 632 AND 654. TO REMOVE DENT THE SKIN WAS CUT OUT, TO A SIZE OF 3.5 BY 5.5 INCH. SKIN DAMAGE WAS REPAIRED PER ERA 378344-14.SDR DL767001664Control Cable · frayedFOUND RUDDER CABLES RA-4 AND RB-4 FRAYED AT AFT RUDDER QUADRANT AT CENTERING MECHANISM. REPLACED CABLES.SDR DL767001647Bulkhead · damagedWEAR DAMAGE FOUND ON THE I/B FLANGES OF BOTH THE NR 1 AND NR 2 PYLON AFT ENGINE MOUNT BULKHEADS. THIS DAMAGE IN CONJUNCTION WITH MULTIPLE NUT PLATE ATTACH RIVETS ON THE NR 1 PYLON GSE ATTACH HOLE REQURED THE HOLE TO BE ENLARGED TO INCORPORATE NEAREST ATTACH RSDR DL767001646Skin · corrodedFUSELAGE SKIN FOUND CORRODED AND CRACKED AT STA 445 - 470, S-34R AND STA 466 AT S-33R S-34R. ER/A 334816-14.SDR DL767001617Skin · corrodedSKIN CORROSION WAS FOUND AT FS 786 AT STRINGER 38L AND WAS REMOVED WITH A 3 X 3 INCH CUTOUT. THE CUTOUT WAS NEAR AN EXISTING REPAIR FOR A 2 X 3 INCH REPAIR BETWEEN STRINGER 39L & 39R. THE EXISTING REPAIR WAS REMOVED AND BOTH CUTOUTS REPAIRED WITH SDR DL767001599Flashlight · inoperativeFLASHLIGHT AT 2R DOES NOT INDICATE CHARGE. FOUND LED INDICATOR INOP. REMOVED AND REPLACED FLASHLIGHT.SDR DL767001645Bulkhead · wornTHE UPPER GSE FASTENER HOLE IN THE AFT ENGINE BULKHEAD OF THE NR 2 PYLON WAS WORN AND ELONGATED. ER/A 334822-14.SDR DL767001679Skin · corrodedEXISTING SKIN REPAIR FOUND CORRODED AT STA 1373 STR 34L. DAMAGE FOUND IN SAME AREA AT THE TEAR STRAP AND STRINGER. TWO LARGE DENTS FOUND IN THE SKIN AT STA 1329 AND 1351 AT STR 34L. ER/A 334806-14 REV A.SDR DL767001613Skin · corrodedTHE CENTER WING, UPPER WING SKIN, LT SIDE FROM STRINGER U-18 TO STRINGER U-8 HAS SURFACE CORROSION CONCENTRATED AROUND FASTENER LOCATIONS. ER/A 334824-14.SDR DL767001611Bulkhead · canningAFT PRESSURE BULKHEAD OIL CANNED AT BL 0 AND LBL 7 AT LOWER END. ER/A 334742-14.SDR DL767001615Fitting · misalignedTHE LT AND RT SIDE LINK FITTINGS HAVE SHORT E/D HOLES IN ADDITION TO ONE OVERSIZED HOLE AND ONE SPOTFACE AREA. ER/A 334808-14.SDR DL767001614Skin · corrodedCORROSION FOUND ON THE UPPER SURFACE OF THE CENTER WING SKIN AT STA 955 APPROXIMATELY LBL AND RBL 72. ER/A 334764-14.SDR DL767001612Fitting · tool damageNR 8 RIB ENGINE SUPPORT FITTING DAMAGED AT THE EDGE OF HOLE LOCATION COMMON TO THE FITTING AND FRONT SPAR. THE HOLE IS THE FOURTH ONE UP FROM THE BOTTOM OF THE FITTING IN THE O/B ROW. ER/A 334807-14AD.SDR DL767001529Handle · stuckWHEN GEAR SELECTED DOWN GEAR DISAGREE LIGHT AND EICAS MESSAGE ILLUMINATED. ON APPROACH GEAR TOO LOW AURAL ANNOUNCED. FOUND GEAR HANDLE STUCK SLIGHTLY UP FROM DOWN DETENT PUSHED HANDLE DOWN, MESSAGE CLEARED AND AMBER GEAR LIGHT EXTINGUISHED. REMOVED AND REPLSDR DL767001569Strap · corrodedC-1 DOOR FWD FRAME FAIL-SAFE STRAP AT STA 539.5 BETWEEN S-25R AND 32R WAS FOUND WITH CORROSION DAMAGE. DURING CORROSION REMOVAL SEVERAL FASTENER HOLES WERE DAMAGED. 334775-14.SDR DL767001436Circuit Board · failedDURING ROUTINE MAINT FOUND COCKPIT EMERGENCY LIGHT ILLUMINATING DURING POWER DOWN. REPLACED CIRCUIT CARD.SDR DL767001427Slide · misinstalledR1 CABIN DOOR SLIDE NOT PROPERLY ATTACHED TO DOOR. REPLACED R1 DOOR SLIDE PER M/M, OPS CHECKS NORMAL.SDR DL767001368Skin · damagedTHE SKIN, BEARSTRAP DOUBLER, INTERCOSTAL CHORD AND WEB SURROUNDING THE ACS HATCH WERE DAMAGED WHEN THE A/C WAS LOWERED FROM JACKS ONTO A LADDER LEFT UNDERNEATH. NEW SECTION OF INTERCOSTAL CHORD SPLICED IN. WEB REPLACED AND SKIN DAMAGE REPAIRED WITH EXTERNAL SDR DL767001349Valve · malfunctionedAT FL350 WITH RT PACK ON GOT CABIN ALT EICAS MSG. TURNED LT PACK ON AND DID EMER DESCENT AND DIVERTED TO MEM. RT PACK TESTED GOOD. LT PACK VALVE INDICATION ON PREVIOUS DEFERRAL. REPLACED VALVE.SDR DL767001334Battery Pack · inoperativeEMERGENCY LIGHTS IN FIRST CLASS INOP. FOUND PINS 11 AND 12 WITH NO OUTPUT. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY. LIGHT OPN CHECKED GOOD.SDR DL767001370Skin · corrodedCORROSION FOUND ON THE UPPER SURFACE OF THE CENTER WING UPPER SKIN OVERLAYING THE REAR SPAR AT STATION 955 AND BETWEEN LBL 70 AND 80. 334562-14.SDR DL767001369Skin · damagedFUSELAGE SKIN FOUND DENTED AND INTERNAL BEAR STRAP DEFORMED IN AREA JUST AFT OF THE C2 CARGO DOOR OPENING AT STRINGER 31R. THE STA 1351 FRAME IS BUCKLED IN THE SAME AREA. ER/A 270824-14 REV A.SDR DL767001326Skin · corrodedFUSELAGE SKIN FOUND CORRODED AT STA 1082 AND STR-38L. DAMAGE TRIMMED OUT AND EXTERNAL DOUBLER AND TRIPLER INSTALLED. ER/A 334619-14.SDR DL767001319Skin · crackedCRACK INDICATIONS FOUND IN THE NR 1 AND NR 2 PYLON O/B SIDELOAD FITTING HOLES. BY REMOVING THE RT WING SKIN PANEL LAYER, IT WAS FOUND THAT THE CRACK INDICATION WAS CAUSED BY AN ENLARGED HOLE IN THAT LAYER, WHICH ACTS AS A SHIM IN THE STACKUP. NO CRACK INDICASDR DL767001283Skin · misrepairedSKIN REPAIR AT STA 566 AND STRINGER 32L FOUND WITH TIGHT FASTENER SPACING. EXISTING REPAIR REMOVED AND HOLE PATTERN CUT OUT. NEW DOUBLER INSTALLED TO REPAIR CUTOUT. STRINGER 33L ALSO REPAIRED IN THIS SAME FRAME BAY ER/A 334530-14.SDR DL767000915Battery Pack · inoperativeRT EMERGENCY CEILING LIGHT AT ROW 13 TO FWD ENTRY DOOR INOP. REPLACED BATTERY PACK, OPS NORMAL.SDR DL767000911Battery Pack · inoperativeALL LEFT SIDE EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS M736 AT M738. RELAMPED FWD SLIDE LIGHT, EMERGENCY LIGHTS CHECK GOOD PER M/M.SDR DL767000859Brace · mismanufacturedNR 1 ENGINE DIAGIONAL BRACE REPLACED WITH NEW THREE PIECE DIAGONAL BRACE ASSY TO MEET AD 200-07-05 REQUIREMENTS. NEW DIAG BRACE ASSY 0.033 INCH TOO SHORT WITH MAXIMUM SHIMMING ALLOWANCES. FABRICATED THICKER SHIMS WITH FAA APPROVAL. CORRECTIVE ACTION: 33432SDR DL767000812Bulkhead · corrodedCORROSION DAMAGE FOUND ON THE AFT FACE AND FLANGES OF THE REAR SPAR BULKHEAD FITTINGS. THE CORROSION IS LOCATED JUST FWD OF THE FWD EDGE OF THE MLH W/W UPPER PRESSURE WEB, AND PROCEEDS INTO THE VERTICAL RAD II OF THE MACHINED FITTINGS ON BOTH THE LT AND RT SISDR DL767000800Light · inoperativeON LAYOVER, FOUND 3 OVERWING EMERGENCY LIGHTS INOP. RELAMPED, CHECKS NORMAL.SDR DL767000612Light · inoperativeDURING LAYOVER, FOUND R1 DOOR EMERGENCY LIGHT INOP. REPLACED CHARGER, CHECKS GOOD PER MM.SDR DL767000308Bolt · damagedWHILE PERFORMING OPN 5940 RC587 FOUND TENSION TIE BOLTS ROTATING AT FS 1702. UPON INSPECTION FOUND BOTH BARREL NUTS L/R AFT POSTION AT FS 1702 HAD FAILED. FOUND TO BE HEAVILY RUSTED. ENGRG ISSUED ERA 373376-14 TO C/W E0 1-74297-12. BOLT AND NUT REPLACEMENTSDR DL767000271Unknown · odorDURING FLIGHT, AN ACIDIC SMELL FROM R2 DOOR AREA, OVERHEAD AFT RT LAV. FOUND C/B B-1 ON P-33 PANEL POPPED. C/B IS FOR NUMBER 1 EQUIP/GALLEY/LAV VENT FAN. FWD TO MCO. REPLACED K629 AND K835 RELAYS. OPS CHECK GOOD.SDR DL767000263Turbine · damagedNR 1 ENG HIGH VIBS 5.0 N-2 WITH HUM AND VIBRATION. FOUND DAMAGE TO TURBINE. REPLACING ENGINE.SDR DL767992832Battery · dischargedDURING SQUIB TEST, LT ESCQPE SLIDE DID NOT ILL WHILE PRESSING TEST 1 AND RT ESCAPE SLIDE DID NOT ILL WHILE PRESSING TEST 2. REPLACED LT OVERWING SLIDE POWER SUPPLY AND BATTERY. OPS CHECK NORMAL.SDR DL767992718Battery Pack · dischargedDURING LAYOVER, FOUND NR 1 SQUIB TEST INOP. LEFT OVERWING ESCAPE SLIDE. REPLACED BATTERY AND BATTERY PACK, OPERATION NOW NORMAL.SDR DL767992658Actuator · crackedA LOUD THUMP HEARD ON GEAR RETRACTION. AFTER GEAR WAS PUT TO THE DOWN POS THE LEFT GEAR GREEN LIGHTS WERE NOT ON AND HAD A GEAR DISAGREE AND DOORS DISAGREE LIGHTS. CREW LANDED UNEVENTFUL. MTC FOUND THE LT GEAR SIDE BRACE CRACKED AND THE BRACE BEYOND OVER CESDR DL767992631Skin · puncturedTHE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 1197 & 1219 AND BETWEEN STRINGERS 36L & 38L. STRINGERS 36L & 37L WERE CRACKED AND THE O/B SKIN FLANGE OF STRINGER 38L WAS CRACKED. THE DAMAGED SKIN WAS CUT OUT WITH A 10 X 18 CUTOUT AND THE DAMAGED FLANGE OF STR 38
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