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 HALA0800408Wedge · delaminatedDELAMINATION ON SLAT POSITION 12 T/E WEDGE, 3 AREAS ON LOWER CLOSURE PANEL INBD END SLAT. REPAIRED PER SRM 57-43-02 AND 51-70-10.SDR DL76G080375Charger · inoperativeLT AND RT EMERGENCY EXIT SQUIB TEST DOES NOT WORK ON TEST 1 OR TEST 2. DISARMED OFFWING ZSCOPE SYSTEM IAW B767-300 AMM 25-65-00. REMOVED AND REPLACED M961 BATTERY CHARGER IAW B767-300 AMM 25-65-17. RE-ARMED OFFWING ESCAPE SYSTEM IAW B767-300 AMM 25-65-00. SDR DL76G080374Fuse · blownEMERGENCY LIGHTS L979, L9700, L975, L9699, L308, L333 ARE INOP. TROUBLESHOT SYSTEM AND DETERMINED PICO FUSE BLOWN. REMOVED AND REPLACED FUSE IAW DAL B767-300 MM 33-51-07. OPS CHECK GOOD IAW B767-300 AMM 33-51-07.SDR DL76G080373Wire · damagedOXYGEN MASK AT FWD MID LAV AND 28AB DID NOT DEPLOY. RECONNECTED CONNECTOR FOR FWD MID LAV DOOR ACTUATOR IAW B767-300 AMM 35-21-16. REPAIRED WIRES FOR 28AB DOOR ACTUATOR IAW SWPM 20-10-13. MANUAL DEPLOY GOOD IAW B767-300 AMM 35-21-00.SDR DL76G080372Lens · missingRT OVERHEAD AISLE EMERGENCY EXIT SIGN MISSING LENS. REMOVED AND REPLACED EMERGENCY EXIT SIGN LENS IAW DAL B767-300 AMM 33-51-01,TIMCO HMV CARD 41147SDR DL76G080371Light · inoperativeSEAT EMERGENCY LIGHTS AT 1A, 2A, 4A, 3G, 17G ARE INOP. RELAMPED SEAT EMERGENCY LIGHTS AT SEATS 1A, 2A, 4A, 3G, AND 17G, NO FAULTS NOTED ON OPS CHECK IAW B767-300 AMM 33-51-10.SDR DL76G080370Wire · brokenOVERHEAD LT AISLE EMERGENCY LIGHTS HAS BROKEN WIRE AT STA 1197+132. SPLICED REPAIRED BROKEN WIRE AT LT AISLE EMERGENCY LIGHT STA 1197+132 IAW B767-300 SWPM 20-30-12. NO FAULTS NOTED ON OPS CHECK IAW B767-300 AMM 33-57-05.SDR DL76G080365Battery Pack · dischargedRIGHT SIDE AFT 3 EXTERIOR EMERGENCY LIGHTS INOP. CHARGED BATTERY PACKS, OPS CHECK GOOD IAW B767-300 MM 33-51-07 WDM 33-51-00.SDR DL76S080362Apu · malfunctionedSMOKE DETECTORS AT STATIONS 214-215-219 SOUNDED DUE TO LIGHT OIL MIST IN THE CABIN, ALL 3 MID LAVS. THIS HAPPENS ONLY ON THE GROUND WITH APU AIR AND NO ENGS RUNNING. FWD APU TO MCO AND PLACARD PER MEL 49-11-01A. REPLACED APU PER M/M. LEAK CKS GOOD. GENERASDR DL76G080360Pin · looseL2 SLIDE LOCK BALL PINS ARE LOOSE. REMOVED AND REPLACED L2 DOOR SLIDE/RAFT.SDR DL76S080359Attach Fitting · corrodedNLG W/W LT AND RT NLG TRUNNION ATTACH FITTINGS. CORROSION IN FITTING BORES AND TOOLING DAMAGED FASTENER HOLES. OVERSIZED BORES AND INSTALLED NEW ENLARGED BUSHINGS.SDR HALA0800409Channel · crackedLT STRUT AFT FAIRING CHANNEL, INBD CRACKED AT FWD END. I/B AFT FAIRING CHANNEL PT NR 313T1380-243. REPLACED IAW SRM 51-40-02, REV 76.SDR HALA0800404Fairing · delaminatedRT ENGINE FAIRING 411AT DELAMINATION AT PREVIOUS REPAIR LOCATION. INJECTED EC9394 INTO AREA TO STABILIZE CORE, 4 CYCLE LIMIT, START AT 30164.SDR HALA0800410Channel · crackedLT STRUT AFT FAIRING CHANNEL OTBD, CRACKED AT FWD END. O/B AFT FAIRING CHANNEL PT NR 313T1380-241, REPLACED IAW SRM 51-40-02, REV 76.SDR HALA0800396Skin · dentedSUP - LT HORIZONTAL STAB HAS L/E DAMAGE IN 5 PLACES INBD, AND 1 PLACE OUTBOARD. NOT ON A/C DAMAGE REGISTER. PERMANENT SRM REPAIR CARRIED OUT IAW SRM 51-70-10, REPAIR 2, REFERENCE ANZ TI 190113615-0001 AND HAL FILE NR 594051.SDR HALA0800397Skin · dentedSUP - RT HORIZONTAL STAB HAS 3X L/E DENTS, NOT IN A/C DAMAGE REGISTER. PERMANENT SRM REPAIR CARRIED OUT IAW SRM 51-70-10, REPAIR 2 REF TI 190113615-0001 AND HAL FILE NR 594051.SDR HALA0800400Wire · exposedLEFT AFT LAV SMOKE DETECTOR WENT OFF DURING FLIGHT. FLIGHT ATTENDANT SAID WIRE WAS EXPOSED ON SMOKE DETECTOR, POSSIBLE TAMPERING WITH. INSPECTED LEFT AFT LAV SMOKE DETECTOR. NO FAULTS NOTED. OK FOR SERVICE.SDR HALA0800405Circuit Card · faultyETOPS SIGNIFICANT SYSTEM, INTERMITTENT LOWER EICAS STATUS MESSAGE "R ENG OH LP2". PERFORMED FIM 26-11-00 FIG 104. CLEANED NR 2 ENG O/H LP2 CONNECTORS AND REPLACED M960 LP2 O/H DETECTOR CARD PER AMM 26-10-01. OVERHEAT TEST CHECKED OK.
SDR HALA0800392Structure · damagedDENT FOUND ON LT SIDE, ABOUT 3M FROM TOP OF RUDDER. REPAIR IN WORK.SDR HALA0800389Keelbeam · corrodedCORROSION ON KEELBEAM TEE PIECES AT AFT EDGE OF PANEL 139AL,139BL, AND 139CL CORRODED AROUND NUTS QTY 3. CORROSION NOTED EXCESSIVE. TEE SECTIONS (3) INSTALLED ON KEEL BEAM IAW 51-40-02 SRM.SDR HALA0800391Access Panel · damagedVERTICAL FIN ACCESS PANEL 324 CLX HAS BUBBLE ON PANEL. PERMANENT REPAIR CARRIED OUT IAW HAL B767-300 SRM 55-30-01/201 AND 51-70-17, 200F WET LAY UP HOT BOND REPAIR.SDR DL76P080368Wire · out of positionWHEN BASE OF GRIMES LT TOUCHES FOOT SHOULDER HEATER SWITCH SPARKS ARE EMITTED. BOTH CAPT AND F/O SIDE. PULLED CB P-32 TO DEACTIVATE ALL GRIMES LTS FWD TO MCO AND PLACARD PER MEL 33-11-01. DISCONNECTED F/O LIGHT ASSY FRM TERMINAL STRIP FOR CIRCUIT ISOLATIONSDR HALA0800395Bracket · crackedAPPROX 1/2" CRACK TO LIGHT STRUCTURE BRACKET RT ENGINE STRUT NAC STA 298.93 - 297, INBD SIDE ATOP AND FWD OF PANEL 447 ELX. BRACKET MEASURES APPROX 3 INCHES BY 1 INCH AND ATTACHES STRUT AFT TORQUE BOX TO SIDE PANELS, FWD AND ABOVE HYDRAULIC SHUTOFF VALVE. RESDR HALA0800394Balance Weight · corrodedSURRFACE CORROSION FOUND LT AND RT ELEVATOR QUADRANT BALANCE WEIGHT X2. SURFACE CORROSION REMOVED PER SRM 51-10-02, REV. 76. SURFACE FINISH RESTORED PER SOFM 20-41-02 REV 104.SDR HALA0800390Sequence Valve · corrodedCORROSION ON MAIN L/G OPERATING SEQUENCE VLV ROD IN RT WHEEL WELL. REMOVED CORROSION AND CPC APPLIED AS PER SRM 51-10-02.SDR HALA0800393Access Panel · damagedRT HORIZONTAL STABILIZER CR PCA ACCESS PANEL ANCHOR NUT MISSING AND ANCHOR NUT RAIL CRACKED. CRACK BLENDED OUT IAW 767300 SRM 55-10-90 FIG 201. DAMAGE WITHIN LIMITS. INSTALLED NEW ANCHOR NUT IAW 767-300 SRM 51-40-02.SDR DL76S080326Wire · shortedON ARRV, FOUND C1 DOOR WILL NOT OPEN ELECTRICALLY. FOUND C/B TRIPPED ON P34 PANEL. FOUND WIRE IN BUNDLE JUST BELOW P34 HAD RUBBED ON FRAME AND SHORTED. REPAIRED WIRE PER PS DOOR OPS NORMAL.SDR DL76G080325Oven · sparksAFT GALLEY OVEN NR 3 HAD SPARKS ON TOP WHEN TURNED ON, PULLED C/B. PULLED OVEN AND INSPECTED OVEN AND AREA FOR EVIDENCE OF ELECTRICAL OR MECHANICAL DEFECT. NO TROUBLE FOUND. REACTIVATED OVER AND PERFORMED OP CK, NO DEFECT NOTED. AS PRECAUTION REPLACED OVENSDR DL76G080323Idg · inoperative90 MIN OUT OF MAN, THE CREW GOT A LT ENG IDG DRIVE LIGHT. AFTER FOLLOWING QRH 50 MIN LATER, THE APU FAILED AND WOULD NOT RESTART. LGCU SWAPPED WITH APU GCU. LEFT S/N 1195 AND APU NOW S/N 6111. IDG REPLACED. ENGINE RUN CARRIED OUT. IDG OPS NML. LEAK OK. SDR HALA0800386Blade · damagedETOPS SIGNIFICANT SYSTEM, ON WALKAROUND ON NR 2 ENGINE FOUND 1 DING ON BLADE 1, 9 APPROX 5 INCHES FROM BLADE ROOT AREA C PER MM 72-31-02-3-08-003. BLENDED BLADE PER MM TASK 72-31-02 AREA C LEADING EDGE. NEEDS DYE PENETRANT INSPECTION PER AMM 70-11-06/201. RSDR HALA0800387Keelbeam · corrodedCORROSION ON FUSE-KEEL BEAMS AT BL62, SEVERAL ANCHOR NUTS INSTALLED WITH STEEL RIVETS WHICH ARE CORRODING. REPLACED CORRODED STEEL RIVETS WITH CORRECT SOLID RIVETS IAW SRM 51-40-02.SDR HALA0800388Bulkhead · damagedSCRATCH FOUND ON AFT PRESS BULKHEAD ABOUT 16" TO RIGHT OF CENTER. BLENDED IAW SRM 53-80-05/101. ALODINED REWORKED AREA IAW SRM 51-20-01. REWORK VARIFIED WITHIN SRM LIMITS IAW SRM 53-80-08/101. MAX BLEND .003". REWORKED AREA PRIMED AND TOP COAT APPLIED IAWSDR HALA0800381Skin · corrodedLEVEL 1 CORROSION ON RT WING LOWER SURFACE, STRINGER L15, BETWEEN RIBS 5 AND 7, CORROSION ON FASTENER HEADS. AREA PAINT STRIPPED IAW SOPM 20-30-02, REV 104. LIGHT CORROSION REMOVED FROM FASTENER HEADS BY GLASS BEADING IAW SRM 51-10-02, REV 76, NEGLIGIBLE MATSDR HALA0800382Skin · corrodedLEVEL 1 CORROSION ON RT WING LOWER SURFACE, RIB 8 AFT OF STRINGER L-6, CORROSION ON FASTENER HEADS. AREA PAINT STRIPPED IAW SOPM 20-302, REV 104. LIGHT CORROSION REMOVED FROM FASTENER HEADS BY GLASS BEADING, IAW SRM 51-10-02, REV 76. NEGLIGIBLE MATERIAL REMSDR HALA0800372Attach Bracket · gougedNR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKET AT 2 O'CLOCK POSITION GOUGED. DAMAGE ON NOSE COWL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIG. 101, DETAIL 111, WITHIN SRM LIMITS.SDR HALA0800376Skin · damagedNR 1 SLAT HAS MINOR DAMAGE TO UPPER LEADING EDGE. BLENDED MINOR DAMAGE, MAX DEPTH OF REWORK AREA IS 0.0065", WITHIN LIMITS AS PER SRM 57-43-01, FIG 10, NOTE B, DETAIL 1V. SURFACE FINISH RESTORED IAW AMM 51-21-06.SDR HALA0800375Attach Bracket · gougedAT 2 ENG NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKETS AT 7 O'CLOCK POSITION GOUGED. DAMAGE ON NOSE COWL AFT BULKHEAD INNER RING, 7 O'CLOCK POSITION BLENDED IAW SRM 54-11-02/1A01, FIG 101, DETAIL 111, WITHIN SRM LIMITS.SDR HALA0800374Attach Bracket · gougedNR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKETS AT 5 O'CLOCK POSITION GOUGED. DAMAGE AT 5 O'CLOCK POSITION ON NOSE COWL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIGURE 101, DETAIL 111, WITHIN SRM LIMITS.SDR HALA0800373Attach Bracket · gougedNR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKET AT 3 O'CLOCK POSITION GOUGED. DAMAGE AT 3 O'CLOCK ON NOSE COWL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIG 101, DETAIL 111, WITHIN SRM LIMITS.SDR HALA0800380Skin · corrodedCORROSION ON RT WING LOWER SURFACE, RIB 7 AFT OF STRINGER L6, SURROUNDING RIVET HEADS. REPAIR IN WORK.SDR HALA0800379Skin · corrodedCORROSION ON RT WING LOWER SURFACE, RIB 8 FWD OF STRINGER L10, CORROSION FOUND SURROUNDING RIVET HEADS. REPAIR IN WORK.SDR HALA0800378Support Beam · crackedFWD CARGO BAY RH SIDE FWD OF CARGO BAY DOOR AT ST 500 SIDE PANEL ATTACHMENT BEAM CRACKED AT UPPER ANGLE, BRACKET THROUGH HOLE. CARRIED OUT REPAIRS TO SUPPORT ANGLE IAW 767-300 SRM 51-70-11, FIG 1. FABRICATED REPAIR PARTS IAW 767-33 SRM 51-70-11, FIG 1. APPLSDR HALA0800377Support Beam · damagedFWD CARGO BAY RT SIDE REAR OF CARGO DOOR AT ST 654 SIDE PANEL, ATTACHMENT BEAM CRACKED AT UPPER ANGLE BY HOLE. CARRIED OUT REPAIRS TO SUPPORT BEAM IAW 767-300 SRM 51-70-11, FIG 1. FABRICATED REPAIR PARTS IAW 767-300 SRM 51-20-11,FIG 1. APPLIED ALODINE 1200 SDR DL76G080315Slide · unsecureL1 DOOR SLIDE HAS BACK BOARD CABLE NOT ATTACHED. FOUND SLIDE PACK NOT SECURED ALONG ONE SIDE AND LOOSE ON THE OTHER SIDE. FOUND DUCT TAPE COVERING RETAINING CABLE HOLE AT TOP OF SLIDE. SLIDE REPLACED ON NR 00175 AND DL JIC 7809 SLIDE PART NBR 251004926 (DL)SDR DL76L080307Warning Message · false activationCENTER ADP PRESS LIGHT AND EICAS MSG. PERFORMED RESET PER FIM. CENTER ADP OPS CKS OK.SDR DL76L080306Apu · malfunctionedNO APU AIR FROM APU AFTER PUSH BACK. APU S/W OFF AND RESTARTED ALL NOW, OPS OK AIR SYSTEM ALL OK.SDR DL76L080298O-Ring · cutFLIGHT 117 - DECLARED EMERGENCY INTO ATL DUE TO LOSS OF CENTER SYSTEM HYD QTY AND PRESS LOST. UNEVENTFUL LANDING AND TAXI. FOUND CUT O-RING ON CTR SYS LCCA FILTER BOWL. REPLACED SAME CKS OK.SDR DL76S080297Elbow · crackedL ENG FIRE LP1 STATUS MESSAGE ABOUT 15 MINUTES INTO FLIGHT FOLLOWED BY ILLUMINATION OF L ENGINE FIRE WARNING LIGHTS. ENGINE SHUTDOWN IN ACCORDANCE WITH QRH. NOTE, FIRE SWITCH WAS PULLED, HOWEVER, FIRE BOTTLE WERE NOT DISCHARGED. FOUND NR 1 ENG LT HIGH PRESSSDR DL76L080296Angle · crackedNR 1 ENGINE PYLON MIDSPAR CLOSE OUT ANGLE FOUND CRACKED. REMOVED AND REPLACED CLOSE OUT ANGLE.SDR DL76P081248Engine · failedCREW REPORTS LOSING N2 INDICATIONS ALONG WITH A C1 MESSAGE EN ROUTE TO HNL ON FLT 1465. WHEN PMA STATOR REMOVED MTC NOTED THE PMA ROTOR DRIVE HAS FAILED. REPLACED RT ENGINE PMA.
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