Boeing 767-200
Service difficulty reports · 568
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 = '767200' 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 = '767200' 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 TAMF20060012SSkin · erodedDURING C-CHECK INSPECTION WAS FOUND A EROSION ON NOSE SKIN AT HORIZONTAL STABILIZER TIP - LT. DAMAGE WAS REPAIRED IAW EWO 767 55-001 AND BOEING SERVICE REQUEST ID: 1-171213467. ERODED AREA WAS CLEANED UP IAW SRM 55-10-30 PAGE 1 TO 3, THICKNESS MEASUREMENT PESDR TAMF20060011SSkin · crackedDURING C CHECK INSPECTION WERE FOUND 2 CRACKS AT FUSELAGE SKIN, STA 1654 STRINGER 3-4RT. DAMAGE WILL BE REPAIRED IAW EWO 767 53-008, SRM 53-80-01 REPAIR 4 - FIGURE 201, AND MFG SERVICE REQUEST ID 1-170241615. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAISDR ABXA060109Battery · inoperativeLEFT INTERIOR EMERGENCY LIGHT ABOVE DOOR IS INOP. T/S AND FOUND M735 PWR SUPPLY CHARGER INOP SWAPPED M735 AND M736, NOW CHECK OK M736 SPARE INOP. PRIMARY PWR SUPPLY CHARGER M735, OPS CHECK GOOD. DEFERRED DI NR 48990 DEFERRED PER GMM 01-07-04 FOR MAINT TRACKSDR TAMF20060009SSpar · crackedDURING INSPECTION C-CHECK, FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA WS 962 RT. DAMAGE WILL BE REPAIRED IAW EWO 767 57-006 AND BOEING SERVICE REQUEST ID: 1-170340546. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAIR.SDR TAMF20060008SSkin · chafedDURING C-CHECK INSPECTION WAS FOUND A CHAFING ON LT AFT FLAP INBOARD TRAILING EDGE STA IFS 108.25. DAMAGE WILL BE REPAIRED IAW EWO 767 57-008 AND BOEING SERVICE REQUEST ID: 1-171370438. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAIR.SDR TAMF20060007SSkin · chafedDURING C-CHECK INSPECTION, FOUND CHAFING ON RT AFT FLAP INBOARD TRAILING EDGE WS 108.25. DAMAGE WILL BE REPAIRED IAW EWO 767 57-007 AND BOEING SERVICE REQUEST ID: 1-171370438. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAIR.SDR TAMF20060005SBulkhead · crackedDURING INSPECTION CHECK WAS FOUND A CRACK ON NOSE WHEEL BULKHEAD RT VERTICAL CHORD STA 287, BL 25. DAMAGE WILL BE REPAIRED IAW EWO 767 53-006, SRM 57-70-12 FIGURE 1.SDR TAMF20060004SBulkhead · crackedDURING INSPECTION CHECK WAS FOUND A CRACK ON NOSE WHEEL BULKHEAD LT VERTICAL CHORD STA 287, BL 25. DAMAGE WILL BE REPAIRED IAW EWO 767 53-005, SRM 57-70-12 FIGURE 1.SDR TAMF20060010SSkin · corrodedDURING C CHECK INSPECTION WAS FOUND A CORROSION ON LEADING EDGE SLAT NR 5, STA WS 460.2. / DAMAGE WILL BE REPAIRED IAW EWO 767 57-009 AND MFG SERVICE REQUEST ID 1-171332193. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAIR.SDR TAMF20060003SDoor · delaminatedDURING INSPECTION CHECK WAS FOUND A DELAMINATION ON RT MAIN LANDING GEAR DOOR OUTER PANEL. RT MAIN LANDING GEAR DOOR WAS REMOVED AND REPLACED IAW B767 AMM 32-12-01 PAGE 401 TO 414 AND IT WAS PERFORMED OPERATIONAL TEST IAW B767 AMM 32-12-00 PAGE 501 TO 504, TSDR TAMF20060002SPanel · delaminatedDURING INSPECTION CHECK WAS FOUND A DELAMINATION ON LT HORIZONTAL STABILIZER UPPER OB ALUMINUM HONEYCOMB SKIN PANEL, BETWEEN LE STA 250.251 - FSS 305.361. SKIN PANEL WAS REMOVED IAW SRM 51-40-02 PAGE 1, SENT TO FAA RS UL6R925Y, REPAIRED IAW B767 SRM 51-70-10 SDR BB06021Battery · inoperativeFLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 14GF AND 22GF. MAINTENANCE REPLACED THE BATTERY AT ROW 16GF. NO FURTHER DIFFICULTIES.SDR BB06016Fuse · failedFLOOR LEVEL EMERGENCY LIGHTING BETWEEN ROWS ONE THROUGH SEVEN LEFT INOPERATIVE. REPLACED THE FORWARD BATTERY PACK FUSE. NO FURTHER DIFFICULTIES.SDR BB06011Connector · damagedLEFT SIDE FLOOR LEVEL EMERGENCY LIGHTS BETWEEN ROWS 9 AND 11 INOPERATIVE. MAINTENANCE SECURED A LOOSE PIN CONNECTOR AT SEAT 12B. NO FURTHER FAULTS.SDR BB06010Slide · failedDURING OPERATIONAL CHECK OF THE RIGHT OVERWING ESCAPE SLIDE, THE SLIDE DID NOT INFLATE. MAINTENANCE ACCOMPLISHED RIGGING OF THE CABLE TO THE INFLATION BOTTLE SQUIB.SDR BB06007Battery Pack · inoperativeEMERGENCY LIGHTING INOPERATIVE AT L1 AND R1 DOORS. MAINTENANCE REPLACED THE BATTERY PACK AT FWD F/A STATION. NO FURTHER FAULTS.SDR TAMF20060001ODuct · delaminatedDURING WEEKLY CHECK, FOUND DELAMINATION ON NR 1 ENGINE RT T/R (FAN COWL DUCT) INNER SKIN (DAMAGE MEASUREMENT IS 34 BY 13.5 INCH), CAUSED BY LIBERATION OF 2 OUTLET VANES ON IDG AIR/OIL COOLER ASSY P/N 35E38-5. FAN REVERSER P/N 683L136G08 WAS REMOVED AND TEMPORSDR ABXA060023A/C Pack · odorOIL ODOR COMING FROM RT PACK INFLIGHT DURING DESCENT TURNED OFF RIGHT PACK, ODOR WENT AWAY. PERFORMED AIR COND OIL CONTAMINATION TEST ON SYSTEM IAW AMM 21-00-21-2. NO CONTAMINATION NOTED.SDR BB05105Windshield · crackedFLIGHT 15, MUC-PHL: DURING CLIMBOUT, F/O WINDSHIELD CRACKED. A/C DIVERTED TO AMS FOR WINDSHIELD CHANGE. MAINTENANCE COMPLETED THE WINDSHIELD CHANGE. NO FURTHER DIFFICULTIES.SDR BB05104AConnector · looseFOUND FLOOR ESCAPE PATH LIGHTING INOPERATIVE ON RIGHT SIDE OF CABIN BETWEEN ROWS SIX AND TWELVE. MAINTENANCE RE-ATTACHED ROW 12 LIGHT CONNECTOR. NO FURTHER FAULTS NOTED.SDR BB05101Socket · disconnectedCABIN FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE ON RIGHT SIDE, ROWS 3-11 AND 28-29. MAINTENANCE RECONNECTED SOCKETS AT TWO LOCATIONS. NO FURTHER FAULTS NOTED.SDR BB05100Compressor · stalledAFTER TAKEOFF, LEFT ENGINE COMPRESSOR STALL. REDUCED LEFT ENGINE THRUST TO IDLE AND RETURNED TO FIELD AMS. MAINTENANCE ACTION PENDING. (OPEN)SDR BB05099Filter · dirtyON CLIMBOUT FROM SJU, RECIEVED E/M -RT ENG FUEL FILTER-. RETURNED TO SJU. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL FILTER AND CLEANED THE DIFFERENTIAL PRESSURE SWITCH CONTACTS. NO FURTHER DIFFICULTIES.SDR BB05098Module · malfunctionedON CLIMBOUT DURING FLAP RETRACTION GOT AILERON LOCKOUT EICAS MESSAGE FOLLOWED BY RUDDER RATIO EICAS MESSAGE. COULD NOT GET AUTO PILOT ENGAGED. MAINTENANCE REPLACED THE LEFT SAM MODULE.SDR USAABB05094Iru · failedFLIGHT 948, PHL-BCN: AFTER TAKEOFF, CREW RECEIVED CENTER IRS FAULT LIGHT WITH ASSOCIATED EICAS MESSAGE, DIVERTED. REPLACED THE CENTER IRS. NO FURTHER DIFFICULTIES.SDR TAMF20050007OSkin · dentedDURING INSPECTION CHECK, FOUND THE AIRPLANE HIT AT FUSELAGE SKIN, STA 172.5 STRINGER 21 RT BY A CARGO LOADING EQUIPMENT.REPAIR DOUBLER AS TEMPORARY REPAIR WAS INSTALLED IAW EWO 767-53-002, MFG SERVICE REQUEST NR 1-134757238 AND SRM 53-00-01 FIGURE 201. PERMANESDR TAMF20050006OSkin · crackedDURING TAKE OFF, THE CREW FELT A SUSPECTED BIRD STRIKE IN THE RIGHT PART OF THE AIRPLANE. DURING MAINTENANCE INSPECTION WAS FOUND A DENT AND CRACK ON THE NOSE SKIN AT SLAT NR 7. TIME LIMITED REPAIR WAS PERFORMED IAW EWO AND MFG APPROVAL NR 1-124395785-2 IN ORSDR ABXA050234Door · openDURING CLIMB-OUT AT FL260, A MODERATELY LOUD NOISE WAS HEARD AND EICAS MESSAGE LEFT FORWARD ENTRANCE DOOR ILLUMINATED. CABIN PRESSURE CONTROL REMAINED NORMAL. PASSENGER REPORTED THAT THE ENTRY DOOR LOCKING HANDLE HAD POPPED TO THE OPEN POSITION. AIRCRAFT WASDR TAMF20050005OWire · chafedDURING TAKEOFF EICAS MSG L/E SLAT ASSYM DISPLAYED & LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. THE AIRPLANE WAS RETURNED TO RNG FRM 27810500. WIRING W176-102-24 IN P-36 WAS REPAIRED IAW WDM 32-09-11 PAGE 1 SH 2. FIMSDR TAMF20050004OWindow · malfunctionedAFTER TAKE OFF A HEAVY NOISE IN THE LEFT SLIDE WINDOW WAS HEARD WITH THE LATCH HANDLE IN LOCK POSITION. THE AIRPLANE RETURNED TO BOGOTA.NR 2 OPENABLE WINDOW WAS INSPECTED AND OPERATIONAL CHECK WAS PERFORMED IAW AMM 56-11-02 PAGE 601-604 WITH NORMAL RESULTS. OVSDR ANCF200400051Heater · defectiveELECTRICAL SMOKE OF UNKNOW ORIGIN FROM THE CAPTAIN'S SIDE, BETWEEN THE LIGHT CONTROL PANEL AND THE GLARESHIELD PANEL, ACCORDING TO THE ABNORMAL CHECKLIST THE RECIRCULATION FANS AND THE UTILITY BUSES WERE SWITCHED OFF AND THE EQUIPMENT COOLING SELECTOR WAS SELESDR EVAS094001Shutoff Valve · failedWHEN AIRCRAFT FLEW TO 31,000 FT , CAPTAIN FOUND BOTH PACK TRIP OFF. AIRCRAFT DESCENT TO 10,000 FT, THEN LEFT PACK RECOVERED. FOR SAFETY REASON, AIRCRAFT DIVERTED TO MNL. ON GROUND CHECK, FOUND LEFT PRSOV (PRESSURE REGULATING SHUT OFF VALVE) MODULATING FUNCTSDR ABXA030031Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED SPARE BATTERY PACK FOR EMERGENCY LIGHTS. OPS CHECKED GOOD IAW MM.SDR ABXA020356Switch · inoperativeEMERGENCY LIGHTS WOULD NOT EXTINGUISH IN OFF POSITION. LIGHTS EXTINGUISHED IN ARMED POSITION AND ILLUMINATED IN ON. CLEANED AND LUBRICATED SWITCH (SW5) IN EMERGENCY CONTROL LIGHT PANEL. EMERGENCY LIGHTS OPS CHECKED GOOD IAW MM.SDR ABXA020325Battery Pack · dischargedDURING PREDEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE, WOULD NOT TEST. INSTALLED NEW EMERGENCY LIGHT BATTERY PACK IN THE LOWER POSITION. OPS CHECKED GOOD IAW B767 MM.SDR ABXA020311Cover · bindingEMERGENCY SLIDE WOULD NOT ARM WHEN MAIN ENTRY DOOR CLOSED. FOUND COVER FOR SLIDE BINDING. ADJUSTED DOOR COVER, SLIDE ARMS NORMAL.SDR ABXA020309Web · cracked#1 ENGINE STRUT AFT FAIRING SPAR WEB, FOUND ONE CRACK ON STIFFENER (P/N 313T1380-15), AND FOUR CRACKS ON WEB (P/N 313T1380-9). REPAIRED STRUT AFT FAIRING IAW REA B654-44936-MR.SDR ABXA020277Bolt · misinstalledWHILE INSPECTING THE OUTBOARD SUPPORT BEAM FOR THE LEFT FLAP, FOR AD2002-16-05, FOUND GAP AT FORWARD ATTACH BOLT. INSTALLED BOLT IAW EA27510002-002.SDR ABXA020294Shear Tie · corrodedFORWARD CARGO LOWER LOBE, STATION 742, BETWEEN STRINGERS 37 - 39 RIGHT, AND STRINGER 38 LEFT, CORRODED SHEAR TIES. REPLACED SHEAR TIES IAW SRM 51-40-02.SDR ABXA020296Cap · corrodedFORWARD CARGO LOWER LOBE, STATION 676, DEEP CORROSION ON UPPER CAP AT LEFT BUTT LINE 20. REPLACED CAP IAW SRM 51-40-02.SDR ABXA020285Strut · corrodedLEFT WING FIXED LEADING EDGE RIB, W.S. 456.98, HAD CORROSION IN ANTI-ICE TAIL DUCT TO LEADING EDGE SLAT AT WING FIXED LEADING EDGE RIB. REMOVED CORRODED RIB AND INSTALLED NEW STRUT IAW BOEING SRM 51-40-02, 57-41-09, AND BAC DWG 114T2202.SDR ABXA020293Frame · corrodedFORWARD CARGO LOWER LOBE, STATION 720, LEFT BUTT LINE 45, CORRODED UPPER CHORD. REPLACED CHORD IAW SRM 51-40-02.SDR ABXA020289Frame · crackedLEFT WING NR 6 INBOARD TRAILING EDGE FLAP AFT FAIRING FORWARD FRAME, FOUND CRACK. NO, THIS PART HAS BEEN PREVIOUSLY ACCOMPLISHED ON A/C SB 767-57-0014. THE COMPONENT THE PART IS INSTALLED ON, IS FLAP LINKAGE FAIRING NR 3. REPAIRED AREA IAW REA B657-44390.SDR ABXA020284Fitting · corrodedLT WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE FITTING ASSEMBLY BEARING BORE, HAD SURFACE CORROSION. THE CORROSION WAS FOUND ON THE SURFACE OF THE BORE, WHERE BEARING INSTALLS. REPAIRED AREA IAW REA B657-44910MR.SDR ABXA020295Cap · corrodedFORWARD CARGO LOWER LOBE, STATION 522, RIGHT BUTT LINE 25, DEEP CORROSION ON UPPER CAP. REPLACED CAP IAW SRM 51-40-02.SDR ABXA020287Spar · corrodedLT WING INBOARD TRAILING EDGE MAIN FLAP FRONT SPAR LOWER CHORD VERTICAL FLANGE BETWEEN FS 286 - 290, FOUND CORROSION. REPAIRED AREA IAW REA B657-44906MR.SDR ABXA020286Spar · corrodedRT WING INBOARD TRAILING EDGE MAIN FLAP MID SPAR UPPER FORWARD CHORD HAD CORROSION, WS 177 - 186 AND BETWEEN WS 252 - 261. REPAIRED AREA IAW REA B756-44900MR.SDR ABXA020298Floor Panel · corrodedFORWARD CARGO LOWER LOBE, STATIONS BETWEEN 544 - 610, FROM RIGHT BUTT LINE 10, LEFT BUTT LINE 10, CORRODED SHEAR FLOOR PANEL. REPLACED PANEL IAW N.R.C. LT 135 AND SRM.SDR ABXA020214Connector · not seatedEMERGENCY LIGHTS WOULD NOT STAY ON. FOUND EMERGENCY BATTERIES DEPLETED. CHARGED USING AIRCRAFT POWER. TROUBLESHOT WIRES IAW B767 WD 33-51-11. CHECKED GOOD. RESEATED PLUG D5124P. OPS CHECKED GOOD IAW B767 MM 31-51-00. EMERGENCY LIGHTS CHECKED GOOD.SDR ABXA020297Angle · corrodedLEFT WING, NR 1 PYLON SKIRT, LOWER CHORD MID SECTION, HAD INTERGRANULAR CORROSION. ALSO FROM MID TO AFT END FOUND SPOTS OF CORROSION. REPLACED CHORD (ANGLE) IAW SRM 54-51-71.
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