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 L43A11230601Ballast · burnedENROUTE FROM JFK TO STN THE CREW REPORTED A SMELL OF SMOKE IN THE COCKPIT AREA JUST AFTER A CREW MEMBER FLUSHED THE FWD LAV. THERE WERE NO VISUAL SIGNS OF SMOKE AND NO FIRE/OVERHEAT WARNINGS. THE CREW FOLLOWED THEIR QRH PROCEDURE SWITCHED THE UTILITY BUS TOSDR ABXA060289Heater · odorCAPTAIN NOTICED HEAT AND BURNING ODOR. TURNED OFF CAPTAIN'S FOOT HEATER AND ODOR STOPPED. SHOULDER HEATER WAS NOT ON. REMOVED AND REPLACED FOOT AIR SUPPLY HEATER IAW B767 MM 21-45-01-4. OPS CHECKED GOOD.SDR SCS4200600001Blade · out of toleranceENGINE WAS REMOVED FROM SERVICE DUE TO A DAMAGE IN C9 BLADE (AREA "E") OUTSIDE BLENDABLE LIMITS ACCORDING TO P&W ENGINE MANUAL. THE DENT WAS DISCOVERED BY BOROSCOPE INSPECTION. DEPTH OF DAMAGE= APPROX .037 , BLEND LIMIT =.031. DURING SHOPVISIT THE BLADE WAS MISDR TAMF20060049SSkin · corrodedDURING INSPECTION C1 CHECK, FOUND CORROSION AT FUSELAGE SKIN - STA 1307-1329 - LT. DAMAGED AREA WAS REPAIRED IAW EWO B767-53-027 AND MFG SERVICE REQUEST ID 1-224967922. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060046SSkin · dentedDURING INSPECTION, C-CHECK FOUND A DENT OUT LIMITS AT APU ACCESS DOOR OUTER SKIN STA 1865 TO 1873 - LT. DAMAGED AREA WAS CUT OUT AND INSPECTED BY NDT PROCEDURES, DOUBLER WAS FABRICATED AND INSTALLED IAW EWO 767 52-003 AND SRM 52-40-01 REPAIR 3. THIS REPAIR COSDR TAMF20060047SFailsafe · corrodedDURING C1 CHECK WAS FOUND CORROSION AT FUSELAGE SECTION 46, AFT CARGO DOOR STRUCTURE UPPER MAIN SILL FAILSAFE STRAP AT BS 1287 AND BS 1307. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-025 AND MFG SERVICE REQUEST ID 1-224967878. THIS REPAIR CONSTITUTES A MAYOR RESDR TAMF20060045SSkin · corrodedDURING INSPECTION, C-CHECK FOUND A CORROSION AT FUSELAGE SECTION 46 - LOWER SKIN AT TCAS ANTENNA DOUBLER. DAMAGE WILL BE REPAIRED IAW EWO 767-53-024 AND MFG SERVICE REQUEST 1-224967985. THIS REPAIR CONSTITUTES A MAJOR REPAIR AND FORM 8100-9 WILL BE ISSUED.SDR TAMF20060048SSkin · corrodedDURING C1 CHECK, FOUND CORROSION AT FUSELAGE SECTION 43, CARGO DOOR SURROUND STRUCTURE, CORROSION, FWD LARGE CARGO DOOR STRUCTURE AT THE MAIN STILL FAIL-SAFE STRAP AT STA 612.AFTER BLENDED REMAINING THICKNESS IS 0.142 INCH. DAMAGED AREA WAS REPAIRED IAW EWO BSDR TAMF20060043SChannel · crackedDURING INSPECTION, IAW EO 767 53-006 (AD 2005-02-02, SB 767-53A0113) WAS FOUND CRACK AT VERTICAL CHORD, STA 287 BL 25 - RT. DAMAGE WILL BE REPAIRED IAW EWO 767 53-022, SRM 53-10-14 AND SRM 51-70-12. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060042SChannel · crackedDURING INSPECTION IAW EO 767 53-006 (AD 2005-02-02, SB 767-53A0113) WAS FOUND CRACK AT VERTICAL CHORD, STA 287 BL 25 - LT. DAMAGE WILL BE REPAIRED IAW EWO 767 53-006, SRM 53-10-14 AND SRM 51-70-12. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060044SSkin · dentedDURING INSPECTION, C-CHECK FOUND DENT OUT OF LIMIT AT FUSELAGE SKIN - STA 1746 STR 36 - LT. DAMAGE WILL BE REPAIRED IAW EWO 767 53-023 AND SRM 53-00-01 FIGURE 201. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR ABXA060225Servo · defectiveEXPERIENCED UNCOMMANDED RUDDER INPUTS ALL PHASES OF FLIGHT WITH AUTO PILOT ENGAGED AND OFF AS WELL. GAINED ACCESS TO RUDDER YAW DAMPERS AND INSPECTED ACTUATORS. FOUND ACTUATOR LEAKING FROM SERVO RUDDER. REMOVED AND REPLACED ACTUATOR IAW B767 MM 22-21-02.4. SDR TAMF20060041SSill · corrodedDURING C CHECK INSPECTION WAS FOUND CORROSION ON FWD CARGO DOOR CUTOUT EXTERIOR LOWER MAIN SILL STRAP BETWEEN STA 522-588. REMOVED AND REPLACED LOWER MAIN SILL AT FWD CARGO COMPARTMENT IAW SERVICE REQUEST IS 1-214773777 AND B767 SRM 51-40-02 PAGE 1-7.SDR TAMF20060040SSill · corrodedDURING C CHECK INSPECTION WAS FOUND A CORROSION ON FWD CARGO COMPARTMENT LOWER MAIN SILL, BELOW NUT PLATE AT STA 588. REMOVED AND REPLACED LOWER MAIN SILL AT FWD CARGO COMPARTMENT IAW MFG SERVICE REQUEST ID 1-214773777 AND B767 SRM 51-40-02 PAGE 1-7.SDR TAMF20060038SSkin · dentedDURING C1 CHECK WAS FOUND A DENT OUT LIMIT AT FUSELAGE SKIN STA 347, 368 STRINGER 17 LT.PROPOSED CORRECTIVE ACTION: DAMAGE WILL BE REPAIRED IAW EWO 767-53-019 AND SERVICE REQUEST 1-214667810 AND SRM 53-10-14. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060036SStringer · crackedDURING C1 CHECK WAS FOUND A CRACK ON S27L AT STA 375.8 RT, WING DRY BAY UPPER. DAMAGE WILL BE REPAIRED IAW EWO 767-57-012 AND BOEING SERVICE REQUEST 1-215286670. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060039SSkin · dentedDURING C1 CHECK WERE FOUND DENTS OUT OF LIMITS AT BULK CARGO DOOR OUTER SKIN LOWER FWD CORNER LEFT. DAMAGE WILL BE REPAIRED IAW EWO 767-52-002 AND BOEING SERVICE REQUEST 1-215286201. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060035SBulkhead · crackedDURING C1 CHECK INSPECTION WAS FOUND A CRACK AT NOSE WHEEL WELL BULKHEAD STA 287 BL 25 RH VERTICAL CHORD. DAMAGE WILL BE REPAIRED IAW EWO 767-53-018 AND SRM 53-10-14, 51-70-12. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060034SBulkhead · crackedDURING C1 CHECK INSPECTION WAS FOUND A CRACK AT NOSE WHEEL WELL BULKHEAD STA 287 BL 25 LH VERTICAL CHORD. DAMAGE WILL BE REPAIRED IAW EWO 767-53-017 AND SRM 53-10-14, 51-70-12. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060037SSkin · corrodedDURING C1 CHECK WAS FOUND SKIN CORROSION AT FUSELAGE STRINGER 36L, STA 1307. DAMAGE WILL BE REPAIRED IAW EWO 767-53-020 AND MFG SERVICE REQUEST 1-215510848. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060033SSkin · crackedDURING C1 CHECK INSPECTION WAS FOUND A CRACK AT FUSELAGE SKIN STA 1725.5 STRINGER 7 RT. DAMAGE WILL BE REPAIRED IAW EWO 767-53-016 AND SRM 53-80-01. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060032SSkin · crackedDURING C1 CHECK INSPECTION WAS FOUND A CRACK AT FUSELAGE SKIN STA 1654 STRINGER 3-4 LT. DAMAGE WILL BE REPAIRED IAW EWO 767-53-015 AND SRM 53-80-01. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20060031SSkin · crackedDURING C1 CHECK INSPECTION WAS FOUND A CRACK AT FUSELAGE SKIN STA 1654 STRINGER 3-4 RT. DAMAGE WILL BE REPAIRED IAW EWO 767-53-014 AND SRM 53-80-01. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR BB06049Connector · looseRIGHT SIDE FLOOR LEVEL LIGHTS INOPERATIVE BETWEEN ROWS 1 - 9. MAINTENANCE FOUND A LOOSE CONNECTION AT ROW 9. SECURED, NO FURTHER FAULTS.SDR TAMF20060028SSkin · dentedTEMPORARY REPAIR HAD BEEN PERFORMED ON FUSELAGE SKIN AT STA 172.5 STRINGER 21 RT (REF: SDR TAMF20050007O). PERMANENT REPAIR WAS PERFORMED IAW EWO 767-53-003 PART III, EWO DRAWING 767 53-002 AND SERVICE REQUEST 1-134757238.SDR TAMF20060022SBear Strap · corrodedDURING INSPECTION ACCORDING TASK CARD S53-003-10 WAS FOUND CORROSION AT BEARSTRAP AT THE AFTER CARGO DOOR CONTROL PANEL CUTOUT LOCATION AT STA 1263 STRINGER 26 - RT. CORRODED AREA WAS REPAIRED IAW EWO 767-53-004 R1 PART I AND II AND MSG NR:1-157473174 AND 1-1SDR TAMF20060024SSplice Plate · crackedDURING C-CHECK INSPECTION WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 314.14 LEFT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-011 AND BOEING SERVICE REQUEST: 1-195119496.SDR TAMF20060027SSkin · scratchedDURING INSPECTION CHECK FOUND A SCRATCH ON PRESSURE SKIN AT STA 1582 STRINGER 5-6R. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-013 AND BOEING SERVICE REQUEST 1-195909646.SDR TAMF20060023SSkin · corrodedDURING C-CHECK INSPECTION WAS FOUND A CORROSION ON CENTER WING SKIN STA 955 AND RBL 74.81. CORRODED AREA WAS BLENDED OUT IAW B767 SRM 51-11-00 PAGE 4-5, THICKNESS MEASUREMENT PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS. DAMAGED AREA WAS REPAIRESDR TAMF20060030SSkin Panel · delaminatedDURING C CHECK INSPECTION FOUND A DELAMINATION ON LT VERTICAL STABILIZER SKIN PANEL, STA FSS 170.259 - 195.390. DELAMINATED PANEL PN: 175T2001-3 WAS REMOVED IAW SRM 51-40-02 PAGE 1 AND SENT TO REPAIR. PANEL WAS REPAIRED AND INSTALLED IAW BOEING MESSAGE NUMBESDR TAMF20060029SFloor Skin · corrodedDURING (C) INSPECTION CHECK AFT CARGO COMPARTMENT RT FLOOR STRUCTURE PANEL SKIN HAVE CORROSION AND LOWER ATTACH ANGLE AFT IS CRACKED (UNDER BALL MAT RT). CORROSION ON FLOORBEAM UPPER CHORD ON STA 1285 BETWEEN LBL-RBL WAS FOUND. CRACKED ANGLE AND CORRODED ARSDR TAMF20060026SSkin · crackedDURING (C) CHECK INSPECTION WAS FOUND CRACK AT SKIN ENGINE 1 LT AT FRAME AT NAC STA 274 - CF6-80C2. DAMAGE WAS REPAIRED IAW EWO 767-54-004 AND MFG REFERENCE CV06-1004-01.SDR TAMF20060021SDoubler · corrodedDURING INSPECTION ON C CHECK FOUND CORROSION AT SKIN DOUBLER. CORRODED AREA WAS REPAIRED IAW EWO 767 54-001, BOEING SERVICE REQUEST 1-194658477 AND SRM 54-52-01 FIGURE 201.SDR BB06039Wire · looseEMERGENCY LIGHT ON FLOOR PATH INOPERATIVE BETWEEN SEAT ROWS 7 AND 17 LEFT. MAINTENANCE FOUND LOOSE CONNECTION AT SEAT ROW 7AB. RESECURED WIRE. NO FURTHER FAULTS.SDR TAMF20060025SSkin · crackedDURING C CHECK INSPECTION WAS FOUND CRACK AT SKIN, ENGINE 1 LT AT FRAME AT NAC STA 274. DAMAGE WAS REPAIRED IAW EWO 767 54-003 AND GOODRICH AEROSTRUCTURES REFERENCE CV06-0985-02.SDR TAMF20060019SStiffener · crackedDURING C-CHECK INSPECTION FOUND A CRACK AT VERTICAL CHORD AT STA 287 BL 25 LT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLERS WERE FABRICATED & INSTALLED IAW EWO 767 53-009, SRM 53-10-14 & SRM 51-70-12.SDR TAMF20060020SStiffener · crackedDURING C-CHECK INSPECTION FOUND A CRACK AT VERTICAL CHORD AT STA 287 BL 25 RT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLERS WERE FABRICATED & INSTALLED IAW EWO 767-53-010, SRM 53-10-14 & SRM 51-70-12.SDR BB06038Fuse · blownON DAILY CHECK, MAINTENANCE FOUND THE LEFT AISLE FORWARD FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. REPLACED THE FUSE ON THE BATTERY CHARGER. NO FURTHER FAULTS.SDR BB06037Light · failedDURING OPERATIONAL CHECK OF MED ESCAPE SLIDE, THE SLIDE MOUNTED LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY.SDR BB06036Wire · damagedFLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT RIGHT AFT POSITION. MAINTENANCE REPAIRED WIRING TO LIGHT ASSEMBLY.SDR TAMF20060018OHose · leakingAFTER TAKEOFF, EICAS MSG GEAR DOORS AND GEAR DISAGREE DISPLAYED WITH GEAR HANDLE UP (LEFT GEAR REMAINED EXTENDED). FLT DEVIATED TO AND LANDED WITHOUT PROBLEMS. MAINTENANCE TECHNICIANS INSPECTED LT WHEEL WELL AREA AND DISCOVERED HYDRAULIC LEAK BY LT MLG UP HOSDR BB06030Light · malfunctionedCOCKPIT EMERGENCY LIGHT REMAINS ON WITH LIGHT SWITCH IN OFF POSITION. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.SDR BB06029Wire · damagedEMERGENCY LIGHTS AT MID RIGHT LAV FOUND INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT.SDR BB06027Pin · damagedLEFT SIDE EMERGENCY LIGHTS FROM ROW 20 THROUGH 28 FOUND INOPERATIVE. RECONNECTED PIN AT ROW 28. NO FURTHER DIFFICULTIES.SDR TAMF20060017OFilter · leakingDURING CLIMB, FLIGHT 850 (MDE-VCP), LEFT HYD QTY DECREASED TO ZERO AND SYSTEM PRESS & QTY LIGHTS ILLUM EICAS MSG L HYD SYS PRESS & LEFT HYD QTY DISPLAYED. RETURNED TO MEDELLIN. FOUND HYDRAULIC LEAK BY PCA SPOILER CAP FILTER. RIGHT NOW THE AIRPLANE IS OUT OFSDR TAMF20060006SSkin · crackedDURING INSPECTION, C-CHECK, FOUND CRACK AT FUSELAGE SKIN AT STA 1654 STRINGER 3- 4 -LT. DAMAGE WILL BE REPAIRED IAW EWO 767 53-007, SRM 538001 FIG 201.SDR TAMF20060016SSupport Beam · corrodedDURING C-INSPECTION CHECK WAS FOUND A CORROSION ON RT WING T/E INBOARD SPOILER SUPPORT BEAM, STA 375.8. CHORD WAS FABRICATED IAW BOEING SMAL (SPARE MATERIAL AUTHORIZATION LICENSE) PO BOEING CONTROL 206706 & BOEING DRAWING 113T1407 AND INSTALLED IAW SRM 51-40-SDR TAMF20060015SSupport Beam · corrodedDURING C-INSPECTION CHECK WAS FOUND A CORROSION ON LT WING T/E INBOARD SPOILER SUPPORT BEAM, STA WS 250.0. CHORD WAS FABRICATED IAW BOEING SMAL (SPARE MATERIAL AUTHORIZATION LICENSE) PO BOEING CONTROL 206705 & BOEING DRAWING 113T1407 AND INSTALLED IAW SRM 51-SDR TAMF20060014SSupport Beam · corrodedDURING C-INSPECTION CHECK WAS FOUND A CORROSION ON LT WING T/E OUTBOARD SPOILER SUPPORT BEAM, BETWEEN STA WS 431.97 TO WS 394.92. CHORD WAS BE FABRICATED IAW BOEING SMAL PO 206740 (SPARE MATERIAL AUTHORIZATION LICENSE) & BOEING DRAWING 113T1407 AND INSTALLED SDR TAMF20060013SSkin · erodedDURING C-CHECK INSPECTION WAS FOUND A EROSION ON NOSE SKIN AT HORIZONTAL STABILIZER TIP - RT. DAMAGE WAS REPAIRED IAW EWO 767 55-002 AND BOEING SERVICE REQUEST ID: 1-171213467. ERODED AREA WAS CLEANED UP IAW SRM 55-10-30 PAGE 1 TO 3, THICKNESS MEASUREMENT PE
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