Boeing 767-281
Service difficulty reports · 1,831
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 = '767281' 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 = '767281' 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 ABXA20131112620Unknown · odorLAVATORY SMOKE DETECTOR WENT OFF DURING CLIMB THROUGH 360 FT, SHORTLY AFTER SELECTING RT PACK ON. STRONG WIRE BURNING ODOR WAS NOTICED IN COCKPIT. NO OTHER INDICATIONS WITH RT PACK ON. TEMP IN FWD & AFT CABIN WILL NOT GO BELOW APPROXIMATELY 22-24 DEGREES. SDR ABXA20131107652Stiffener · crackedNR 1 PYLON FWD OF PANEL 437DB INSIDE STRUCTURE LOWER CROSS BRACE HILOCK LOOSE. R & R NEW FABRICATED PADS ON ALL AREAS DAMAGED. PN 313T3380-303 WEB & FRAME 1INCH CRACK, PN 313T1355-169 SPLICE 2 1/2 INCHES CRACK, PN 313T1355-181 1 INCH CRACK 313T3380-244 & 31SDR ABXA20131107651Skin Panel · corrodedUPPER TRAILING PANELS FWD OF OTBD AILERON RAISED IN TWO SPOTS ON PANEL LE. R & R UPPER TE PANELS IAW B767 SRM 51-40-02 PARA 4 & PARA 7. REPAIRED CORRODED SKIN IAW ABX REA B657-60785-MR REV IR DATED 11-14- 13. PN 112T3101, PN SKIN PANEL, SN NSN, CORRODED, A/SDR ABXA20131107650Channel · corrodedREAR SPAR TO TE PANEL ATTACH CHANNEL AT WING STATION 1046 SPLIT ON EDGE. FABRICATED NEW CHORD ON RFA B657-60757 REMOVED OLD CHORD & INSTALLED NEW CHORD IAW B767-200 SRM 51-40-02. CORRODED PN 113T1683-14 PN CHORD RIGHT WING LOWER TE EXACT STRINGER & WS LOCATISDR ABXA20131011649Bulkhead · crackedDURING A HFEC INSPECTION OF THE Y RING ATTACHMENT OF THE AFT PRESSURE BULKHEAD A CRACK WAS INDICATED AT A FASTENER HOLE LOCATED AT STRINGER 10R B STATION 1582 INTERIOR OF THE FUSELAGE. TIMED OUT VERIFIED CRACK & REPAIRED IAW REA B653-60742-MR, TRIM OUT MEASURSDR ABXA20131011646Strut · corrodedNUMBER 5 SLAT INBD AUX TRACK OTBD LOWER STRUT HAS CORROSION UNDER NUTPLATES. R & R NR 5 SLAT INBD AUX TRACK OTBD LOWER RIB STRUT PN 114T2201-23 IAW REA NR B657-60734-MR AND B767 SRN 51-40-02. PN 114T2201-23, NSN, STRUT RIB CORRODED AT 433.1 TO 434.1. AIRCRSDR ABXA20131010648Stringer · crackedFORWARD LOWER CARGO STRINGER 23L AFT OF STATION 767 FRAME HAS A 1.1 INCH CRACK AT STRINGER END FITTING LOC. REPAIRED STRINGER 23L AT STATION 676 TO 700 IAW B767-SRM 53-00-03 FIG 201 REPAIR 2. PN143T3001, NSN, STRINGER CRACKED 1.3 INCHES AT 676, 23L. AIRCRASDR ABXA20131008576Gpu · malfunctionedLEFT ENGINE VERY SLOW TO RESPOND WITH THROTTLE ADVANCEMENT. ON BLOCK IN, LT ENGINE ADVANCED UNCOMMANDED, THROTTLE IN IDLE POSITION, TO APPROXIMATELY 80 PERCENT, N2. PERFORMED ENGINE RUN IAW 74-00-00-2, NO DEFECTS NOTED. AS FAR AS ENGINE GOING TO FLIGHT IDLESDR ABXA20131006645Bracket · crackedBRACKET ON FLAP ANGLE GEARBOX 18 INCHES FROM FUSELAGE ON WING TE CRACKED. R & R ANGLE GEARBOX BRACKET IAW B767-SRM 51-40-02 P. 10 PN 256T3022+-7, NSN, BRACKET CRACKED 1/2 INCH AT WBL 121 TO WBL 124. AIRCRAFT WAS GROUNDED.SDR ABXA20131005577Skin · damagedFUSELAGE SKIN DAMAGED BS 434, STRINGERS 31-32R. SKIN REPAIRED IAW COI59981-001 AND REA B653-607-24-MR ACFT WAS GROUNDED.SDR ABXA20131003647Strut · corrodedNUMBER 2 SLAT INBD AUX TRACK OTBD LOWER STRUT SPLIT AT FWD EDGE. NES STRUT RIB WAS FABRICATED ON REA B657-60736-MR. INSTALLED NEW STRUT RIB PN 114T2221-17 & A NEW TRACK FTG SHIM PACK IAW B767 SRM 51-40-02 PARA 4 & 7. PN 114T2221-17, NSN, STRUT CORRODED AT OSDR IXXA20130921034OAileron Sys · malfunctionedAFTER THREE HOURS IN CRUISE FLIGHT AND DISENGAGING AUTOPILOT, AILERONS VERY STIFF. AFTER ACTUATING ON GROUND SEVERAL CYCLES, RETURNED TO NORMAL OPERATION. ACCOMPLISHED FIM PROCEDURE 27-11, FAULT TREE 808, PAGE 119, BLOCKS 1, 21 AND 41. LUBED LEFT LATERAL CESDR ABXA20130820507Structure · corrodedUPPER PANEL ATTACH CAP ON RIB FROM REAR SPAR TO T/E AT WS 433 HAS CORROSION UNDER NUTPLATE. FABRICATED NEW CAP IAW DWG 113T1510, HEAT TREATED TO T6 IAW BAC 5602, TABLE 1, PAGE 12 AND 17 NOTE C, INSTALLED NEW CAP IAW SRM 51-40-02 AND AMM 20-11-00D.SDR ABXA20130819510Frame · crackedNR 1 PYLON INBD FRAME BELOW HYD BAY ACCESS DOOR CRACKED AT FWD LATCH FITTING. R & R DEFECTIVE FRAME IAW SRM 51-40-2. ACFT WAS GROUNDED.SDR ABXA20130819509Angle · crackedSTRUCTURE INSIDE OF VERTICAL STAB PANEL 324CLX, ON TOP OF FUSELAGE HAS CRACKS IN FWD ANGLE. REMOVED WEB TO FORM IAW SRM 51-40-02, DRILLED AND INSTALLED NEW STIFFENER IAW SRM 51-40-05 AND 51-40-02,SDR ABXA201308185012Spar · corrodedLEFT WING REAR SPAR APPROX. W.S. 250 AT APU FUEL SHUTOFF VALVE MOUNTING BASE CORRODED. MARKED. REPAIRED REAR SPAR IAW REA B657-60671-MR. REAR WING SPAR, PN: 112T1007-7, SN: NSN, LOC: RSS-250.00, CORRODED; ACFT WAS GROUNDED.SDR ABXA20130818508Channel · splitT/E PANEL, 661NB LOWER AFT ATTACH CHANNEL AND BRACKET FROM REAR SPAR TO T/E AT WS 1055 SPLIT. R & R AFT LOWER ATTACH BRACKET AND CHANNEL IAW SRM 51-40-02.SDR ABXA20130810503Failsafe · crackedFRAME FAILSAFE CRACKED AND CORRODED. CRACK VERIFIED WITH HFEC IAW NDTM, PART 6 51-00-19 AND VISUALLY VERIFIED. FAILSAFE REPAIRED ON JC EA53500013-003. ACFT WAS GROUNDED.SDR ABXA20130806502Battery Pack · inoperativeSUPER NUMERARY EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT IAW AMM 33-50-00-00, AND FOUND M736 POWER SUPPLY INOPERATIVE. R & R BATTERY ASSY. ALL EMERGENCY LIGHTS OK, ACFT WAS GROUNDED.SDR ABXA20130805504Failsafe · crackedFAILSAFE CRACKED 1.7", LEFT FS 955, LBL 85.9. AIRCRAFT WAS GROUNDED. REPAIRED IAW REA B653-60654-MR.SDR ABXA20130730505Pressure Panel · crackedOTBD FWD CORNER OF PRESSURE WEB CRACKED JUST AFT OF SIDE FRAME ATTACH FLANGE. FABRICATED NEW WEB IAW DWG 145T8752 INSTALLED IAW EA 53500013-003, PG. 10, STEP 25.SDR ABXA20130727500Bracket · crackedRT WING BRACKET ATTACHING INBD L/E STRUCTURE TO FWD UPPER SPAR AT WING STA 155 IS CRACKED. R & R BRACKET IAW SRM 51-40-02. LEAK CHECK GOOD IAW AMM 28-11-00. WS LOC; ACFT WAS GROUNDED.SDR ABXA20130724484Warning Message · false activationPASSING FL 260, LT FWD ENTRANCE DOOR MESSAGE ILLUMINATED. CHECKED IAW MM 52-11-00-6, OPS CHECKED NORMAL AND DOOR WARNING SYS OPS IAW 52-71-00-5. OPS CHECKED GOOD, ACFT WAS GROUNDED.SDR ABXA20130723501Strut · corrodedNR 5 SLAT OTBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R STRUT AT OTBD SIDE OF OTBD AUX. TRACK IAW SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20130723499Angle · crackedL/E VERTICAL STABILIZER FWD ANGLE HAS CRACKED INSIDE LT SIDE OF VERTICAL STABILIZER AT VERTICAL FUSE BOXED STRUCTURE INSIDE OF LOWEST PANEL OPENING. R & R FWD ANGLE INSIDE LEFT VERTICAL STABILIZER AT VERTICAL FUSE BOX IAW DWG 173T1215 AND SRM 51-40-02. ACFT SDR ABXA20130723498Frame · corrodedFRAME CORRODED AT APU EXHAUST DUCT SUPPORT FUSELAGE, BS 1943.5. CLEANED UP CORROSION, SPLICED IN NEW SECTION OF FRAME AT STA 1943.5 IAW REA B653-60618, ACFT GROUNDED.SDR ABXA20130722496Strut · corrodedNR 2 SLAT ON LT WING OTBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R NR 2 SLAT OTBD AUX TRACK AND OTBD LOWER STRUT IAW SRM 51-40-02, PARA 7B AND REA B657-60610, ACFT GROUNDED.SDR ABXA20130722493Rib · corrodedNR 5 SLAT ANTI-ICE TELESCOPING DUCT INBD STRUT CORRODED AROUND NUTPLATES. REMOVED CORRODED AIR LOAD RIB, INSTALLED NEW AIR LOAD RIB IAW REA 657-60614 AND SRM 51-40-02. INSTALLED NR 5 SLAT & TELESCOPING DUCT IAW AMM 20-11-00-2, FIG 209 & SRM 51-40-02 AMM 30-1SDR ABXA20130722492Strut · corrodedNR 5 SLAT INBD AUX TRACK OTBD LOWER STRUT HAS CORROSION AROUND NUTPLATES. R & R NR 5 SLAT INBD AWS TRACK OTBD LOWER STRUT IAW SRM 51-40-02, AND EA B657-60615.SDR ABXA20130721491Rib · corrodedCORROSION ON RIB AND FRONT SPAR LOWER TEE FRAME AT NR 9 SLAT INBD AUX TRACK OTBD RIB. R & R AIRLOAD RIB AT NR 9 SLAT INBD AUX TRACK IAW SRM 51-40-02 AND REA B657-60613, ACFT WAS GROUNDED.SDR ABXA20130722490Support · crackedINBD VERTICAL STRUCTURE FOR PNEUMATIC DUCT UPPER FWD ADJUSTABLE ROD FITTING HAS A CRACK COMING OUT OF TOP FASTENER, UNDER PANEL 441AT. R & R INBD VERTICAL STRUCTURE FOR ANTI ICE DUCT UPPER FWD ADJUSTABLE ROD IAW SRM 51-40-02 AND DWG 311T151510, ACFT WAS GROUNSDR ABXA20130721487Strut · corrodedCORROSION AROUND NUTPLATES ON LOWER STRUT OF NR 8 SLAT OTBD AUX TRACK OTBD STRUT. R & R LOWER STRUT OF NR 8 SLAT OTBD AUX TRACK OTBD STRUT IAW SRM 51-40-02 AND REA B657-60609, ACFT WAS GROUNDED.SDR ABXA20130718489Beam · chafedCHAFE ON BACKSIDE OF FWD ATTACHING FLANGE FOR ACCESS PANEL 447BR AT BS 298-RT NACELLE STA 410, RT PYLON OTBD SIDE. R & R NR 2 OTBD PYLON BEAM IAW SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20130717494Strut · corrodedNR 3 SLAT OTBD AUX TRACK INBD LOWER STRUT CORRODED AT FORWARD END. R & R STRUT IAW SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20130717488Structure · corrodedCORROSION UNDER NUTPLATE ON WING L/E AFT OF NR 8 SLAT LES 466. R & R OUT OF LIMIT DAMAGE. IAW SRM 51-70-11, DETAIL II. ACFT WAS GROUNDED.SDR ABXA20130716495Strut · corrodedNR 2 SLAT INBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R INBD AUX TRACK OTBD STRUT ON NR 2 SLAT IAW DWG 114T2222, REV D, ACFT GROUNDED.SDR ABXA20130715497Web · crackedNR 1 SLAT WEB ON L/E OF WING AT OTBD AUX TRACK INBD STRUT ATTACH POINT SPLIT FROM CORROSION. REPAIRED NOSE BEAM WEB IAW SRM 57-41-13, FIG 201, REPAIR 1, ACFT WAS GROUNDED.SDR ABXA20130715486Beam · corrodedCORROSION AROUND NUTPLATE ON WING L/E AT L/E S682 AFT OF INBD END OF NR 10 SLAT. REPAIRED AREA IAW SRM 51-70-11, REPAIRED AREA IAW SRM 51-70-11, ACFT WAS GROUNDED.SDR ABXA20130711485Beam · corrodedCORROSION ON WING L/E WEB AT LES 695 AFT OF NR 10 SLAT. REPLACED NOSE BEAM IAW SRM 51-40-02, ACFT WAS GROUNDED.SDR IXXA20130709025J-Box · failedLEFT ENGINE EGT FLUXUATES FROM NORMAL TO 70C ON EICAS AND ALTERNATE SYS. ACFT RETURNED TO STATION. ACCOMPLISHED FIM PROCEDURE 77-21 FAULT TREE 103, BLK 1,2,21. R & R LT ENGINE EGT JUNCTION BOX IAW AMM 77-21-02. OPS CHECKS NORMAL ON ENGINE RUN UP IAW ERH B7SDR ABXA20130621459Seal · brokenDURING SERVICE CHECK FOUND 2 EMERGENCY DESCENT DEVICE SEAL BROKEN AND ACTIVATED. R & R TWO EMERGENCY DEVICE IAW AMM 25-61-02-2, ACFT WAS GROUNDED.SDR ABXA20130619457Lamp · unsecureENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND LAMP NOT SECURED IN SOCKET. SECURED LAMP IAW AMM 33-51-06-2. LIGHT OPERATES NORMAL, ACFT WAS GROUNDED.SDR ABXA20130516434Angle · damagedFUSELAGE SKIN AT LT HORIZONTAL ANGLE, BS 1809, S12L HAS DEFECT INDICATION IN LOWER FWD FASTENER OF INSPECTED AREA 1 IAW NDTM PART 6, FIG 1. FASTENER OBLONG, REAMED TO .341" ON EXTERIOR RUB STRIP CUT OUT LOCATION. FASTENER DOUBLER REPAIRED IAW ENGINEERING REASDR ABXA20130514436Skin · corrodedRIGHT SIDE EMERGENCY EXIT DOOR CUTOUT FOUND WITH CORROSION IN THE FORWARD LOWER CORNER AREA APPROX. 2" LONG. REMOVED CORROSION IN RT SIDE EMERENCY EXIT CUTOUT FORWARD LOWER CORNER AREA. IAW REAB653-60542, ACFT WAS GROUNDED.SDR IXXA20130514019Proximity Switch · malfunctionedEICAS FLAP MESSAGE ON TAKEOFF ROLL. TAKEOFF REJECTED AT 70 KTS. ACCOMPLISHED TAKEOFF WARNING ALERT TEST IAW MM 31-51-00, PARA 2 AND TESTED THE FLAP SLAT ELECTRONICS UNIT IAW MM 27-51-00, PARA 3E AND 3F. TESTED THE PROXIMITY SWITCH ELECTRONICS UNIT OF L/E ISDR ABXA20130506432Mount · corrodedNR 2 ENGINE AFT MOUNT HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED ENGINE MOUNT IAW B767 MM CH 71-21-02-4, ACFT WAS GROUNDED.SDR ABXA20130506430Pbe · unserviceablePBE (PERSONAL BREATHING EQUIPMENT) HOOD CONTAINER LOST VACUUM SEAL. REMOVED AND REPLACED IAW AMM 25-64-00-0, ACFT WAS GROUNDED.SDR ABXA20130503435Stiffener · corrodedSTIFFENER BETWEEN KEELBEAM PANELS CORRODED ON BOTH ENDS, STIFFENER CORRODED BEYOND LIMITS, R & R IAW SRM 51-40-02, PARA 4B AND 51-40-0, ACFT WAS GROUNDED.SDR IXXA20130503014ODoor · unsecureON DEPARTURE, ACFT WOULD NOT PRESSURIZE. EICAS MESSAGE CARGO DOORS INDICATED AND CARGO DOORS LIGHT ILLUMINATED. ACFT RETURNED TO STATION. DURING INSPECTION FOUND AFT CARGO DOOR NOT CLOSED AND LOCKED. MANUALLY CLOSED AND LOCKED DOOR. OPERATED THE DOOR ELECTSDR ABXA20130501433Mount · corrodedNR 1 ENGINE AFT ENGINE MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED AFT ENGINE MOUNT IAW B767 AMM 71-21-02-4, ACFT WAS GROUNDED.
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