Boeing 767-36N
Service difficulty reports · 1,013
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 = '76736N' 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 = '76736N' 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 UIEA2024052300421Vent · misinstalledRIGHT WING MAIN, TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE MISSING ON BOTH NUT RETAINER(<P>RIGHT WING MAIN TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE WAS INSTALLED CORRECTLY IAW AMM 20-10-23-420-801 REV 142, APR 22,2023; TORQUE ASDR UIEA2024052300422Skin · dentedLH WING, INBOARD FLAP SURFACE LEADING EDGE AREA UPPER OUTSIDE CORNER WITH TWO DENTS.(<P>LH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 5 PAG 2-6 AND SRM 51-70-17-0G-0 PAR 4.A FIG 10 PAG 13,14,34 REV 49 APR 15/-2024. NO FURTHESDR UIEA2024052300423None · noneFAA AGING INSPECTION RH A/A PACK EXHAUST RAM AIR ACTUATOR BONDING LEAD WITH WIRES BROKEN.(<P>RH A/A PACK EXHAUST RAM AIR ACTUATOR BONDING LEAD WAS REPLACED IAW AMM TASK 21-53-03-404-012 REV. 142, APR 22, 2024. BONDING TEST WAS PERFORMED 0.003 MILLIOHMS. BONDINSDR UIEA2024052300424Control Cable · abnormalSECTION 48 INTERNAL AREA, LH ELEVATOR CONTROL CABLE RUBBING WITH PULLEY BRACKET (DUE BAD INSTALLATION) LOCATED AT B. STA 1605.5 LH SIDE.(<P>SECTION 48 INTERNAL AREA, LH ELEVATOR CONTROL CABLE RUBBING WITH PULLEY BRACKET (DUE BAD INSTALLATION) LOCATED AT B. STASDR UIEA2024052400437Skin · delaminatedRH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WITH DELAMINATION(<P>RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WAS REPAIRED IAW SRM 57-60-01-2R-1 REPAIR 1 TABLE II FIG 201 PAG 1-6 AND SRM 51-70-03-0G-0 PAR 5A(2) FIG 12 PAG 10,11, 36 REV 49 APR 15/2024.SDR UIEA2024052800463Skin · delaminatedRH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WITH DELAMINATION(<P>RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WAS REPAIRED IAW SRM 57-60-01-2R-1 REPAIR 1 TABLE II FIG 201 PAG 1-6 AND SRM 51-70-03-0G-0 PAR 5A(2) FIG 12 PAG 10,11, 36 REV 49 APR 15/2024.SDR UIEA2024052400438Skin · corrodedPYLON #1 UPPER SURFACE, CORROSION DAMAGE ON THE BUSHING OF THE INBD LUG OF FWD UPPER SPAR FITTING.(<P>REPAIR FOR CORROSION DAMAGE ON THE BUSHING OF THE INB LUG OF FWD UPPER SPAR FITTING WAS ACCOMPLISHED IAW TRE 6754190 ISSUED DATE MAY 16,2024. FAA FORM 8100-9 SDR UIEA2024052400439Skin · dentedRH WING, INBOARD FLAP, MAIN FLAP, AT 2" FROM TRAILING EDGE AND 6" FROM INBOARD EDGE, DENT ON UPPER SKIN(<P>RH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 TABLE I FIG 201 SHEET 5 PAG.2,3,6 AND SRM 51-70-03-0G-0 PAR 5.A FIG.5 PAG 10,11,25 RESDR UIEA2024052400440Skin · puncturedLH INB ELEVATOR UPPER PANEL, PUNCTURE AT ELEV STA 104.2 APPROX. AND 28" FROM T.EDGE.(<P>LH INBOARD ELEVATOR, UPPER PANEL WAS REPAIRED IAW SRM 55-20-01-2R-1 REPAIR 1 FIG 201 TABLE I PAG 1-3, SRM 51-70-04-0G-0 PAR.5.B PAG.16 AND SRM 51-70-17-0G-0 PAR 4.B FIG.24 SDR UIEA2024052400442Skin · puncturedLH INB ELEVATOR UPPER PANEL, PUNCTURE AT ELEV STA 104.2 APPROX. AND 28" FROM T.EDGE.(<P>LH INBOARD ELEVATOR, UPPER PANEL WAS REPAIRED IAW SRM 55-20-01-2R-1 REPAIR 1 FIG 201 TABLE I PAG 1-3, SRM 51-70-04-0G-0 PAR.5.B PAG.16 AND SRM 51-70-17-0G-0 PAR 4.B FIG.24 SDR UIEA2024052400441Fitting · corrodedLH WING FWD LOAD PITCH FITTING, CORROSION DAMAGE ON INB FITTING.(<P>CORROSION ON INBD FITTING WAS REWORKED IAW TRE6757246, REV 1, MAY 20, 2024. LEVEL CORROSION 2. NO FURTHER DEFECTS NOTED.</P>)SDR CNMA202403130001Hmu · faultedDURING CRUISE FLIGHT AT FL370 LEFT ENGINE N1 ROLLED BACK WITH CORRESPONDING VIBRATIONSSDR CNMA202312210002Cdu · intermittentL CDU FAILURE, L FMC FAILURE: DURING FLIGHT CREW REPORT THE L FMC FAILED. DISCUSSIONS WITH MOC AND DO. ALL PARTIES AGREED TO CONTINUE. CREW CALLED BACK 1 HOUR LATER AND STATED THE L CDU FAILED AND WENT BLANK. FIGHT DIVERTING TO ANC DUE TO ETOPS AND FUEL RESTRISDR IXXA2023090802Skin · crackedRH FWD SERVICE DOOR CUTOUT AFT LWR CORNER CRACKED.SDR UIEA2023082800799Light · unknownEMER LIGHTS "UNARMED" LIGHT BROKEN(<P>R/R UNARMED LIGHT IAW B767 AMM 33-11-00. OPS CKS GOOD</P>)SDR UIEA2023053000529Evas Unit · unknownCAPTAINS EVAS IS INOP(<P><SPAN>REMOVED AND REPLACED CAPTAINS EVAS AS PER 25-60-00 (AMM) OPS CHECKED NORMAL.</SPAN></P>)SDR UIEA2023050700410Unknown · unknownTWO INERTIA DESCENT DEVICE REELS BROKEN #1 AND #7(<P>PLACED ON DEFERRAL 185160 PER MEL 25-61-01-01 CAT C DUE DATE 17MAY23</P>)SDR UIEA2023050800425Smoke Goggles · unknownFIRST OBSERVERS SMOKE GOGGLES INOP(<P>TRANSFERRED TO MDDR 185104 PER MEL 25-11-02-01A CAT A DUE 17MAT23. PLACARDS INSTALLED. LOGPAGE 1773702 M3: REMOVED AND REPLACED FIRST OBSERVERS SMOKE GOGGLES IAW AMM 25-64-00. THIS ACTION CLEARS DMI 185109. MCC NOTIFIED. PSDR UIEA2023042700388Spring · unknownTWO ESCAPE REELS FELL OUT DURING TAKE OFF. R/R HOLDING SPINGS FOR #2 AND #3 INERTIA REEL IAW SRM 51-40-02 AND AMM 25-61-00. OPS CHECK GOOD AT THIS TIME.SDR UIEA2023032300281Unknown · unknownEXIT SIGN BY DOOR HANDLE FELL OFF(<P>RE-INSTALED EXIT SIGN IAW B767 AMM 25-63-00. NO FURTHER DEFECTS NOTED</P>)SDR IXXA2023042001Shroud · crackedSHIELD FOR APU PNEUMATIC DUCK HAS A CRACK AT ATTACH POINTSDR UIEA2023031000236None · noneSUSPECTED HARD LANDING(<P>COMPLETED PHASE 1 INSPECTION IAW B-767 AMM 05-51-01 PER MCC, NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2023022300178None · noneDEBONDED TWO AREAS ON RH PANEL OUTER SKIN LOCATED AT FRONT SPAR AND BETWEEN FSS145.128 TO FSS 270.784 FROM VERTICAL STABILIZER.(<P>IT WAS REPAIRED PER SRM 55-30-01-2R-1 REPAIR 1 FIG. 201 PAGE 2 AND SRM 51-70-10-2R-4 REPAIR 4 FIG. 201 SHEET 1 PAGE 1-3 REV. 121 SDR UIEA2023022300179None · noneDEBONDED TWO AREAS ON LH PANEL OUTER SKIN LOCATED AT FRONT SPAR AND BETWEEN FSS145.128 TO FSS 270.784 FROM VERTICAL STABILIZER.(<P>IT WAS REPAIRED PER SRM 55-30-01-2R-1 REPAIR 1 FIG. 201 PAGE 2 AND SRM 51-70-10-2R-4 REPAIR 4 FIG. 201 SHEET 1 PAGE 1-3 REV. 121 SDR UIEA2023022300180None · noneENGINE #1, INLET COWL LIP SKIN WAS FOUND WITH GOUGE OUT OF LIMITS AT 8 O CLOCK POSITION(<P>IT WAS REPAIRED PER COLLINS REPAIR FORMAT #CV23-01267-REPAIR AND BOEING SR 4-5692112122.</P>)SDR UIEA2023022300182None · noneLH PYLON - UPPER SKIN - WEAR DAMAGE BETWEEN NAC STA 149.43 TO NAC STA 139.73 FOUND OUT OF LIMITS (IT WAS EXCEEDED THE MAXIMUM DEPTH).(<P>IT WAS REPAIRED PER BOEING SR 4-5704143162</P>)SDR UIEA2023022300183None · noneBULK CARGO DOOR SURROUND STRUCTURE - LOWER SILL - EXISTING EDGE REWORK AT LIGHTENING HOLE OF FLOOR PLATE.(<P>IT WAS REPAIRED PER BOEING SR 4-5708956820.</P>)SDR UIEA2023022300184Window · noneFLIGHT COMPARTMENT WINDOW, LH WINDOW (#3) WITH CRACKING(<P>IT WAS REPLACED PER AMM 56-11-10. OPS CHECK GOOD.</P>)SDR UIEA2023022300185None · noneDURING A ZONAL INSPECTION, MISSING RIVETS ON THE ANGLE ON THE FLOOR BEAM LOWER CHORD LOCATED AT STA 654+121, S-20LH AND STA 676, S-20LH.(<P>IN ACCORDANCE WITH IAI CUSTOMER SERVICE - REPAIR INSTRUCTION #CS-30111-001 IS NECESSARY TO REMOVE THE AFFECTED ANGLES FRSDR UIEA2023022300186None · noneLOOSE SHIM LOCATED IN THE HOUSING ASSY (112T1018-1) FROM FWD TRUNNION SUUPORT, LH MAIN LANDING GEAR(<P>REMOVED THE HOUSING ASSY (112T1018-1) TO REPLACE FILLERS / SHIMS PER AMM 32-11-01/401, AIPC 57-53-15 AND DWG 112T1717</P>)SDR UIEA2023022300188None · noneLH WING #6 L/E SLAT (P/N 114T3100-401G, S/N 000010) SKIN BIRD STRIKE DENT DAMAGE - TIME LIMIT REPAIR(<P>IT WAS REPAIRED IN ACCORDANCE WITH ATLAS EO 1957A609 / SRM 57-43-01-2R-2 REPAIR 2</P>)SDR UIEA2023030200197None · noneRH WING, SPOILER #9, TRAILING EDGE LOWER SURFACEÂ (OUTBOARD CORNER), CLOSE TO WSTA 616.2.(<P>IT WAS REPAIRED PER SRM 57-70-01-2R-1 AND SRM 51-70-04-0G-0.</P>)SDR UIEA2023030200198None · noneLH MLG DOOR WITH PUNCTURE DAMAGE ON INNER SKIN AT 30 INCH FROM DOOR LEADING EDGE AND 4 INCH FROM LOWER EDGE.(<P>IT WAS REPAIRED BY SRM 52-80-02-2R-1 / SRM 51-70-03-0G-0 AND BOEING SR 4-5739242265.</P>)SDR IXXA20221111146Roller · out of adjustPRE-DEPARTURE CREW REPORTED COPILOT WINDOW WILL NOT LOCK CLOSED. CRANK ROLLER OF R2 WINDOW ADJUSTED IAW B767 AMM 56-11-02. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS WERE NOTED. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20221101144Display · failedLOWER EICAS DISPLAY WAS BLANK UPON ARRIVAL. AIRCRAFT GROUNDED FOR FAULT ISOLATION. REMOVED EICAS DISPLAY SWITCHING MODULES AND CHECKED WIRES FOR SHORT GROUNDS AND CONTINUITY. CLEANED AND ENSURED SECURITY OF CONNECTORS D5055, D5057, D5009, AND D5227. OPERATIONSDR CNMA202209280371Skin · corrodedCORROSION TOP OF STABILIZER BOX ASSESSMENT FRONT RIGHT SPLICE. LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED DAMAGE ON H-STAB BOX UPPER SKIN FROM FRONT SPAR TO S-11 AT RBL 13.833 IAW STS EA 79-2022-141 REV IR AND OMNI AIR INTERNATIONAL EO B7655-10 INITIAL ISSSDR UIEA2022082600906Sign · detachedDURING COCKPIT OBSERVATION, I FOUND EXIT SIGN ON LIFE RAFT GALLEY COMPUTER NEAR BUTTON BROKEN OFF.(<P>RESECURED EXIT SIGN IN PLACE IAW AMM 25-00-00. OPS CHECK GOOD</P>)SDR UIEA2022070700736None · noneCOCKPIT PORTABLE OXYGEN FULL FACE MASK LENS FRAME DAMAGED P/N 10800C15F(<P><SPAN>REMOVED AND REPLACED PORTABLE OXYGEN FULL FACE MASK AS PER B767-300 AMM 35-31-00.</SPAN></P>)SDR UIEA2022032300220Skin · gougedDURING AIRCRAFT TOUCH UP PAINT MX FOUND GOUGE IN LOWER AFT SECTION OF FUSELAGE AT APPROX FS 1632 IN THE NON PRESSURIZED AREA(<P ><SPAN>REPAIRED FUSELAGE IAW B767 SRM 53-00-01-2R-12 REPAIR 12. EO 6753A992</SPAN></P> / <P> </P>)SDR UIEA2022021400104Mask · inoperativeLH SUPERNUMERARY OXYGEN MASK INOP(<P>TRANSFERRED TO MDDR #161209 PER MEL 35-11-02-03A, CAT C. DUE: 23FEB22. PLACARDS INSTALLED. MCC ADVISED.</P> / <P>DISP: TS@ 1003Z.</P> / <P><SPAN>REMOVED AND REPLACED O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD IAW AMM 35-11-00SDR UIEA2022011100011None · noneUPON DOOR CLOSURE L1 PUSH BUTTON FOR ESCAPE SLIDE WAS NOT CENTERED IN PRECUT PANEL(<P>TRIMMED AND ADJUSTED PRECUT PANEL IAW SRM 51-70-16-06-0 PUSH BUTTON EXTENDS NORMAL .OPS CKS GOOD </P>)SDR UIEA2022010400005None · noneCREW OXYGEN PRESSURE READS 40PSI ON EICAS INDICATION INOP.(<P>TRANSFER TO MDDR 159293 IAW MEL 35-11-02-01, CAT B.</P> / <P>LP 1604090 - REMOVED AND REPLACED VOLTAGE AVERAGING UNIT IAW AMM 35-11-06. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR 159293.</P>)SDR UIEA2021111302412None · noneEMERGENCY LIGHT SWITCH WIRE CLIP IS LOOSE AND DOES NOT FUNCTION PROPERLY(<P>SECURED EMERGENCY LIGHT SWITCH WIRE CLIP IAW AMM 33-51-08. PERFORMED LIGHT TEST IAW AMM 33-51-08. OPS CHECK GOOD.</P>)SDR UIEA2021111002386None · noneFO SIDE OUTLET / NO HEAT.(<P>PERF PACK TEMP CONTROL TEST IAW AMM 21-51-16. OPS CHECK GOOD. AIR TEMP FROM ALL FLIGHT DECK VENTS BLOWS WARM EVENLY. NO DEFECTS AT THIS TIME.</P>)SDR UIEA2021110902380None · noneR2 WINDOW FWD WINDOW HEAT INOP ( FLIGHT DECK WINDOW HEAT SYSTEMS, NO. 2 (SIDE) WINDOWS )(<P><SPAN>DEFFERED IAW MEL 30-40-01-02. DUE 18 NOV 21, MDDR # 156473 CAT C, PERF RT BITE IAW FIM 30-41 FT 804, RT WINDOW #2 FAULTED.</SPAN></P>)SDR UIEA2021110902375None · noneAPU FAILED TO START(<P>T/S PER FIM 49-11 FT 980 TO BLOCK 13 SHEET 2, FOUND GRND ON RELAY K442 PIN 7, BLOCK 34 REPLACE ECU RECOMMENDED, PERF CONT CHECK OF CONNECTOR D40813 PIN H7 TO RELAY K442 PIN 7, CHECK GOOD, MCC UPDATED, ECU ON ORDER.</P>)SDR UIEA2021110902378None · noneAPU FAULT ON START ON GROUND(<P>PERFORMED APU BITE IAW FIM 49-11 FIG 103. NO FAULTS NOTED.</P>)SDR UIEA2021110902379None · noneRIGHT FWD WINDOW EICAS(<P>PERFORMED RH FWD WINDOW BITE TEST IAW FIM 30-41 FAULT TREE 804 FIG 104. NO FAULTS NOTED.</P>)SDR UIEA2021110802360Circuit Breaker · trippedAPU FIRE LP1 AFTER EXT POWER DISC(<P><SPAN>RESET FIRE LOOP BREAKER IAW B767 AMM 20-60-01</SPAN></P>)SDR UIEA2021110802364None · noneAFTER EXT POWER DISC DUCT PSI FALLS TO ABOUT 10PSI W/ PACKS ON(<P><SPAN>PLACED ON MDDR 156389 IAW MEL 49-11-01-01 CAT C DUE 17NOV21 </SPAN></P> / <P><SPAN>EH 1155Z REFENCE LOG 1386918 ITEM M14 CVG 07NOV INSPECTED APU COMPARTMENT DUCTS AND PERFORMED BLEED AIR O
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