Boeing 757-23A
Service difficulty reports · 1,397
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 = '75723A' 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 = '75723A' 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 FDEA201605201690Frame · corrodedRIGHT ELEVATOR TE 2ND STATIC WICK FROM OTBD END, HAS SIGNS OF CORROSION AROUND BASE. REMOVED 2ND STATIC WICK FROM O/B END, EVAL AREA FOUND CONDUCTIVE FRAME OUT OF LIMITS. REMOVED CONDUCTIVE FRAME , FABRICATED, LOCATED AND INSTALLED CONDUCTIVE FRAME ON RT ELESDR FDEA201605201681Skate Angle · corrodedMAIN CABIN STATION 1018 LT SIDE, SKATE ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A. CUT OUT DAMAGED SECTION FROM STA 990 TO 1040 LT SKATE ANGLE. FABRCATED AND INSTALLED CREASE BEAM INBRD SPLICE REPAIR STA 990-1040 IAW B757 SRM 53-00-13-2R SDR FDEA201605191670Cusp Web · corrodedMAIN CABIN, BETWEEN STATION 1420 - 1440 RT SIDE CUSP WEB CORRODED. R & R CUSP WEB MAIN CABIN IAW SRM 51-40-02 & DWG 1465590 REV E.SDR FDEA201605191669Skate Angle · corrodedMAIN CABIN STATION 939 RT SKATE ANGLE CORRODED. REMOVED CORROSION IAW 51-10-02, MATERIAL LOSS OF .011, ORIGINAL THICKNESS.071, REMAINING MATERIAL .060, OUT OF LIMITS IAW SRM 53-60-13-1A. CUT OUT DAMAGED SECTION OF MAIN CABIN SKATE ANGLE, STATION 900 - 957. SDR FDEA201605191668Skate Angle · corrodedMAIN CABIN, BETWEEN STATION 1180 - 1020, LT SIDE SKATE ANGLE CORRODED. REMOVED CORROSION FROM MAIN CABIN SKATE ANGLE IAW SRM 51-10-02. MATERIAL LOSS .035, ORIGINAL THICKNESS .071, REMAINING MATERIAL .036, OUT OF LIMITS IAW SRM 53-40-13-1A. CUT OUT DAMAGED SSDR FDEA201605181661Fitting · corrodedNUMBER 2 ENG STRUT TO DIAGONAL BRACE FITTING, HORIZONTAL OTBD AFT, INBD MOST FASTENER HOLE HAS CORROSION. WORK PERFORMED ON EA F-5450-T0325148 AT NR 2 ENG STRUT TO DIAGONAL BRACE FITTING, HORIZONTAL FLANGE OTBD AFT FASTENER HOLE. NACELLE & PYLON- PYLON STRUCSDR FDEA201605111535Skin · gougedLEFT HORIZONTAL STAB LOWER SKIN HAS A DENT WITH GOUGE AT STAB STATION 104. EVALUATED GOUGED DENT ON LT HORIZONTAL STAB LOWER SKIN & FOUND TO BE OUT OF LIMITS DUE TO GOUGE IAW SRM 55-10-01-1A FIG 101 TABLE I DETAIL IV. BLENDED GOUGE & APPLIED PERMANENT REPAIRSDR FDEA201605031447Skin · crackedL1 DOOR OUTER SKIN, UPPER FWD CORNER BENT WITH POSSIBLE CRACK. COMPLIED WITH REPAIR ON L1 DOOR OUTER SKIN UPPER FWD CORNER IAW SRM 52-10-01-2R REPAIR 7.SDR FDEA201605021443Panel · corrodedLEFT WING TE INBD MAIN FLAP, UPPER SURFACE TE WEDGE PANEL HAS SPOTS OF CORROSION AT MID OTBD SECTION. REPAIRED LT WING INBD MAIN FLAP UPPER SURFACE BY HOT BONDING FILLER & DOUBLER IAW SRM 57-53-01-2R FIG 201 & SRM 51-70-10-2R PARA 20.SDR FDEA201605021441Skin · dentedDENT & GOUGED IN FUSELAGE SKIN, STATION 1580 - 1600, STRINGER 15R - 16R. CUT OUT DAMAGED AREA OF SKIN , DIM 2.3" X 1.8" & INSTALLED REPAIR IAW SRM 53-00-01-2R REPAIR 16.SDR FDEA201604201284Static Line · out of positionLEFT ENTRY DOOR WAS DIFFICULT TO ARM. SLIDE REQUIRED SEVERAL ATTEMPTS OF OPENING & CLOSING DOOR TO ARM. FOUND STATIC LINE INTERFERING GIRT BAR. RE-STOWED STATIC LINE CYCLED DOOR ARMING MECHANISM SEVERAL TIMES. GIRT BAR OPERATIONS CHECKED NORMAL IAW AMM 52SDR FDEA201604111185Seat Track · damagedSEAT TRACK STATION 580, LBL 45.5, INBD SIDE FLANGE HAS A BROKEN AREA. R & R SEAT TRACK FROM STATION 440 - 680, LBL 45.50 IAW SRM 51-40-02, STA MOBLE 757-200SF & SRM 53-00-00.SDR FDEA201604011136Attach Angle · corrodedAFT CARGO COMPARTMENT, BS 1440 UNDER TRANSITION PANEL, INTERCOSTAL ATTACH ANGLE HAS CORROSION. R & R INTERCOSTAL ATTACH ANGLE AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 & DWG 146N8522 REV E.SDR FDEA201604011135Shear Tie · corrodedAFT CARGO COMPARTMENT, BS 1440, RBL 22 UNDER TRANSITION PANEL, BRACKET ATTACHED TO INTERCOSTAL & TIE DOWN HAS CORROSION. R & R SHEAR TIE ATTACH BRACKET ON INTERCOSTAL IN AFT CARGO COMPARTMENT IAW SRM 51-40-02 & DWG 146N5421 REV A & B.SDR FDEA201603291114Hinge · brokenON ARRIVAL FOUND DOOR 1L SLIDE COVER LT HINGE BROKEN. SLIDE COVER REPAIRED IAW CMM 25-00-66. COVER REINSTALLED IAW MM TASK 25-66-01 401. ACFT OK FOR SERVICE.SDR FDEA201603291099Fseu · inoperativeAT LEVEL OFF FLIGHT 360, EICAS MSG LE SLAT ASYM MSG CAME ON. COMPLIED WITH QRH. ACFT ARRIVED WITH NO LOWER EICAS MSG OR MX MSG. LE LIGHT WAS ON ABOVE POSITION GAUGE. CREW HAD LE SLAT ASYM ORANGE ON UPPER EICAS. RESETTING FSCUE 1 BREAKER CLEARED LIGHT. BISDR FDEA201603291098Computer · inoperativeAT LEVEL OFF FLIGHT 360, EICAS MSG LE SLAT ASYM MSG CAME ON. COMPLIED WITH QRH. ACFT ARRIVED WITH NO LOWER EICAS MSG OR MX MSG. LE LIGHT WAS ON ABOVE POSITION GAUGE. CREW HAD, LE SLAT ASYM, IN ORANGE ON UPPER EICAS. RESETTING FSCUE 1 BREAKER CLEARED LIGHTSDR FDEA201603281085Girt Bar · out of positionON BLOCK IN, WHEN ATTEMPTING TO DISARM & OPEN L1 DOOR, GIRT BAR DID NOT ATTACHING FITTING CAME OFF, SLIDE DID NOT ACTIVATE. FOUND GIRT BAR OUT OF PLACE, GIRT BAR REINSTALLED IAW AMM 25-66-01 401 & 25-66-10-2. ACFT OK FOR SERVICE.SDR FDEA201603090877Adc · failedFIRST OFFICER ADC RT SIDE ON DESCENT 320 KTS IAS, SPEED BRAKE LEVER OUT, HOOK ON FIRST OFFICERS SIDE APPROVAL COMMAND SPEED, ALTN ADC SELECTED RT SIDE, CONTINUED TO LANDING. CHECKED RT ADC A FEW TIMES, NO CHANGE. BSL U AIR DATA COMPUTER RT SIDE HAS BEEN RESDR FDEA201603060855Access Panel · looseL1 DOOR WILL NOT OPEN COMPLETELY, APPEARS TO BIND & ONLY OPENS TO ABOUT 2/3 FULLY. FOUND UPPER EXTERNAL ACCESS PANEL FOR DOOR HINGE LOOSE. TORQUED CTR PANEL SCREW, DOOR WAS HITTING PANEL. OPERATIONS CHECKED DOOR IAW MM 52-11-00-6, SUB TASK 52-11-00-216-025SDR FDEA201603020800Autothrottle Sys · malfunctionedAT 40 KTS, MASTER CAUTION, AUTOTHROTTLE DISC, ALERT APPEARED ON EICAS. REJECTED TAKEOFF. CLEARED MESSAGE WITH AUTOTHROTTLE DISCONNECTS ON THROTTLE QUADRANT. PERFORMED TROUBLESHOOTING & TEST ITEM 02, 05, 10 IAW FIM 22-03 FAULT TREE 828 FIM 22-03 FAULT TREE SDR FDEA201603020798Warning Light · false activationAT 40 KTS, MASTER CAUTION, AUTO THROTTLE DISC, ALERT APPEARED ON EICAS. REJECTED TAKEOFF. CLEARED MSG WITH AUTOTHROTTLE DISCONNECTS ON THROTTLE QUADRANT. THRUST MANAGEMENT SYS & AUTO THROTTLE SYS INOPERATIVE. THRUST MANAGEMENT SYS & THROTTLE SYS INOPERATIVSDR FDEA201602030422Light · inoperativeSLIDE BULB BURNED ON RT DOOR. RE-BULB IAW SMP. OPERATIONS CHECKED OK.SDR FDEA201602020421Switch · dirtyON TAKEOFF, AT APPROX 40 KTS, MASTER CAUTION ILLUMINATED WITH CHIMES, AUTO THROTTLE DISC, DISPLAYED ON EICAS. TAKEOFF WAS REJECTED. FOLLOWED QRH PROCEDURES, ALERT CLEARED. NORMAL TAKEOFF WAS COMPLETED. INSPECTED & CLEANED LT & RT AUTO THROTTLE DISCONNECT SSDR FDEA201601240309Actuator · faultyDURING ENG START, LT ENG, AFTER POWER TRANSFER, LT ENG SPAR VLV ILLUMINATED WITH ENG SHUTDOWN. PERFORMED ADJUSTMENT TEST IAW MM 28-22-11-5. EXERCISED VLV MANUALLY, EXERCISED VLV ELECTRICALLY, SHOOK DOWN WIRING TO ATTEMPT TO INDUCE MALFUNCTION, ALL OK. PERFOSDR FDEA201512164015Skin · dentedUPON INSPECTION OF NR 4 SLAT, DENT DAMAGE TO LE SKIN & NOSE RIB FOUND AT OSS 333.35, SLAT REPAIRED AS DETAILED IN EA F-5750-T0321726.SDR FDEA201512144001Panel · crackedLEFT WING NR 2 SLAT COVE PANEL CRACKED. LT WING NR 2 SLAT COVE PANEL REPLACED IAW DWG 114N4076 AS INSTRUCTED BY EA F-5750-T0321712.SDR FDEA201512144000Skin · dentedSMALL DENT EVIDENT ON LT WING INBD MAIN FLAP UPPER SURFACE ALUMINUM HONEYCOMB PANEL, APPROX 8 INCHES FROM INBD END. REPAIR CARRIED OUT IAW SRM 57-53-01 & SRM 51-70-10-2R REV 116 DATED 20 SEPT 2011.SDR FDEA201512143999Access Panel · damagedRIGHT WING ACCESS PANEL 611KT PAINT SURFACES IN POOR CONDITION & COUNTERSINKS PULLED THROUGH. REPAIR CARRIED OUT TO RT WING ACCESS PANEL 611KT IAW EA F-5750-T0321912.SDR FDEA201512143997Panel · crackedRIGHT WING NR 10 SLAT COVE PANEL HAS EVIDENCE OF A CRACK. RT WING NR 10 SLAT COVE PANEL REPLACED IAW DWG 114N 4076 AS INSTRUCTED BY EA F-5750-T0321711.SDR FDEA201512143992Skin · gougedRIGHT WING OTBD MAIN FLAP HAS TWO GOUGES ON ALUMINUM NOSE SKIN AT WBL 561.0. GOUGES ON RT WING MAIN FLAP REMOVED & FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01. REPAIR CARRIED OUT IAW EA INSTRUCTION DETAILED IN EA F-5750-T0321786. BONDED PATCH REPAIR, MAJOR RSDR FDEA201512143987Shim · damagedDURING ACCOMPLISHMENT OF EA F-5310-TO321633A DAMAGE TO ONE HOLE WAS FOUND AT BS 395 LT, STRINGER -17L TO -18L. CORRECTION ACTION CARRIED OUT IAW EA F-5310-T-321940. FURTHER DETAILED INSPECTION FOUND MECHANICAL DAMAGE OF HOLE AT 6 O'CLOCK POSITION TO SHIM, BSDR FDEA201512073940Floor Support · corrodedFLOOR SUPPORT BOX SECTION STATION 1660 & 1680 AT BL 0.0 CORRODED AT FLOORBOARD FASTENER HOLES. FLOOR SUPPORT BOX SECTION STATION 1660 & 1680 AT BL 0.0 REPLACED IAW SRM 51-40-02 & DWG 146N5230. REPAIR CLASSIFIED AS MAJOR CAT A.SDR FDEA201512073933Stringer · corrodedREMOVAL OF DAMAGED CAPTIVE NUT FROM BS 750, STRINGER 21 LT, HAS REVEALED CORROSION DAMAGE TO STRINGER 21L IN THAT AREA CARRY OUT STRINGER REPAIR TO STRINGER 21L H, BS 750 IAW SRM 53-00-03-2R.SDR FDEA201512033880Scuff Plate · crackedSCUFF PLATE CRACKED L2 DOORWAY SCUFF PLATE FWD CORNER PLATE CRACKED. REPAIRED IAW PRODUCT STANDARDS BAC 5975 REVISION M DATED 01 JUNE 2005.SDR FDEA201512033879Scuff Plate · crackedSCUFF PLATE CRACKED, R2 DOORWAY SCUFF PLATE FWD CORNER PLATE CRACKED. REPAIRED IAW PRODUCT STANDARDS BAC 5975 REVISION M DATED 01 JUNE 2005.SDR FDEA201512013832Proximity Switch · out of adjustDURING PRE-FLIGHT CHECK, FOUND ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT R1 DOOR WORKING INTERMITTENTLY. PROXIMITY SWITCH ADJUSTED IAW AMM 25-66-11-2.SDR FDEA201511293815Slide · unsecureAFTER LANDING, FIRST OFFICER FAILED TO DISARM RT ENTRY DOOR. SLIDE & RAFT CAME OUT OF CONTAINER BUT DID NOT INFLATE, WHEN MX OPENED DOOR. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE. REF AMM 25-66-01-4. ITEM REMOVED FROM MEL, A/C OK FOR SERVICE.SDR FDEA201511283813Slide · partial deployDURING WALK AROUND FOUND RT FWD ESCAPE SLIDE PARTIALLY DEPLOY.SDR FDEA201511263792Paint · deterioratedEVIDENCE OF PAINT DETERIORATION ON SEAT TRACK NR 5 AT STATION 1180 - 1200.SDR FDEA201511253790Window · crackedDURING CRUISE, LT FWD WINDOW ARCING & THEN OUTER PANE CRACKED. R & R NR 1 FLIGHT DECK WINDSHIELD IAW AMM 56-11-01-4. PERFORMED WINDOW HEATING SYS TEST, TEST PASSED. PERFORMED FIRST & SECOND TORQUE OF NR 2 BOLTS. THIRD TORQUE SEQUENCE WILL BE TRANSFERRED TSDR FDEA201511233762Paint · deterioratedEVIDENCE OF PAINT DETERIORATION ON STRUCTURE BELOW FLOOR PANEL 242MQF, AT STATION 1180 - 1200.SDR FDEA201511233761Seat Track · unknownEVIDENCE OF BARE METAL ON SEAT TRACK NR 2 AT BS 1140 - 1180. FABRICATED & REPLACED IAW SRM 51-40-02 & DWG 146N5130.SDR FDEA201511233760Seat Track · unknownEVIDENCE OF BARE METAL ON SEAT TRACK NR 3 AT BS 1140 - 1180. FABRICATED & REPLACED IAW SRM 51-40-02 & DWG 146N5130.SDR FDEA201511233759Floor Support · corrodedFLOOR SUPPORT BOX SECTION, AT STATION 1660 - 1680, BL0, CORRODED AT FLOORBOARD FASTENER HOLES.SDR FDEA201511233758Floorbeam · damagedFLOORBEAM AT BS 1200, BETWEEN SEAT TRACK 5 & 6, RBL 24.75 - 45.50, TOP FLANGE IN POOR CONDITION. REPAIRED IAW SRM 53-00-51-2R REPAIR 1 & SRM 51-40-02. MAJOR REPAIR.SDR FDEA201511053488Skin Panel · corrodedRIGHT WING UPPER SURFACE FIXED PANEL HAS SEVERAL PULLED RIVETS & PANEL IS BULGING AT ATTACHMENT TO TOP WING SKIN AT AFT REAR SPAR WS 231. ON REMOVAL OF RT WING FIXED UPPER PANEL, CORROSION FOUND ON SKIN & FALSE SPAR. AREAS OF CORROSION REWORKED IAW EA F-5700SDR FDEA201511053485Door · crackedSUSPECT CRACK AT NR 2L DOOR UPPER HINGE CUT OUT. CRACK BLENDED IAW SRM 52-10-01-1A & NDT CARRIED OUT TO ENSURE CRACK REMOVED IAW NTM 51-00-19 P16. REPAIR CARRIED OUT TO UPPER HINGE CUT OUT ON L2 IAW SRM 52-10-02-2R-1 REPAIR 1. OPEN HOLE HFEC INSPECTION CARRSDR FDEA201511043475Rivet · pulledAT BS 1460, STRINGER 1 FOUND TWO OFF RIVETS PULLED & LOOSE. REPLACED IAW EA T F-5300-T0321171. CLASSIFIED AS A MAJOR CAT A WITH NO SMR REQUIREMENTS. EO F-5100-7-5001 PT 1 ATTACHMENTS B & C UPDATED ON THIS INPUT. REF JPF STAGES 1 - 2 FOR WORK CARRIED OUT.SDR FDEA201511043471Bracket · damagedDAMAGE FOUND ON FLOORBEAM TO FRAME BRACKET AT STATION 1681.8, RBL 70. FRAME BRACKET REPLACED IAW SRM 51-40-02 & DWG 146N8725. CLASSIFIED AS A MAJOR CAT A WITH NO SMR REQUIREMENTS. EO F-5100-7-5001 PT 1 ATTACHMENTS B & C UPDATED ON THIS INPUT. REF JPF STAGE
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