Boeing 757-2G5
Service difficulty reports · 557
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 = '7572G5' 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 = '7572G5' 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 IXXA20221201Skin · crackedLEFT MLG BODY DOOR EXTENSION TRAILING EDGE IS CRACKED/DIS-BONDED.SDR FDEA202210052470Panel · crackedRW LEADING EDGE PANEL BEHIND #7 SLAT IS CRACKED AT OB SPLICE AREA. REPAIRED RW LEADING EDGE PANEL BEHIND #7 SLAT IAW B757-200 SRM 57-41-02-2RFIG 201 SHEET 8 AND 51-70-07SDR FDEA202210052469Panel · damagedLH VERTICAL PANEL 322CL DAMAGED REPAIRED L/H VERTICAL STAB PANEL 322CL SKIN IAW B757-200 SRM 55-30-01-2R FIG 201 REPAIR 4 SHEET1 AND SRM 51-70-07-0G.SDR FDEA202209282381Gcu · failedON FINAL TO KSBD LOST THE LEFT AC BUS. WE HAD L GEN OFF, L BUS OFF, AND L BUS TIE TO ISLN ON THE OVERHEAD PANEL. LOST ASSOCIATED EQUIPMENT ON CAPTAIN SIDE. FLAPS AT 20 DEGREES. WENT AROUND AND RAN THE AC BUS OFF CHECKLIST. WE WE ABLE TO GET THE LEFT SDR IXXA20220929001Attach Angle · crackedFWD ATTACH ANGLE AT PANEL 198JR IS CRACKED(RT FILLET AREA) REF AMES N/R 147534-0100-0281SDR FDEA202208262078Support Bracket · corrodedAUXILIARY POWER UNIT DOOR SURROUND STRUCTURE CORRODED. REMOVED & REPLACED ANGLE SUPPORT BRACKETS & APU FWD STRAP OF AUXILIARY POWER UNIT DOOR SURROUND STRUCTURE IAW BAC DWG 148N3152-1, 148N3152-2 ,148N3141-5 & 148N3138-20.SDR FDEA202208222028Inlet · corroded#1 ENGINE INLET COWL MOUNT FLANGE ON THE ENGINE SIDE IS CORRODED SPORADICALLY AROUND THE ENTIRE CIRCUMFERENCE OF THE ENGINE REMOVED AND REPLACED ENGINE PER FEDEX CARD # 7180260-01-02SDR IXXA2022112901Skin · corrodedLEFT WING LOWER WING PNL STA. 822-829 IS CORRODED AT FUEL PNLSDR IXXA20220100201Bracket · corrodedREF AMES NR 147534-0100-0150 LWW FS1180 35" OTBD KEEL CENTER WEB AT CEILING ISOLATION VALVE STAND OFF MOUNTING WEB CORROSION ON AFT SIDE.SDR IXXA2022111103Web · corrodedKEEL WEB IN LEFT WHEEL WELL AT STA 1175 SHOWS SIGNS CORROSION AROUND HYDRAULIC LINESSDR IXXA20220100102Web · corrodedREF AMES NR 147534-0100-0077 AFT SIDE OF STA 900 WEB IS CORRODED AROUND PNEUMATIC DUCT AND HYDRAULIC LINE RBL 12SDR IXXA2022100101Skin · corrodedCORROSION ON UPPER SURFACE LWING 60" FROM FUSELAGE 18" FROM L/E. REF AMES NR 147534-0500-0030SDR IXXA2022093001Skin · corrodedCORROSION ON EXTERNAL SURFACE OF LEFT WING LOWER SKIN AT WS 74.5 AND APPROXIMATELY SIX INCHES AFT OF STRINGER L8 REF AMES NR 147534-0500-0018SDR IXXA20220929002Roller Tray · cutUPPER CARGO ROLLER TRAY AT RBL 30.0 IS CUT REF AMES N/R 147534-0200-0042SDR FDEA202110282647Flap System · malfunctionedWHEN SELECTING FLAPS 25, GOT TE FLAP DISAGREE ON EICAS. USED QRH TO SELECT FLAPS 20 WITH ALTERNATE SYSTEM AND LANDED UNEVENTFULLY. UPON BLOCK IN TO GATE FLAPS WERE DOWN. INSPECTED TRIALING EDGE FLAPS AND FOUND NO DISCREPENSIES. PER FIM 27-51 FAULT TSDR FDEA202105201321Idg · failedR GEN OFF CAUTION WITH ASSOCIATED R HYD ELEC 2, R UTIL BUS, AND L UTIL BUS ADVISORIES AT 40 KTS DURING TAKEOFF JUST AFTER PRESSING THR BUTTON FOR TAKEOFF THRUST. REJECTED, RAN QRH AND CAUTIONS CLEARED. COORDINATED WITH GOC AND MOCCASIN TO CONTINUE. ALLSDR FDEA202103040556Actuator · inoperativeUPON GEAR RETRACTION ON THE AFTER TAKEOFF PHASE THE NOSE GEAR DID NOT RETRACT. WE HAD A --NOSE GEAR GREEN LIGHT-- WITH --DOORS AMBER LIGHT-- ACCOMPANNIED BY --AMBER GEAR LIGHT-- WITH EICAS --GEAR DISAGREE-- ANNUNCIATION. HIGH NOISE AND VIBRATION. UPON LEVSDR IXXA20210225013Battery · inoperativeAIRCRAFT GROUNDED FOR UNSCHEDULED POWER PLANT MAINTENANCE, IDENTIFIED R1 DOOR EMERGENCY EXIT DOORS LIGHT INOPERATIVE. REMOVED AND REPLACED REMOVED AND REPLACED R1 EMERGENCY EXIT LIGHTS POWER SUPPLY IAW AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. NO FURTHESDR FDEA202102120340Guide Vane · damaged#1 ENGINE I/B GUIDE VANES COMPOSITE COVERINGS IS DAMAGED IN SEVERAL PLACES REPAIRED DAMAGE ON A-FRAMES IAW B757 AMM 72-34-10-6-4 AND RR EM 72-34-13-300-001SDR FDEA202102110332Skin · corrodedR/H WING #8 SLAT HAS CORROSION AT THE UPPER SURFACE AT BULLNOSE AREA APPROX 32.8" FROM I/B SIDE REPLACED SLAT PER B757 AMM 27-81-02-4SDR FDEA202102110333Cover · crackedL1 DOOR PRISM COVER CRACKED REMOVED AND REPLACED IAW B757 DWG 411N2044 REV ASDR FDEA202102110331Ring · crackedL1 DOOR TRIM RING ASSY CRACKED REPAIRED L1 DOOR TRIM IAW B757-2 AMM 25-00-00-8 STEP 7,E, METHOD 2 AND BAC 5010 TYPE 70SDR FDEA202102030285Structure · crackedMAIN CABIN R1 DOOR LOWER HINGE CUTOUT UPPER CORNER CRACKED TRIMMED OUT DAMAGED AREA PER BDWG 141N6200 SHEET 2 REVISION M AND B757 SRM 51-10- 02. HFEC ACCOMPLISHED TO VERIFY NO CRACK INDICATIONS PER B757 NDTM 51-00-19 PT 6. RESTORED SURFACE FINISH IAW B757 SSDR FDEA202102030283Skin · cracked#2 PYLON PANEL 443KL IS CRACKED. REPAIRED #2 PYLIN PNL 443KL CRACK IAW B757 SRM 54-50-70-2R FIG 201, 51-70-04-0G, B757AMM 51-24-02SDR FDEA202012023017Gust Lock · brokenL1 ENTRY DOOR GUST LOCK COLLAR BROKEN. REMOVED BROKEN PIECES OF GUST LOCK AND HARDWARE FROM DOOR HINGE AREA. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR, AS PER AMM 52-11-08-4. CHECKS OK.SDR FDEA202011212942Girt Bar · failedL1 GIRT BAR CENTERING BLOCK EXFOLIATED. REPLACED GIRT BAR AND GIRT BAR CENTERING BLOCK, REF B757 AMM 25-66-10-2. A/C OK FOR SERVICE.SDR FDEA202011202924Drag Fitting · crackedTHE RT WING OUTBOARD DRAG FITTING HAS INDICATIONS OF DEFECTS ON THE NR 4 & NR 13 HOLE. THE NR 4 HOLE HAS INDICATION AT THE 3 O`CLOCK LOCKING AFT AND NR 13 HAS INDICATION ALSO AT THE 3 O`CLOCK LOOKING AFT. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPLSDR FDEA202011202923Drag Fitting · corrodedTHE RT INBOARD DRAG FITTING UPPER SURFACE HAS CORROSION AT NR 3 AND NR 8 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPLACED INBOARD FITTING.SDR FDEA202011202922Drag Fitting · crackedTHE RT WING INBOARD DRAG FITTING HAS INDICATIONS ON THE NR 3, NR 8 HOLE AND THE 3RD HOLE FROM THE BOTTOM THAT ATTACHES TO THE SPAR. THE 2 HOLES THAT ATTACH TO THE SKIN HAVE MULTIPLE SIGNALS AND UNABLE TO CLOCK POSITION. THE 3RD HOLE FROM THE BOTTOM THAT ATTASDR FDEA202011202921Drag Fitting · crackedTHE RT UPPER SKIN DRAG FITTING NR 3 AND NR 5 HOLES HAVE INDICATIONS OF DEFECTS NOTED. THE NR 3 HOLE HAS INDICATION AT THE 1 O`CLOCK LOOKING AFT. THE NR 5 HOLE HAS INDICATION AT THE 12 O`CLOCK LOOKING AFT. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINSDR FDEA202011202918Drag Fitting · corrodedTHE RT WING OUTBOARD DRAG FITTING UPPER SURFACE HAS CORROSION ON NR 4 AND NR 13 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINGS-ATTACH FITTINGS-RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR. REPLACED OUTBOARD FITTING.SDR FDEA202011192911Skin · dentedLH ENGINE PYLON IB SIDE ABOUT MID SECTION ON LWR FACE HAS DENT. COMPLIED WITH FEDEX EA. F - 5430-T0358210 P1 NACELLS / PYLON - SKIN /PLATES/ PANELS - LH ENGINE PYLON INBOARD SIDE SKIN PANEL REPAIR NEAR PPS 136. PERFORMED SATIFACTORY LEAK CHECK IAW B757 AMMSDR FDEA202011072791Frame · crackedTHE RT 1640 FRAME BY STR 14R LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING OUTBOARD). REPAIR AS REQUIRED, LAYERS NEED TO BE SEPARATED TO DETERMINE WHAT LAYER HAS DEFECT ALL WORK ACCOMPLISDR FDEA202011072790Frame · crackedTHE LT 1640 FRAME BY STR 14L LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING INBOARD). REPAIR AS REQUIRED, LAYERS NEED TO BE SEPARATED TO DETERMINE WHAT LAYER HAS DEFECT. ALL WORK ACCOMPLSDR FDEA202009272333Idg · malfunctionedRECEIVED A LT GEN OFF EICAS ON TAKEOFF ROLL AND REJECTED THE TAKEOFF. RAN THE REJECTED TAKEOFF CHECKLIST AND THE QRH, WHICH RESET THE FAULTS. TRIED THE TAKEOFF AGAIN AND REJECTED FOR THE SAME LT GEN OFF EICAS FAULT. REPLACED NR 1 ENGINE IDG. OPS AND LEAK SDR FDEA2020091422189Lamp · inoperativeLT FUSELAGE EMERGENCY ESCAPE LIGHT BY L1 DOOR INOP. RELAMPED, REF AMM 33-51-06-2-1. GOOD FOR SERVICE.SDR FDEA2020072761662Tee Fitting · corrodedMAIN DECK BETWEEN STA 920-1040 RBL45.5 T CHORD CORRODED REMOVED CORR ON T CHORD STA 900-1040 RBL 45.5 IAW B757 SRM 51-10-02. ORIG MAT .090 REM O FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW T CHORD IAW B757 SRSDR FDEA202007241642Tee Fitting · corrodedMAIN DECK STA 1200 BETWEEN LBL 24.75- LBL 45.5 T CHORD CORRODED REMOVED CORROSION FROM BS 1200 FLOOR BEAM (T CHORD) IAW B757 SRM 51-10-02. ORIG MAT .125 REMAING 0 FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DET III, REPAIRED FLOOR BEAM IAW B757 SSDR FDEA202007201594Seat Track · corrodedSEAT TRACK HAS CORROSION IN MAIN CABIN @ RBL-45.5 BETWEEN STA. 1640 AND 1660 SEAT TRACK AT STA. 1640-1660 RBL45.5 OUT OF LIMITS DUE TO EXFOILATION IAW B757 SRM 53-00-52-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40-02 AND SDR FDEA2020072301594Seat Track · corrodedSEAT TRACK HAS CORROSION IN MAIN CABIN AT RBL 45.5 BETWEEN BS 1640 AND 1660. FOUND OUT OF LIMITS DUE TO EXFOILATION IAW SRM 53-00-52-1A, FIG 101. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK IAW SRM 51-40-00-02, DWG 657N3318, REV B, AND 657N3311, REV BSDR FDEA202007171565Crease Beam · corrodedMAIN DECK, BS 765 RT INBD CREASE BEAM WAS CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. EVALUATED 100% MATERIAL LOSS, AND OUT OF LIMITS IAW SRM 53-30-13, FIG 101. REPAIRED THE CREASE BEAM IAW SRM 53-00-13-2R, REP 1, ALT 1.SDR FDEA202007171564Seat Track · corrodedMAIN DECK BETWEEN BS 1060 - 1180 LBL 58.22, THE SEAT TRACK WAS CORRODED. REPAIRED IAW EA F-5310-T0355139 P1.SDR FDEA202007171563Frame · crackedDURING AN NDT OPEN HOLE INSPECTION, TWO CRACK NDICATIONS NOTED IN LOWER INBOARD HOLE AT APPROX. 8 AND 4 O'CLOCK POSTIONS LOOKING AFT. BS 1640 FRAME STRINGER 14L. ALL WORK ACCOMPLISHED IAW EA F-5310-T0355050 P1.SDR FDEA202007171562Seat Track · corrodedMAIN DECK BETWEEN STA 1180-1200 LBL 44.5 SEAT TRACK CORRODED. REMOVED CORR ON SEAT TRACK STA 1180-1200 LBL 44.5 IAW B757 SRM 51-10-02. ORIG MAT .070 REM 0 OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAWSDR FDEA202007171561Crease Beam · corrodedMAIN DECK BS 1600, LEFT SIDE INBD CREASE BEAM CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. EVALUATED 100% MATERIAL LOSS, OUT OF LIMITS IAW SRM 53-60-13-1A, FIG 101. REPAIRED THE CREASE BEAM IAW SRM 53-00-13-2R, REP 1, ALT 1.SDR FDEA2020072351517Floorbeam · corrodedMAIN DECK STA 1015 BETWEEN LBL24.75-LBL45.5 FLOOR SUPPORT CORRODED REMOVED CORR ON FLOOR SUPPORT STRAP ONLY IAW B757 SRM 51-10-02. ORIG MAT .012 REM .005 LOSS .007 FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101. REMOVE, FABRICATED AND INSTALLED NEW SDR FDEA2020071751517Strap · corrodedMAIN DECK BS 1015 BETWEEN LBL 24.75 - LBL 45.5 FLOORBEAM CORRODED. REMOVED THE CORROSION ON THE STRAP ONLY IAW SRM 51-10-02. ORIG MAT .012 REM .005 LOSS .007, FOUND OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101. REMOVED, FABRICATED AND INSTALLED A NEW STRASDR 2020F00333Battery Pack · dischargedDURING EMERGENCY LIGHT OPS CHECKS MULTIPLE LIGHTS FAILED TO COME ON. REMOVED AND REPLACED TWO BATTERY PACKS AT M736 AND M737 IAW AMM 33-51-07. REMOVED AND REPLACED 5 AMP FUSE IAW AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW 33-51-00 OPS CHECK GSDR 2020F00334Switch · faultyDURING EMERGENCY LIGHT OPS CHECKS MULTIPLE LIGHTS FAILED TO COME ON. REMOVED AND REPLACED TWO BATTERY PACKS AT M736 AND M737 IAW AMM 33-51-07. REMOVED AND REPLACED 5 AMP FUSE IAW AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CSDR 2020F00335Stringer · corrodedRIGHT WING STA 718 STRINGER U12 WAS CORRODED. REMOVED AND ELVAUATED CORROSION, ORIGNAL MATERIAL .100 IN., MATERIAL LOSS .068 IN., MATERIAL REMAINING .022., MATERIAL LOSS ALLOWABLE 10%. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND PERFORMED STRINGER REPAIR
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