Boeing 757-28A

Service difficulty reports · 2,000

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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 = '75728A'
  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.

SDR FDEA200908253081Frame · misalignedBS 600 FRAME LWR FLANGE OTBD OF STR 26L O/B HOLE ED WILL NOT ALLOW ACCOMPLISHMENT OF PTF CONVERSION - PREEXISTING INSTALL BS 600 FRAME, LWR FLANGE OTBD OF STR 26L O/B HOLE SED WAS ACCOMPLISHED ON MAE W/C NR 118250287 DSS R08, AND MAE NR 757-5332-16-F2205 REVAug 25, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908213064Frame · corrodedAFT FUSELAGE FRAME AT STA 1681.8 BETWEEN STR 22L AND 23L THE UPPER FLANGE HAS A SPOT OF SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02. BLENDED AREA TO GIVE SMOOTH AND ROUNDED SURFACE. PERFORMED HFEC FOR CRACKS IAW EA NR Aug 21, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908203061Splice · misalignedUPON INCOMING CONDITION AT STA 1040 LBL 45.5 THRU LBL 63.0, IF SPLICE CLIP 657N3338-33 IS LOCATED AND DRILLED WOULD HAVE POTENTIAL SHORT EDGE MARGIN WITH THE AFT FASTENER HOLES. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD A 757-5343-16-F2235-1 REPAIR CLIP WAAug 20, 2009 · N913FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA200908193054Crease Beam · corrodedRT CREASE BEAM INBD CHORD UPPER SURFACE CORR, STA 1340-1360. REMOVED CREASE BEAM, RECEIVED NEW CREASE BEAM PN 146N8326-2, INSTALLED CREASE BEAM RT AT STA 1300-1400, IAW SRM 51-40-02, CATEGORY "A", MAJOR REPAIR.Aug 19, 2009 · N913FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA200908183038Stringer · corrodedFS 440, STR 18L CORRODED. REMOVED STR, FABED NEW STR ON MAE TRAV NR T9/799070, INSTALLED STR REPAIR IAW SRM 51-40-02, AT STA 400-440, S18L, CATEGORY "A". MAJOR REPAIR.Aug 18, 2009 · N913FD · Boeing 75728A · Fuselage Main, Longeron/StringerSDR FDEA200908183037Crease Beam · corrodedAFT PIT STA 1343, NR 3 LT DOOR LWR HINGE MOUNT CLIP EXFOLIATED STR 17. REMOVED CREASE BEAM, RECIEVED NEW PART NR 146N8326-1, INSTALLED CREASE BEAM STA 1290-1370, IAW SRM 51-40-02, CATEGORY "A", MAJOR REPAIR.Aug 18, 2009 · N913FD · Boeing 75728A · Fuselage Main, StructureSDR NOCA05209Fuel Tank · peelingON DESCENT THE LEFT ENGINE SHUT DOWN, AN INFLIGHT START WAS ACCOMPLISHED. FLIGHT CREW DECLARED AN EMERGENCY. NR 1 ENG LOW PRESSURE FUEL FILTER REMOVED, INSPECTED FOR WATER/ CONTAMINATION NEEDS TO BE REPLACED, NO WATER OR CONTAMINATION FOUND. REPLACED NR 1 EAug 18, 2009 · N752NA · Boeing 75728A · Fuel StorageSDR FDEA200908173035Floorbeam · damagedWHILE DELETING PARTS FOR AFT PALLET MOD, LT PRODUCTION FOUND SEVERAL FASTENER HOLES WITH LESS THAN 40 PITCH. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD, A REPAIR WAS ACCOMPLISHED AT STA 1640, WHERE THE FLOORBEAM AND FRAME MEET. WORKED ON MAE MOD W/C 11835Aug 17, 2009 · N913FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200908173034Floorbeam · damagedWHILE DELETING PARTS FOR AFT PALLET MOD RHS PRODUCTION FOUND SEVERAL FASTENER HOLES WITH LESS THAN 40 PITCH. DUE TO DISCREPANCY EFFECTING THE PTF MOD, A REPAIR WAS ACCOMPLISHED AT STA 1640, WHERE THE FRAME AND FLOOR BEAM MEET. WORKED ON MAE MOD W/C 1183504Aug 17, 2009 · N913FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200908133010Skin · dentedDENT AT BS 1730, S3L, FUSELAGE SKIN. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101, DETAIL 3. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED TREATED AND PRIMED PER SRM 53-00-01, REPAIR 3. INSTALLED REPAIR DOUBLER AAug 13, 2009 · N913FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200908112973Splice · misalignedEXISTING FASTENER PATTERN AT STA 900 AND LT INNER CREASE BEAM CHORD SPLICE DOES NOT ALLOW THE NEW 657N3338-31 SPLICE TO BE INSTALLED WITHOUT DRILLING THRU IT'S MILLED RADIUS. A REPAIR SPLICE WAS FABRICATED TO REPLACE THE 657N3338-31 SPLICE. ACCOMPLISHED ON MAug 11, 2009 · N913FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA200908112977Seat Track · mismanufacturedSEAT TRACK AT STA. 1640 RBL 24.75 HAS THE SCALLOPS MILLED OUT 6" IN LENGTH AND WILL INTERFERE WITH THE INSTALLATION OF THE HANDLING SYSTEM. FABRICATED SEAT TRACK PER DRAWING 146N5130. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02.Aug 11, 2009 · N913FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908112976Seat Track · mismanufacturedSEAT TRACK AT STA. 1640 LBL 24.75 HAS THE SCALLOPS MILLED OUT 6" IN LENGTH AND WILL INTERFERE WITH THE INSTALLATION OF THE HANDLING SYSTEM. FABRICATED SEAT TRACK PER DRAWING 146N5130 MAT. I.D. BAC1520-792 BATCH 0001511987. REMOVED AND REPLACED SEAT TRACK IAug 11, 2009 · N913FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908112975Skin · dentedDENT AT BS 1708, S-13R/14R, 4" ABOVE SKIN LAP JOINT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01. THIS IS A CLASS "A" REPAIR.Aug 11, 2009 · N913FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200908112974Skin · dentedDENT AT BS 720-740, S-20L/21L, FUSELAGE SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER FROM 2024-T3 .071 IAW SRM 53-00-01. THIS IS A CLAS "B" REPAIR WITH INSPECTION THRESHOLD AT 37,500 F.C. AND INTERNAL INSPECTIONS EVERY 6,000 FC.Aug 11, 2009 · N913FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR NOCA05109Eec · inoperativeAFTER STARTING RIGHT ENGINE, RIGHT EEC INOP LIGHT & RIGHT ENGINE LIMITER INOP LIGHT REMAINED ON. SWAPPED RIGHT & LEFT EEC & FOUND RIGHT EEC INOP. RIGHT EEC WOULD NOT BITE TEST IN EITHER POSITION. RETURNED BOTH EEC TO ORIGINAL POSITION PER AMM 73-21-07. REPAug 9, 2009 · N752NA · Boeing 75728A · Fuel Control/Turbine EnginesSDR FDEA200908072950Frame · dentedFWD CARGO COMPT. RT FRAME AT STA 720, HAS A DENT BETWEEN STR- 25R-27R. TRIMED DAMAGED AREA IAW SRM 53-00-07. FABED REPAIR ANGLE ON MAE TRAV T9/800371. INSTALLED REPAIR ANGLE BS. 720, BETWEEN STR- 25R- 27R, IAW SRM 53-00-07. THIS IS A CLASS "B", REPAIR 5, WITAug 7, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908072949Frame · dentedFWD CARGO COMPT. RT FRAME AT STA 660, HAS A DENT BET STR- 24R-25R. CUT OUT FRAME SECTION IAW SRM 53-00-07, FABED NEW FRAME REPAIR ON MAE TRAV T9/800360, INSTALLED FRAME "J" SECTION REPAIR PARTS STA 660, STR 24R-25R, IAW SRM 53-00-07. CATEGORY "B" REPAIR 5. THAug 7, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908072948Skin · corrodedRT NAC- I/B FWD PANEL 443GL CUT OUT EXTERNAL SURFACE CORRODED. REMOVED SKIN, FABRICATED NEW SKIN P/N 311N5193-1, INSTALLED NEW SKIN ASSY I/B PYLON SURFACE, IAW SRM 54-50-01, 51-20-01, 51-40-02. MAJOR REPAIR.Aug 7, 2009 · N913FD · Boeing 75728A · Nacelle/Pylon, Plate/SkinSDR FDEA200908072947Seat Track · damagedSEAT TRACK AT STA 1640 LBL 45.50 HAS THE SCALLOPS MILLED OUT 6" IN LENGTH AND WILL INTERFERE WITH THE INSTALLATION OF THE HANDLING SYSTEM. REMOVED SEAT TRACK STA 1540-1640 LBL 45.50 PER SRM 51-40-02. VERIFIED MATERIAL PER SRM 53-60-52 FIG 1 AS BAC1520-792. FABAug 7, 2009 · N913FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908072946Seat Track · damagedSEAT TRACK AT STA 1640 RBL 45.50 HAS THE SCALLOPS MILLED OUT 6" IN LENGTH AND WILL INTERFERE EITH THE INSTALLATION OF THE HANDLING SYSTEM. REMOVED SEAT TRAC STA 1540-1640 RBL 45.50 PER SRM 51-40-02. VERIFIED MATERIAL PER SRM 53-60-52 FIG 1 AS BAC1520-792. FAAug 7, 2009 · N913FD · Boeing 75728A · Fuselage Main, StructureSDR NOCA04809Light · inoperativeR4 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED IAW AMM 33-51-00, OPS OK.Aug 3, 2009 · N752NA · Boeing 75728A · Emergency LightingSDR NOCA04709Autothrottle Sys · malfunctionedREJECTED TAKEOFF DUE TO A/T DISCONNECT AND AUTOTHROT DISC EICAS LIGHTS ILLUM WITH A/T ENGAGED IN EPR MODE. THRUST REF MODE DISP ON EICAS AND F/S POINTER DISPLAY ON ADI NORM (RTO AT 90 KTS). HIGH ENERGY STOP INSPECTION ACCOMPLISHED / PLACARD A/T INOP PER MEL Jul 31, 2009 · N750NA · Boeing 75728A · Auto Throttle SystemSDR FDEA200907312858Support · corrodedAPU INLET DOOR HSG FWD FRAME SUPPORT HAS CORROSION UNDER NUTPLATES. REMOVED FWD STRAP, FABRICATED NEW STRAP ON MAE TRAV NR T9/799157, AND INSTALLED FWD STRAP AT APU INLET, STA 1787, S3R- S6R IAW SRM 51-40-02, 51-10-02, 53-80-07. CATEGORY "A", MAJOR REPAIR.Jul 31, 2009 · N913FD · Boeing 75728A · Fuselage Main, StructureSDR NOCA04609BBAutothrottle Sys · disconnectedREJECTED TAKEOFF DUE TO A/T DISCONNECT RTO 90 KNOTS. HIGH ENERGY STOP INSPECTION ACCOMPLISHED/ PLACARD A/T INOP PER MEL 22-30-1, ITEM REMAINS OPEN.Jul 31, 2009 · N750NA · Boeing 75728A · Auto Throttle SystemSDR NOCA04609AABulb · inoperativeEXTERIOR EMERGENCY LIGHT (EVACUATION SLIDE) AT L1 DOOR INOP. RELAMPED SAME IAW AMM 33-51-00, OPS CHECK OK.Jul 30, 2009 · N752NA · Boeing 75728A · Emergency LightingSDR FDEA200907272791Support · corrodedFWD CABIN FLOORBEAM AT STA 365, BET RBL 0, AND RBL 16, HAS CORRISON, REMOVED SUPPORT, FABED NEW SUPPORT ON MAE TRAV NR T9/798619, INSTALLED SUPPORT AND T- CHORD REPAIR PARTS AT STA 324- 365, LBL-17, RBL- 70, IAW SRM 51-40-02, 53-00-5, CATEGORY "A", REPAIR NR3Jul 27, 2009 · N913FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA200907242734Seat Track · corrodedSTA 377-418, SEAT TRACK SUPPORT IS CORRODED AT LBL 24. REMOVED CORROSION IAW SRM 53-00-52, DETAIL7 AND FOUND OUT OF LIMITS. ORIG MAT.=.070 INCH, AFTER REWORK=.054 INCH, REMOVED .016 INCH. REMOVED AND FABRICATED NEW SUPPORT, PN BAC1508-237, IAW BATCH NR 161Jul 24, 2009 · N913FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907232725Web · corrodedMCD STA 920, S17L, WEB IS CORRODED AND CRACKED. REMOVED WEB, FABED WEB ON MAE TRAV NR T9/798803, INSTALLED WEB STA 920, S17L, IAW SRM 51-40-02, 51-20-01. CATEGORY "A", MAJOR REPAIR.Jul 23, 2009 · N913FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA200907212687Floorbeam · corrodedFWD CABIN FLOORBEAM UPPER SURFACE AT BS 377, LBL 61, HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, DETAIL 3, FIG. 101. CUT OUT DAMAGED AREA AND REMOVED PREVIOUS REPAIR OF UPPER TEE CHORD, BS 377, LBL 70Jul 21, 2009 · N913FD · Boeing 75728A · Fuselage Main, Floor BeamSDR NOCA03909Coffeemaker · defectiveCOFFEEMAKER IN AFT GALLEY, SPARKS COMING FROM WIRING. REPLACED COFFEEMAKER AS PER MM 25-31-99.Jun 27, 2009 · N755NA · Boeing 75728A · Buffet/GalleysSDR CNMA20090012Floorbeam · corrodedCABIN FLOORBEAM BS 345 IS CORRODED ON UPPER FLANGE BETWEEN BL 0 AND RBL 70. REMOVED DAMAGED PART OF THE FLOORBEAM UPPER CHORD (REF NR37652) ASSEMBLED AND INSTALLED PARTS IAW SRM 53-00-51 FIG 201 DETAIL I.Jun 23, 2009 · N639AX · Boeing 75728A · Fuselage Main, Floor BeamSDR CNMA20090011Floorbeam · corrodedCABIN FLOORBEAM AT BS 345 IS CORRODED ON UPPER FLANGE BETWEEN BL 0 AND LBL 24.75. REMOVED THE DAMAGED PART OF THE FLOORBEAM UPPER CHORD. ASSEMBLED AND INSTALLED THE REPAIR PARTS IAW SRM 53-00-51 FIG 201 DETAIL I.Jun 23, 2009 · N639AX · Boeing 75728A · Fuselage Main, Floor BeamSDR CNMA20090010Floorbeam · corrodedCABIN FLOORBEAM BS 365.25 IS CORRODED ON UPPER FLANGE BETWEEN BL 0 AND RBL70. FLOORBEAM BS 365.25 BETWEEN BL 0 AND RBL 70 IS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. FABRICATED PARTS IAW SRM 53-00-51. REPAIR NR 3 TREATED AND PRIMED PARTS AND AREA IAW SRMJun 18, 2009 · N639AX · Boeing 75728A · Fuselage Main, Floor BeamSDR NOCA03809Apu · inoperativeAPU INFLT START UNSUCCESSFUL, OK ON GROUND.Jun 17, 2009 · N750NA · Boeing 75728A · APU Core EngineSDR NOCA03609Apu · malfunctionedFLIGHT CREW REPORTED DURING SCHEDULED APU INFLT START APU DID NOT START INFLIGHT. FLIGHT WAS NOT AN ETOPS FLIGHT. OAT (-58 C), ALT FL 390, PEAK EGT 20, 3 ATTEMPTS - NO START. IF START NOT SUCCESSFUL DID APU SHUT DOWN AFTER 95 % ? NO IF START NOT SUCCESSFUJun 9, 2009 · N750NA · Boeing 75728A · APU Core EngineSDR NOCA03209Charger · inoperativeEMERGENCY LIGHTS INOP ROW 12 ABC- 20 ABC. REPLACED BATTERY CHARGER ASSEMBLY AS PER MM 33-51-07.May 25, 2009 · N750NA · Boeing 75728A · Emergency LightingSDR NOCA03009Impeller · brokenLEFT ENG FLAMED OUT ON DESCENT THROUGH FL 250 IN FLT START ENVELOPE DISPLAYED & CONDITION ADEQUATE TO ATTEMPT RESTART, RESTARTED AT FL 120 & OPERATED NORMAL TO GATE. MX IS FOLLOWING FIM'S 71-05-00 FIG 106, PER REQUEST 73-21-00 FIG 118, PER REQUEST 71-06-00 FIMay 22, 2009 · N752NA · Boeing 75728A · Engine Fuel PumpSDR NOCA03109Pin · looseEMERGENCY LIGHTS BY DOOR 3L NOT WORKING. SECURED LOOSE PIN 10 ON CONNECTOR D76 BATTERY PACK M735 AS PER MM 33-51-00 AND WD33-51-22, OPS CHECK OK.May 22, 2009 · N754NA · Boeing 75728A · Light System WiringSDR NOCA02809Apu · malfunctionedMCC REQUESTED AN APU IN FLIGHT START. APU FAULT LIGHT AND APU AUTO SHUT DOWN, IN FRU OPENED CI 49-08 FOR APU IN FLT START IS REQUIRED DUE TO UNSUCCESSFUL START.May 10, 2009 · N754NA · Boeing 75728A · APU Core EngineSDR FDEA200904291467Panel · damagedVERTICAL STAB, RT SIDE CROWN PANEL ATTACHMENT STRIP HAS DAMAGED HOLES, LOWER AFT CORNER. ACCOMPLISHED VERTICAL STAB FIXED T/E BEAM REPAIR AND FITTING REPLACEMENT IAW EA F-5530-124086, AND ATTACHMENTS A AND B OF EA, RELEASE DATE 04/20/09. THIS REPAIR IS CLASSApr 29, 2009 · N912FD · Boeing 75728A · Rudder, Plate/SkinSDR FDEA200904291466Skin · dentedDENT ON FUSELAGE SKIN AT BS 1575, S-26R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL 3. ACCOMPLISHED REPAIR AND INSTALLED IAW SRM 53-00-01, REPAIR NR 16. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.Apr 29, 2009 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200904291465Skin · dentedDENT ON FUSELAGE BS 1628, AT S-26L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL 3. HFEC ACCOMPLISHED WITH NO CRACKS NOTED. ACCOMPLISHED REPAIR AND INSTALLED IAW SRM 53-00-01, REPAIR NR 7, FIG 1 AND 2. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REApr 29, 2009 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR NOCA02309Slide · unserviceableFOUND L4 DOOR SLIDE PRESSURE INDICATION NEEDLE IN RED ZONE. REMOVED AND REPLACED L4 DOOR SLIDE AS PER AMM 25-66-01.Apr 17, 2009 · N756NA · Boeing 75728A · Escape SlideSDR NOCA02209Light · inoperativeFLOOR PATH EMERGENCY LIGHTS INOP BETWEEN ROWS 10 - 15. REMOVED AND REPLACED FOUR EMERGENCY LIGHT ASSY'S FOR THE FLOOR PATH EMERGENCY LIGHTS SYSTEM BETWEEN ROWS 10 - 15 IAW THE WDM 33-51-14 SYSTEM, OPS CHECKS NORMAL.Apr 16, 2009 · N756NA · Boeing 75728A · Emergency LightingSDR NOCA01409Fuse · blownEXTERIOR EMERGENCY EXIT LIGHT AT DOOR 2R LIGHT IS INOP. REPLACED LIGHT ASSY FUSE AND CLEANED TERMINALS, OPS CHECK GOOD AS PER MM 33-51-00.Mar 23, 2009 · N750NA · Boeing 75728A · Emergency LightingSDR NOCA01309Light · inoperativeEMERGENCY LIGHT BY SEAT 28C INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY AS PER AMM 33-51-11. OPS CHECK OK.Mar 14, 2009 · N752NA · Boeing 75728A · Emergency LightingSDR NOCA01109Eec · faultyN1/EPR FAILED TO ENGAGE TO THRUST WHEN SELECTED ON TAKEOFF ROLL. RT ENGINE LIMITER MESSAGE ILLUMINATED ON EICAS FOR APPROXIMATELY 3 SECONDS THEN EXTINGUISHED. REPLACED RIGHT EEC PER MM 73-21-00.Mar 8, 2009 · N750NA · Boeing 75728A · Fuel Control/Turbine EnginesSDR FDEA200903010773Skin · dentedLOWER LOBE FUSELAGE SKIN, BS 485, LBL, DENTED. REPAIR ACCOMPLISHED ON MAE 757-5300-16-A1824.Mar 1, 2009 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200902230671Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER CHORD LOWER SURFACE HAS CORROSION, STA 1681. MAIN CABIN FLOORBEAM UPPER CHORD REPAIRED IAW EA 757-5365-16-F1710 REV-C AT STA 1681, LBL- 58, TO RBL- 58. REPAIR CLASSIFIED AS MAJOR ALTERATION.Feb 23, 2009 · N912FD · Boeing 75728A · Fuselage Main, Floor Beam
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