N991FD

Service difficulty reports · 133

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N991FD' AND registry_match = 'registration'
  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 FDEA201308051779Intercostal · crackedBS 400 INTERCOSTAL IS CRACKED AT FASTENER HOLE, RBL 24. REMOVED DAMAGED INTERCOASTAL, FABRICATED NEW INTERCOASTAL AND INSTALLED IAW SRM 51-40-02, MM 20-60-02-2, DWG 141N5150, FAS ER 2-37153-801A, REV D, SRM 51-40- 05, SRM 51-20-01, AMM 51-21-10-7 AND SRM 51-Aug 5, 2013 · N991FD · Boeing 757232 · Fuselage Miscellaneous StructureSDR FDEA201308041775Skin · gougedR2 DOOR UPPER HINGE CUTOUT GOUGED. REPAIRED IAW SRM 51-40-02 AND SRM 52-10-02, REP1.Aug 4, 2013 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201302160358Warning Message · false activationRECEIVED EICAS LT WING SLIDE ON FINAL APPROACH. LIGHT WENT OUT BEFORE LANDING. COULD NOT FIND IN QRH. MESSAGE WAS CLEARED BY TIME GOT TO GATE. GAINED ACCESS AND DID VISUAL INSPECTION OF LT DOOR NO DEFECTS NOTED. NO HISTORY.Feb 16, 2013 · N991FD · Boeing 757232 · Central WarningSDR FDEA201210163619Lamp · inoperativeR1 DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. LAMPED IAW AMM 33-51-06-2-1.Oct 16, 2012 · N991FD · Boeing 757232 · Emergency LightingSDR FDEA201210033545Wire · damagedDURING CLIMBOUT FL 210 L/E SLAT ASYM EICAS LIGHT AND L/E CAUTION LIGHT CAME ON. PRIOR TO LIGHTS FLAPS WERE UP, FLAP HANDLE UP AND FLAP INDICATOR INDICATED FLAPS UP. REDUCED SPEED TO 240 IAS LIGHTS STAYED ON DURING FLIGHT. NEEDED TO USE QRH PROCEDURES TO COct 3, 2012 · N991FD · Boeing 757232 · Flight Control System WiringSDR FDEA201206122192Bulb · burned outDURING TRANSIT CHECK, FOUND RT EMERGENCY LIGHT OUT. R & R BULB ASSY IAW AMM 33-51-06. OPS CHECKED GOOD.Jun 12, 2012 · N991FD · Boeing 757232 · Emergency LightingSDR FDEA201205201897Bulb · burned outEMERGENCY EXIT LIGHTS UNARMED LIGHT HAS BULB BURNED OUT. RELAMPED EMERGENCY EXIT UNARMED LIGHT IAW MM REF: 33-13-00-2-0. OPS CHECKED GOOD. OK FOR SERVICE.May 20, 2012 · N991FD · Boeing 757232 · Emergency LightingSDR FDEA201205101785Lamp · inoperativeR1 SLIDE LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.May 10, 2012 · N991FD · Boeing 757232 · Emergency LightingSDR FDEA201205011688Handle · wornL1 DOOR DOES NOT COMPLETELY CLOSE USING EXTERIOR HANDLES. DOOR OPENS AND CLOSES NORMALLY USING INTERIOR HANDLE. IF CLOSED USING INTERIOR HANDLE DOOR INDICATIONS ALSO NORMAL. FOUND THAT THE OUTSIDE DOOR HANDLE BUTTERFLIES EARLY, HAS EXCESSIVE PLAY, AND OVER May 1, 2012 · N991FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201204281665Lamp · inoperativeR1 SLIDE LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.Apr 28, 2012 · N991FD · Boeing 757232 · Emergency LightingSDR FDEA201204201511Windshield · failedF/O WINDSHIELD BEGAN TO ARC FROM LOWER LT CORNER, THEN SPREAD THROUGHOUT WINDSHIELD. TURNED OFF WINDOW HEAT, ENTIRE OUTER LAYER OF WINDSHIELD CRACKED. COMPLIED WITH QRH PROCEDURES. R & R WINDSHIELD IAW MM 56-11-01-4 AND EA F-5610-160380. ACFT OK FOR SERVICEApr 20, 2012 · N991FD · Boeing 757232 · Flight Compartment WindowsSDR FDEA201204061278Lamp · inoperativeDOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.Apr 6, 2012 · N991FD · Boeing 757232 · Emergency LightingSDR FDEA201203090862Lamp · inoperativeR1 EXIT EXTERIOR EMERGENCY LIGHT BURNED OUT. RELAMPED R1 EXTERIOR EMERGENCY LIGHT IAW MM 33-51-06-2-1. OPS CHECKED GOOD, ACFT OK TO CONTINUE. FINAL CLOSED.Mar 9, 2012 · N991FD · Boeing 757232 · Emergency LightingSDR FDEA201111034733Bottle · dischargedL1 DOOR DISCHARGE BOTTLE GAUGE SHOWS EMPTY. REMOVED AND REPLACED L-1 DOOR EMERGENCY POWER RESERVOIR REF AMM 52-11-30-4.Nov 3, 2011 · N991FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201110124435Mechanism · bindingWHILE WORKING ACFT, FOUND THAT ON 1L DOOR, UPPER AND LOWER FLAPPER DOORS WILL NOT CLOSE COMPLETELY FROM THE OUTSIDE. DOOR WILL CLOSE FROM THE INSIDE; HOWEVER, WHEN REOPENED A BINDING NOISE IS HEARD. REMOVED DOOR LINER, REF MM 52-11-02-4 AND INSPECTED AREA FOOct 12, 2011 · N991FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201110064342Hinge · damagedPRIOR TO PUSH TRYING TO SECURE 1L DOOR CLOSED DOOR WOULD NOT SHUT ALL THE WAY, RAMP AGENT NOTICED PROBLEM WITH HINGE. RELEASED FOR SERVICE IAW CDL: 52-11-01.Oct 6, 2011 · N991FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201109133860Skin · corrodedHORIZONTAL STAB CENTER COMPARTMENT BS 1844 AFT AREA, CORROSION ON SKIN BETWEEN STR'S 23, 25L. A SKIN REPAIR WAS ACCOMPLISHED ON MAE W/C 46130440001 & MAE EA 757- 5381- 16-F3411, REV- DATED 07/28/2011 AT STA 1844 B/T STR'S 23L- 25L. THIS NON ROUTINE IS FOR TRASep 13, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201109073742Skin · dentedBS 1665 BETWEEN S27-28R, PROTRUDING DENT. DENT FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG. 101 DET. III, REPAIRED IAWSRM 53-00-01 FIG. 201 REPAIR 16 CLASS B REPAIR MAJOR.Sep 7, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201109063722Skin · damagedFOUND SCRIBE LINE AT BS 676.613 THROUGH BS 680.125 AND S14L LAP JOINT. ACCOMPLISHED EA F-5330-147696, MAJOR REPAIR.Sep 6, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201109023639Angle · mismanufacturedREWORK REQUIRED DUE TO INCORRECT MATERIAL USED IN REPAIR. REACCOMPLISH REPAIR IAW EA F-5310-152605 ACCOMPLISHED EA F-5310-152605. MAJOR REPAIR.Sep 2, 2011 · N991FD · Boeing 757232 · Fuselage Miscellaneous StructureSDR FDEA201109023638Angle · mismanufacturedREWORK REQUIRED DUE TO INCORRECT MATERIAL USED IN REPAIR. REACCOMPLISH REPAIR IAW EA F-5310-152604. REMOVED REPAIR ANGLE IAW SRM 51-40-02. ACCOMPLISHED EA F-5310-152604. MAJOR REPAIR.Sep 2, 2011 · N991FD · Boeing 757232 · Fuselage Miscellaneous StructureSDR FDEA201108293566Skin · damagedFOUND SCRIBE LINE AT BSTA 1681.8 THROUGH 1700.55 S-10L LAP JOINT. ACCOMPLISHED EA F-5330-147692 PART 1 ONLY, VERIFICATION OF NO ADDITIONAL SCRIBLINES AT BUTT JOINT STA 1621 TO 1720 ALONG S-10L. PART 2 REQUIRED AT 1500FC AFTER PART 1 AND PART 3 OF EA REQUIRED Aug 29, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201108293565Skin · damagedFOUND SCRIBE LINE AT BSTA 1533 THROUGH 1534.25 S4L LAP JOINT ACCOMPLISHED EA F-5330-147690 PART 1 ONLY, VERIFICATION OF NO ADDITIONAL SCRIBELINES AT BUTT JOINT STA 1459 TO STA 1621 ALONG S-4L. PART 2 OF EA REQUIRED AT 1500 FC AFTER PART 1 AND PART 3 OF EA REQAug 29, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201108183360Frame · misrepairedFRAME REPAIR LOCATED AT BS 1520 S29R TO S29L DOES NOT CONFORM TO CURRENT SRM REQUIREMENTS. FRAME REPAIR REPLACED IAW EA. F-5310-147719.Aug 18, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201108103181Mount · corrodedNR 2 PYLON FWD ENG MOUNT STRUT FITTING WITH CORROSION ON LOWER SURFACE FWD AND AFT MOUNT MATING. REMOVED CORROSION BY BLENDING AREA PER SRM-54-51-90 PG.104 FIG.101 DET.VII, REMOVED AND REPLACED FWD. STRUT MOUNT FITTING, PER SRM-51-40-02.Aug 10, 2011 · N991FD · Boeing 757232 · Engine Mount SectionSDR FDEA201108053111Skin · misrepairedSKIN REPAIR LOCATED AT STA 1680, S-20L DOES NOT CONFORM TO CURRENT SRM CONFIGURATION.Aug 5, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201108043098Frame · misrepairedREPAIR AT BS 1240 BETWEEN S25L AND 26L DOES NOT CONFORM CURRENT S/F CONFIGURATION ACCOMPLISHED EA F 5310-152610. FUSELAGE EXISTING FRAME REPAIR REPLACEMENT AT BS 1240 AND S24L-S26L. MAJOR REPAIR.Aug 4, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201108033087Frame · misrepairedFRAME REPAIR AT STA 1200, S27R DOES NOT CONFORM TO CURRENT SRM S/F CONFIGURATION. ACCOMPLISHED EA F-5310-147708.Aug 3, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201108023072Fitting · corrodedFWD CARGO COMPT, CARGO TIE DOWN FITTING CORRODED AT STA 845, S-26L CENTER PLUG. REMOVED CORROSION STA 845 S-26L TIE DOWN FITTING IAW SRM 51-10-02. ORIG MAT .180 REMAINING .147 OUT OF LIMITS IAW SRM 53-00-53 FIG 101, DET V. REMAINING THICKNESS ACCEPTABLE IAWAug 2, 2011 · N991FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023071Fitting · corrodedFWD CARGO COMPT, CARGO TIE DOWN FITTING CORRODED AT STA 760, STR 26R. REMOVED CORROSION FROM TD FITTING STA 760, 26R IAW SRM 51-10-02. ORIG MAT .180 REMAINING .141 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET V. REMAINING THICKNESS ACCEPTABLE IAW EA. ACCAug 2, 2011 · N991FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023069Fitting · corrodedFWD CARGO COMPT, CARGO TIE DOWN FITTING CORRODED AT STA 680, STR 26R. REMOVED CORROSION TIE DOWN FITTING IAW SRM 51-10-02. BLENDED AREA ORIG. MAT .180 REMAINING .146 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET V. ACCOMPLISHED EA F5310-147700. MAJOR REPAAug 2, 2011 · N991FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023068Fitting · corrodedFWD CARGO COMPT, CARGO TIE DOWN CORRODED AT STA 640, STR 26R. REMOVED CORROSION TD FITTING IAW SRM 51-10-02. BLENDED AREA ORIG MAT .180 REMAINING .159 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET V. ACCOMPLISHED EA F5310-147700. BLEND OUT ACCEPTABLE IAW EAug 2, 2011 · N991FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023067Fitting · corrodedFWD CARGO COMPT, CARGO TIE DOWN FITTING CORRODED AT STA 720 STR 26R. REMOVED CORROSION TD FITTING IAW SRM 51-10-02. BLENDED AREA ORIG MAT .180 REMAINING .150 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET V. ACCOMPLISHED EA F-5310-147700. BLEND OUT ACCEPAug 2, 2011 · N991FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107293029Stringer Splice · failedAFT CARGO AREA AT BS 1460, STRINGER S29R, WITH DEEP GOUGE ON SPLICE. REMOVED STRINGER SPLICE IAW SRM 51-40-02 AND STRINGER CLIP IAW SRM51-40-02, REPLACED SPLICE IAW SRM 51-40-02 AND INSTALLED STR CLIP IAW SRM 51-40-02. MAJOR REPAIR.Jul 29, 2011 · N991FD · Boeing 757232 · Fuselage Main, Longeron/StringerSDR FDEA201107293024Skin · damagedFOUND 2EA VERTICAL SCRIBE LINES RUNNING INTO LAP SEAM AT S19R AND BUTT JOINT AT BS 661. ACCOMPLISHED EA F-5330-152621, MAJOR REPAIR.Jul 29, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201107283012Angle · failedL-2 DOOR UPPER HINGE CUTOUT DAMAGED. ACCOMPLISHED EA F-5210-152619. MAJOR REPAIR.Jul 28, 2011 · N991FD · Boeing 757232 · Fuselage Miscellaneous StructureSDR FDEA201107283005Skin · misrepairedPREVIOUSLY INSTALLED SKIN REPAIR AT BS 470 BETWEEN S22R-S23R DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED REPAIR, COMPLIED IAW EA F- 5330-147725. MAJOR REPAIR.Jul 28, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201107283004Skin · misrepairedPREVIOUSLY INSTALLED SKIN REPAIR AT BS 450 BETWEEN S23R- S24R DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED REPAIR COMPLIED IAW E.A. F-5330-147725. MAJOR REPAIRJul 28, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201107283013Frame · misrepairedFRAME REPAIR AT STA 780 S-28L TO S-28R DOES NOT CONFORM TO CURRENT SRM CONFIGURATION. REMOVED REPAIR AND COMPLIED WITH EA F-5310-147694 FUSELAGE MAIN FRAME EO F5100-7-5001, REPAIR REWORK STA 70 BETWEEN S-28L TO S-28R. MAJOR REPAIR.Jul 28, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201107202864Skin · crackedFUSELAGE SKIN ABOVE PRODUCTION DOUBLER HAS A CRACK ABOUT 1.3" LONG AT BS 1787.45, S-17L, WL 208. ACCOMPLISHED E.A. F 5330-152606. FUSELAGE STAB SEAL FAIRING SKIN CRACKED MAJOR REPAIR.Jul 20, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201107192801Shear Tie · corrodedAFT CARGO AREA AFTER REMOVAL OF DOUBLER FOUND AT STA 140 BETWEEN S-29R TO S-30 SHEAR TIE WORN AND HAS CORROSION. REMOVED CORROSION AT AFT CARGO SHEAR TIE STA 1400 BETWEEN S-29R TO S-30 IAW SRM 51-10-02. BLENDED AREA L=1 W=.5 D=.010 ORIGINAL MATERIAL .050 AFJul 19, 2011 · N991FD · Boeing 757232 · Fuselage Internal Mounting StructureSDR FDEA201107132684Frame · misrepairedFRAME REPAIR LOCATED AT STA 1580 BETWEEN S24L AND S25L MISREPAIRED. ACCOMPLISHED EA F5310-152611. MAJOR REPAIR.Jul 13, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201107132680Frame · inoperativeTHE PREVIOUSLY INSTALLED FRAME REPAIR LOCATED AT STA 1220 BETWEEN S24L TO S26L REQUIRES REPLACEMENT ACCOMPLISHED EA F-5310-147710, FUSELAGE-MAIN FRAME-EO F-5100-7-5001-EXISTING REPAIR. REWORK STA 1220 S-24L TO S-26L.Jul 13, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201107122664Skin · misrepairedSKIN REPAIR AT BS 400-420 BETWEEN S20L-S21L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. ACCOMPLISHED E.A. F5330-147718. MAJOR REPAIRJul 12, 2011 · N991FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201107072604Frame · damagedFRAME LOCATED AT STA 1640,S-6R-S-7R DAMAGED. ACCOMPLISHED E.A. F5310-152613.Jul 7, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201107062600Frame · damagedFRAME LOCATED AT BS 1400 BETWEEN S-25L TO S-26L DAMAGED. REPAIRED IAW F-5310-146538. CATEGORY "A" MAJOR REPAIR.Jul 6, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201107062598Frame · misrepairedFRAME AT STA 1260 BETWEEN S-25R AND S-26R MISREPAIRED. REMOVED EXISTING REPAIR ANGLE IAW EA F-5310-147706. MAJOR REPAIR.Jul 6, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201107062597Frame · damagedFRAME LOCATED AT BS 1320 BETWEEN S-23R DAMAGED.Jul 6, 2011 · N991FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201107062596Stringer Splice · gougedAFT CARGO AREA AT BS 1460, STRINGER S29L WIYH GOUGE ON SPLICE. REMOVED SPLICE AT BS 1460, STRINGER 29L IAW SRM 51-40-02. REPLACED SPLICE AT BS 1460, STRINGER 29L IAW SRM 51-40-02, PN 146N3820. REPAIR A , MAJOR REPAIR.Jul 6, 2011 · N991FD · Boeing 757232 · Fuselage Main, Longeron/StringerSDR FDEA201106282480Stringer · corrodedAFT CARGO COMPT STRINGER CORRODED AND GOUGED AT STA 1460 TO 1470, STR 29R REMOVED STRINGER STA 1460 THRU 1490 STR 29R IAW SRM 51-40-02, REMOVED GOUGES AND CORROSION IAW SRM 51-10-02 CHECKED LIMITS OF BLENDED AREA L= .60, W= .50, D= .050 ORIGINAL MATERIAL .Jun 28, 2011 · N991FD · Boeing 757232 · Fuselage Main, Longeron/Stringer
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