N997FD

Service difficulty reports · 158

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 = 'N997FD' 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 FDEA201409242757Lifter · wornFOUND R1 DOOR NOT RELEASING GIRT BAR WHEN DISARMED. SLIDE FELL OUT ONTO STAIRS BUT DID NOT INFLATE, ALSO DOOR ASSIST BOTTLE DEPLOYED. ALSO DOOR ASSIST BOTTLE DEPLOYED. R & R R1 DOOR EMERGENCY POWER SPRING CYLINDER. INSTALLED NEW SLIDE. R & R RT R1 DOOR Sep 24, 2014 · N997FD · Boeing 757200 · Emergency EquipmentSDR FDEA201409142609Piston · damagedL1 ENTRY DOOR EMER POWER SPRING CYLINDER PISTON BROKEN. R & R THE EMER POWER SPRING PISTON FOR THE L1 DOOR IAW AMM 52-11-33-4-0. OPERATIONS CHECKED GOOD.Sep 14, 2014 · N997FD · Boeing 757200 · Passenger/Crew DoorsSDR FDEA201305070934Battery Pack · inoperativeL1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT WILL NOT LIGHT. R & R SLIDE LIGHT POWER SUPPLY BATTERY PACK IN REF WITH AMM 33-51-07-2. OPS NORMAL. ACFT IS OK FOR SERVICE.May 7, 2013 · N997FD · Boeing 757200 · Emergency LightingSDR FDEA201305040911Cover · damagedFOUND SLIDE COVER ASSY FOR LT ENTRY DOOR SAGGING AND BROKEN. FOUND LOWER SLIDE COVER LATCH HAD BECOME LOOSE AND PULLED OUT OF COVER. ATTACHED LOWER SLIDE COVER LATCH PER SMP. INSTALLED.May 4, 2013 · N997FD · Boeing 757200 · Escape SlideSDR FDEA201304240856Frame · damagedTWO MISSED DRILLED HOLES, L2 DOOR FUSELAGE FRAME BS 680 BETWEEN S12-13L. REPAIRED IAW EA F-5310-154149 PT 1.Apr 24, 2013 · N997FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201304210823Skin · crackedCRACK ON CROWN SKIN S4R, BS 403, 1.25 INCHES LONG. REPAIRED IAW EA F-5330-154147 PART 1.Apr 21, 2013 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201304190814Shear Tie · crackedSHEAR TIE CRACKED BS 1300 BETWEEN STR 20 - 21 LT. REMOVED DAMAGED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW DWG 140N2002 AND INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.Apr 19, 2013 · N997FD · Boeing 757200 · Fuselage Internal Mounting StructureSDR FDEA201304190811Skin · dentedSKIN DENTED BS 1597 AT STRINGER 15R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW STA MOBILE SF SRM 53-00-00 AND SRM 53-00-01, REP 15, FIG 201.Apr 19, 2013 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201304190810Skin · dentedSKIN DENTED BS 1443 BETWEEN STRINGERS 23-24L. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER OF 2024T3 .063" AND INSTALLED. REPAIR DOUBLER ALL IAW SRM 53-00-01, REP.16, FIG 201 AND 51-40-02.Apr 19, 2013 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201304190809Skin · dentedSKIN DENTED BS 404 AT STRINGER 16L. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-00-00 AND SRM 53-00-01, REP 15, FIG 201.Apr 19, 2013 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201212144303Switch · dirtyWITH LT FWD ENTRY DOOR OPEN, THERE IS NO EICAS ALERT NOR IS "ENTRY DOORS" OVERHEAD PANEL ANNUNCIATOR ILLUMINATED. RT FWD ENT DOOR ALERT IS NORMAL. CLEANED DOOR SWITCH IAW SMP, INDICATIONS NORMAL. OK FOR SERVICE.Dec 14, 2012 · N997FD · Boeing 757200 · Door Warning SystemSDR FDEA201212054248Sequence Valve · malfunctionedON APPROACH, LOWERED MLG, RECEIVED A "GEAR DISAGREE" EICAS MESSAGE. NO INDICATION ON NOSE GEAR. BOTH MAIN GEAR DOWN AND LOCKED GREEN INDICATION WITH AN AMBER DOORS LIGHT ILLUMINATED AS WELL AS AN AMBER GEAR LIGHT. COMPLETED A GO AROUND AND COMPLIED WITH QRDec 5, 2012 · N997FD · Boeing 757200 · Landing Gear Retraction/Extension SystemSDR FDEA201210123605Actuator · malfunctionedNOSE GEAR EXTENSION TAKES ABOUT DOUBLE THE TIME AS NORMAL ALONG WITH "GEAR DISAGREE" ALERT & THEN "GEAR DOOR: ALERT" R & R NOSE GEAR LOCK ACTUATOR IAW MM 32-34-02-4 AND PERFORM ADJ /TEST IAW 32-34-00-5 SWUNG GEAR SEVERAL TIMES AND OPS. CHECKED NORAML. ACFOct 12, 2012 · N997FD · Boeing 757230 · Landing Gear Retraction/Extension SystemSDR FDEA201202260685Actuator · failedDURING CRUISE FLIGHT AT FL 360 RECEIVED AN EICAS " LT HYD QTY " MESSAGE, LT SYS QUANTITY READ .48, AND "RSVR" LIGHT ILLUMINATED ON HYD OVERHEAD PANEL. LT SYS QUANTITY WAS DECREASING .01 EVERY FEW SECONDS, LOWERED GEAR WITH QUANTITY READING ABOUT .25. RECEIVEFeb 26, 2012 · N997FD · Boeing 757200 · Elevator Control SystemSDR FDEA201105051760Floor Panel · damagedUNABLE TO INSTALL FLOOR PANEL BETWEEN STA 900-1020 LBL 45.5 - RBL 64.2. DUE TO INCOMING ACFT CONFIGURATION AND EXISTING REPAIR AT STA 900-1020, LBL 45.5 - RBL 64.2 FLOOR PANEL FABRICATION AND INSTALLATION WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P May 5, 2011 · N997FD · Boeing 757200 · Fuselage Floor PanelSDR FDEA201105031740Skin · crackedL4 DOOR INNER SKIN MID SECTION IS CRACKED L4 DOOR INNER SKIN MID SECTION CRACK REPAIR ACCOMPLISHED ON STAM EA 757-5211-16-F-2354, REV- DATED APRIL 27, 2011 AND 8110-9, DATED APRIL 26, 2011. REF: EA F-5210-146524 THIS N/R IS FOR TIME TRACKING PURPOSES ONLY. May 3, 2011 · N997FD · Boeing 757200 · Passenger/Crew DoorsSDR FDEA201104141489Bulkhead · gougedNR 2 PYLON AFT BULKHEAD DAMAGED, COMPLIED WITH EA F-5450-146384. REPAIR CLASSIFIED AS A CAT "A" MAJOR.Apr 14, 2011 · N997FD · Boeing 757200 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201104141488Bulkhead · gougedBULKHEAD DAMAGED, COMPLIED WITH EA F-5450-146255. REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR.Apr 14, 2011 · N997FD · Boeing 757200 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201103231161Rub Strip · damagedAFTER REMOVAL OF RUBSTRIP ON NR 2 ENGINE OTBD CORE COWL, UPPER HINGE GOUGE FOUND. POWER PLANT-COWLING CORE COWL SKIN REPAIR COMPLIED WITH ON E. A. F-7111-146400 STEPS 1-23 DATED 03/17/2011,8100-9 DATED 05/03/2011 CAT MAJOR REPAIR.Mar 23, 2011 · N997FD · Boeing 757200 · Nacelle/Pylon, Main FrameSDR FDEA201103231317Skin · misrepairedFUSELAGE UPPER CROWN HAS PREVIOUS LIGHTNING STRIKE REPAIR AT FS 1661, JUST BELOW STR 5L, THE REPAIR FASTENER CONTACTS THE STRINGER AND CAUSES DISPLACEMENT ( DENT ) OF STRINGER. COMPLIED WITH EA. F5330-146283 DATED 3/31/11. 8100-9, MAJOR REPAIR.Mar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201103231182Frame · gougedMDC FRAME AT STA.310.5 AND STRINGER 4L, GOUGED. MAIN CARGO DECK FRAME AT STA 310.5 S-4L WAS REPAIRED IAW EA F-5310-146268. MAJOR REPAIRMar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201103231282Frame · damagedAFT CARGO COMPT FRAME HAS 2 DRILLED HOLES ON UPPER CHORD BEND RADIUS AT STA 1520, STR 26R. FUSELAGE STA 1520 LOWER LOBE FRAME REPAIR, REPAIRED ON EA F-5310-146389. MAJOR REPAIR.Mar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201103231232Frame · misrepairedAFT CARGO COMPT FRAME HAS A IMPROPER REPAIR AT STA 1520, STR 26-L. REMOVED IMPROPER SPLICE ON STA 1520, S-26L IAW SRM 51-40-02, FABRICATED NEW SPLICE ON STAM TRAVELER NR T10/863349, LOCATED & DRILLED NEW SPLICE IAW SRM -53-00-07-3, INSTALLED NEW SPLICE IAW SMar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201103231365Stringer · misrepairedFUSELAGE STRINGER REPAIR STA 1610, STR 19 MISREPAIRED. REMOVED REPAIR PER SRM 51-40-02. FABRICATED NEW HAT SECTION REPAIR PART, SRM 53-00-03, ON TRAVELER T11/877285, PER SRM 53-00-03. INSTALLED NEW HAT SECTION AT BS 1610, S19R, PER SRM 53-00-03, REPAIR 2, P.20Mar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, Longeron/StringerSDR FDEA201103231184Skin · damagedFUSELAGE SKIN BETWEEN BS 1620 AND 1630 AT STRINGER 1, AREA HAS TOOLMARKS ON 5 LOCATIONS, AS MARKED AT 12 0'CLOCK. ACCOMPLISHED AND COMPLIED WITH EA F-5330-146390. MAJOR REPAIR.Mar 23, 2011 · N997FD · Boeing 757231 · Fuselage Main, Plate/SkinSDR FDEA201103231351Skin · misrepairedREPAIR AT BS 1703 TO BS 1718 AT STR 14L/16L REQUIRES REPLACEMENT DUE TO NON COMPLIANCE WITH APPROVED DATA. REMOVED NON-COMPLIANT REPAIR, AND INSTALLED NEW REPAIR IAW SRM 51-40-02 AND SRM 53-00-01, DETAIL 1, P 201-204, REPAIR NR 15, CAT. "B" REPAIR, AT BS 1703Mar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201103231281Splice Plate · misalignedPRODUCTION SPLICE CAP HAS ELONGATED HOLES AT STA 1520 STR 24- 25R. REMOVED SPLICE PLATE BS 1520, STR 24R TO 25R IAW SRM 51-40-02, FABRICATED SPLICE PLATE ON STAM TRAVLER NR T10/864155, LOCATED & DRILLED SPLICE PLATE IAW SRM 51-10-02, INSTALLED NEW SPLICE PLMar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA201103231237Skin · damagedFUSELAGE SKIN AT STA 400-410, STR 25R-27R REQUIRES REPLACESMENT DUE TO LACK OF APPROVED DATA. REPAIRED IAW SRM 53-00-01. REPAIR 15, FIG 201, DETAIL I. MAJOR REPAIR.Mar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201103231233Skin · misrepairedEXSITING FUSELAGE SKIN REPAIR AT STA 1610-1620, STA 19R REQUIRES REPLACEMENT NOT PER CURRENT SRM REQUIREMENTS. REMOVED EXISTING DOUBLER IAW SRM 51-40-02, HFEC CUT-OUT AND HOLES IAW NTM 51-00- 01, NO CRACKS NOTED, FABRICATED REPAIR DOUBLER IAW SRM 53-00-01 FIGMar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201103231148Skin · dentedLT MAIN FLAP, LOWER SURFACE, DENTED. REPAIRED LT MAIN FLAP LOWER SURFACE IAW SRM 51-70-10. FINAL REPAIR DIMENSION IS APPAROX 6" IN DIAMETER. REPAIR IS LOCATED APPROX 18" OTBD OF FLAP TRACK FAIRING. MAJOR REPAIR.Mar 23, 2011 · N997FD · Boeing 757200 · Trailing Edge FlapsSDR FDEA201103231146Skin · damagedNR 1 CARGO DOOR, LOWER CUTOUT, FUSELAGE SKIN BEND DAMAGE AT BS 605, 7" LONG BY 2" WIDE. (CLASSIFIED MINOR REPAIR).Mar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201103231145Skin · damagedNR 1 CARGO DOOR, LOWER CUTOUT, FUSELAGE BEND DAMAGE AT BS 580, 8" LONG BY 2" WIDE. COMPLIED WITH EA F-5330-146253. CLASSIFIED MAJOR REPAIR.Mar 23, 2011 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201103181074Stringer · dentedSTA 1661, STR 5L HAS A DENT CAUSE BY A REPAIR FASTENER. FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-03, FIG 101, DETAIL II. PG 102. ORIGINAL MATERIAL THICKNESS IS .100", REMAINING MATERIAL THICKNESS IS .070", MATERIAL REMOVED IS .030", W=400, L=500, DEPTH= .Mar 18, 2011 · N997FD · Boeing 757200 · Fuselage Main, Longeron/StringerSDR FDEA201103100936Intercostal · misalignedSECTION 44, FROM STA 1160-1180 BL0 UNABLE TO INSTALL PN 144N8006-211 INTERCOSTAL DUE TO EXISTING FASTNER HOLE 3EA LOCATIONS COMMON TO SKIN PANEL IF DRILLED WILL HAVE SHORT ED .385 IN THE INTERCOSTAL FIG "A" SECTION 44 FROM STA 1160-1180 BL0 PN 144N8006-211Mar 10, 2011 · N997FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA201103100937Skin · damagedPREVIOUS OPERATORS MULTIPLE FUSELAGE SKIN BLENDS, FOUND OUT OF LIMITS. REPAIRED PER SRM 53-00-01, REPAIR 16, CAT. "B" MAJOR REPAIR.Mar 10, 2011 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201103100928Skin · tornDOOR 4L INNER SKIN MID FWD LIGHTENING HOLE CUT-OUT IS TORN. COMPLIED WITH EA F-5210-146224, CAT. "A" MAJOR REPAIR AND FAA FORM 8100-9 DATED 12\23 \2010. (L4 DOOR INNER SKIN REPAIR, P/N: 146N6100-3, S/N: 226 FOR DOOR ASSY).Mar 10, 2011 · N997FD · Boeing 757200 · Passenger/Crew DoorsSDR FDEA201102240728Skin · dentedRT SIDE EXTERNAL FUSELAGE : STA 1710 BETWEEN STR, S 22&23- DENTED, JUST BELOW PREVIOUS REPAIR.Feb 24, 2011 · N997FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201102230698Fitting · unknownCOMPLY WITH EA F-2900-146376 , HYD POWER- ENGINE STRUT FIREWALL HYD PRESS FITTING REPLACEMENT. (SB 757-29-0041).Feb 23, 2011 · N997FD · Boeing 757200 · Hydraulic System, MainSDR FDEA201102220695Skin · gougedLT WING, INBD FLAP, LOWER SKIN, BEHIND GEAR GOUGED/ DENTED. REPAIRED LT WING INBD FLAP, LOWER SKIN IAW SRM 51-70-10 REPAIR IS LOCATED APPROX 5'' INBD OF FLAP TRACK FAIRING AND APPROX 6'' AFT OF L/E , FINAL REPAIR DIMENSION IS 5'' IN DIAMETER. FLAP PN 113N2003Feb 22, 2011 · N997FD · Boeing 757200 · Trailing Edge FlapsSDR FDEA201102220694Skin · delaminatedLT WING, INBD LOWER FLAP, LOWER SKIN OTBD OF CTR TRACK DELAMIATION. REPAIRED LT WING INBD LOWER FLAP, LOWER SKIN IAW SRM 51-70-17. REPAIR IS APPROX 2" OTBD OF FLAP TRACK FAIRING, AND 18" FWD OF T/E, FINAL REPAIR DIMENSION WAS 3.0" IN DIAMETER. FLAP PN : 11Feb 22, 2011 · N997FD · Boeing 757200 · Trailing Edge FlapsSDR FDEA201102050478Stringer · corrodedAFT PIT, RT-STA 1195 AT STR 22R- SPOT ON STRINGER, EXFOILATED CORROSION. REMOVED CORROSION PER SRM 51-10-02. MEASURED OUT OF LIMITS ; BEFORE: .056, AFTER: .000, LOSS" .056. DEPTH OF CLEAN UP EXCEEDS .025. REPAIRED STRINGER PER SRM 53-00-03, REPAIR NR 2,Feb 5, 2011 · N997FD · Boeing 757200 · Fuselage Main, Longeron/StringerSDR FDEA201102050479Frame · gougedFRAME GOUGED AT STA 239 RBL 11 TO 20. REMOVED GOUGES IAW SRM 51-10-02. MEASURED OUT OF LIMITS. FRAME FOUND DENT, DENT NOT ALLOWED FIG 101 PG 101 IAW SRM 53-00-07. RECEIVED FRAME ON TRAVLER T11/867390. INSTALLED FOM PAST REMOVED FOR ACCESS IAW SRM 51-40-02Feb 5, 2011 · N997FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201102050480Skin · crackedRT WING NR 10 SLAT, NR 19 ATTACH FITTING, POSSIBLE CRACK AROUND FASTENER, UNDER PAINT. UPON FURTHER INVESTIGATION, NDT VERIFIED A NO CRACK CONDITION EXISTS ON NR19 ATTACH FITTING, CRACK IS IN COVE SKIN, FROM OSS 736-748 ONLY. FOUND TO BE OUT OF LIMITS IAW SRFeb 5, 2011 · N997FD · Boeing 757200 · Leading Edge DevicesSDR FDEA201102030464Frame · misalignedSTA 540, INST. INBD AT THE STR CLIP AT STR 25 LT UNABLE TO LOCATE AND DRILL FASTENER HOLE FOR A YYT 8 FASTENER AND MAINTAIN PROPER E.D. ON THE DSS LOWER 540 FRAME, THIS CONDITION ALSO EXIST AT STA. 560, 520, 580 AND 600. STA 520, 540, 560, 580, 600. JUST INBDFeb 3, 2011 · N997FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201102020452Skin · crackedRT WING NR9 SLAT, OTBD IDLER ATTACHMENT HARDWARE APPEARS TO HAVE CRACKS COMING FROM FASTENER. COVE SKIN AT ISS 615 TO ISS 663, CRACKED AND FOUND TO BE OUT OF LIMITS, IAW SRM 57-43- 01, FIG 101, DETAIL II, PG 102. REMOVED AND REPLACED COVE SKIN AT ISS 615 TO Feb 2, 2011 · N997FD · Boeing 757231 · Leading Edge DevicesSDR FDEA201101300419Fitting · gougedNACELLE STRUT NR 2 AFT BULKHEAD STA 201.02 INBD AND OUTBD LOWER SIDES SURFACE HAS A GOUGE. REPAIR DISPOSITION WAS REJECTED. REFERENCE "REWORK" NON-ROUTINE N01498. W/O 00049340, FOR CORRECTIVE ACTIONS.Jan 30, 2011 · N997FD · Boeing 757200 · Nacelle/Pylon, Attach FittingsSDR FDEA201101270389Firewall · gougedAPU COMPARTMENT, FIREWALL JUST ABOVE RT DOOR LATCH BRACKET GOUGE IN FIREWALL. GOUGE ON FIREWALL APU WEB FOUND OUT OF LIMITS ORIG. MAT. .016" LOSS .012" REMAINING .004" AS PER SRM 53-80-08 DET. IX FIG 101 P. 109. FABRICATED DOUBLER AS PER SRM 53-80-08 TABLEJan 27, 2011 · N997FD · Boeing 757231 · APU Cowling/ContainmentSDR FDEA201101270390Skin · corrodedLT WING LWR SURFACE, WS 177.50, STRINGER L-6 TO L-8, 3 EA SPOTS OF CORROSION. COMPLIED WITH/ACCOMPLISHED REPAIR ON EA F-5730-143248 MAJOR REPAIR.Jan 27, 2011 · N997FD · Boeing 757200 · Wing, Plate/SkinSDR FDEA201101190285Cusp Web · damagedSTA 1140 TO 1160, CUSP WEB HAS INCOMING DOUBLE DRILLED FASTNER HOLE.Jan 19, 2011 · N997FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA201101180277Skin · dentedEXTERNAL FUSELAGE SKIN STA 1520-1540 BETWEEN STR 22R TO STR 23R HAS DENT. FOUND OUT LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. CUT-OUT DAMAGE AREA 1.100" LONG X 0.800" WIDE AT STA 1522 BETWEEN STR 22R- STR 23R IAW SRM 53-00-01 REPAIR 16. PERFORMED SURFACJan 18, 2011 · N997FD · Boeing 757231 · Fuselage Main, Plate/Skin
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