N998FD

Service difficulty reports · 106

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 = 'N998FD' 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 FDEA201411183880Closeout Panel · crackedMCD LOWER FWD CLOSE OUT PANEL CRACKED. REMOVED MCD LOWER CLOSE OUT PANEL IAW SRM 51-40-02. FABRICATED NEW PANEL IAW DWG 65-49309 REV D. INSTALLED NEW PANEL IAW SRM 51-40-02 & DWG 65-49309 REV D.Nov 18, 2014 · N998FD · Boeing 757230 · Cargo/Baggage DoorsSDR FDEA201410243376Module · miswiredDURING SVC CHECK FOUND COCKPIT EMER LIGHT INOPERATIVE. RELAMPED NO HELP. TROUBLE SHOT IAW WDM 33-51-12. FOUND NO GND PRESENT AT LIGHT ASSEMBLY. LOCATED GND LOCK GD602-DC IN OVERHEAD PANEL BETWEEN CB PANELS P 11 - 1 & P 11 - 2. HUD OHU WILL HAVE TO BE REMOOct 24, 2014 · N998FD · Boeing 757230 · Light System WiringSDR FDEA201407081655Battery Pack · dischargedRIGHT EMER EXIT SIGN M730 WILL NOT ILLUMINATE DURING TEST. R & R BATTERY PACK IAW MM 33-51-07-2-2. OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE.Jul 8, 2014 · N998FD · Boeing 757230 · Emergency LightingSDR FDEA201212084269Skin · puncturedNR 3 SLAT L/E LOWER SIDE PUNCTURED 2 FT FROM INBD EDGE. FOUND DAMAGE TO BE OUT OF LIMITS PER SRM 57-43-01 FIG 101. REPAIRED IAW SRM 57-43-01 FIG 201 REPAOR 1. CATEGORY A MAJOR REPAIR.Dec 8, 2012 · N998FD · Boeing 757230 · Leading Edge DevicesSDR FDEA201212054247Skin · corrodedNR 10 SLAT HAS SPOT AREAS OF CORROSIONS ON THE T/E WEDGE UPPER SURFACE. REPAIRED NR 10 SLAT T/E WEDGE UPPER SURFACE IAW-SRM-51-70-10, REP NR 2.Dec 5, 2012 · N998FD · Boeing 757230 · Leading Edge DevicesSDR FDEA201212034233Frame · chafedBS 418.00 FRAME HAS DEEP CHAFE, BETWEEN S20-21R. ACCOMPLISHED EA F-5310-162460. REMOVED CHAFE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101. MAJOR REPAIR.Dec 3, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211294205Skin · dentedRT WING, INBD FLAP UPPER SURFACE, OTBD OF WS 313, HAS A DENT. REPAIRED FLAP UPPER SURFACE IAW-SRM-51-70-10, CAT."A" MAJOR REPAIR,Nov 29, 2012 · N998FD · Boeing 757230 · Trailing Edge FlapsSDR FDEA201211264184Skin · dentedBETWEEN BS 520 & 540 AT STR 26 & 27L, A DENT IN FUSELAGE SKIN. REPAIRED IAW EA 757-5331-16-F3986, REV -.Nov 26, 2012 · N998FD · Boeing 757230 · Fuselage Main, Plate/SkinSDR FDEA201211234137Beam · crackedR-4 DOOR INNER SKIN, EDGE OF LIGHTING HOLE, NR 4 BEAM, CRACKED. REPAIRED IAW EA F-5210-162564. MAJOR REPAIR.Nov 23, 2012 · N998FD · Boeing 757230 · Service DoorsSDR FDEA201211134003Rib · corrodedRT WING AFT SPAR AT WSTA 815 BONDING JUMPER ATTACHMENT TO RIB CORRODED. REMOVED CORROSION AT GROUNDING POINT. FOUND TO BE OUT OF LIMITS IAW SRM 57-51-09, FIG 101 DET VI. RIB FABRICATED & INSTALLED IAW DWG 113N1511. MAJOR REPAIR.Nov 13, 2012 · N998FD · Boeing 757230 · Wing, Rib/BulkheadSDR FDEA201211123982Frame · crackedFRAME BS 760 S9L RIVET HAS SET MARK AND AT STRINGER 10L-11L THERE IS A TRAPPED HOLE. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3. MAJOR REPAIR.Nov 12, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211093925Wedge · damagedNR 4 SLAT WEDGE EDGE, CHIPPED OFF, .5" X .0625", WS 344.0. REPAIRED NR 4 SLAT WEDGE EDGE IAW SRM 51-70-10, REPAIR NR 4. MAJOR REPAIR.Nov 9, 2012 · N998FD · Boeing 757230 · Leading Edge DevicesSDR FDEA201211063889Frame · corrodedFWD CARGO LT SIDE AT BS 760 BETWEEN STR 23-25L CORROSION ON FRAME. REMOVED CORROSION ON FRAME BETWEEN STR 23 & STR 25 AT STA 760 LT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. REMOVED FRAME AT STA 760 LT STR 13 TO STR 26. REPLACED FRAMNov 6, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211063885Bulkhead · chafedLEFT STRUT BULKHEAD, LT LWR SIDE, CHAFED ACCOMPLISHED IAW EA F-5450-162447, FOUND OUT OF LIMITS IAW SRM 54-51-02 FIG 101 DET VII.THIS IS A CATEGORY A, MAJOR REPAIR.Nov 6, 2012 · N998FD · Boeing 757230 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201211043827Frame · damagedFRAME BS 1620, S5L TO S5R HAS DOUBLE DRILLED AND ELONGATED FASTENER HOLES. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, SHEET 2, DETAIL 1, REPAIR 3. MAJOR REPAIR.Nov 4, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211043826Frame · damagedBS 418, FRAME BETWEEN STR 5L AND STR 4R DAMAGED. FRAME REPAIRED IAW EA 757-5312-16-F3926, REV, MAJOR REPAIR.Nov 4, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211043825Frame · damagedFRAME STA 1560, BETWEEN S5L AND S5R HAS DOUBLE DRILLED AND ELONGATED FASTENER HOLES. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3. MAJOR REPAIR.Nov 4, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211043824Frame · damagedFRAME BS 1540, S3R -S6L, HAS DOUBLE DRILLED AND ELONGATED FASTENER HOLES. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3. MAJOR REPAIR.Nov 4, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211043823Frame · damagedFRAME BS 1520 BETWEEN S4L-S4R HAS DOUBLE DRILLED AND ELONGATED FASTENER HOLES AT BS 1520, FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3.Nov 4, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211043822Frame · damagedFRAME BS 1260 S4L- 4R HAS DOUBLE DRILLED AND ELONGATED HOLES. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3.Nov 4, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201211023817Skin · corrodedLEFT WING UPPER SKIN UPPER SURFACE CORRODED. FOUND TO BE OUT OF LIMITS, WITHIN 1.5 IN. OF ANY CHORD WISE ROW OF FASTNERS IAW SRM 57-20-01, FIG 101, NOTE "A". THIS REPAIR IS A CATEGORY A , MAJOR REPAIR.Nov 2, 2012 · N998FD · Boeing 757230 · Wing, Plate/SkinSDR FDEA201210313790Frame · misrepairedFUSELAGE FRAME AT BS 760, STR 24-26R, MISREPAIRED. REPLACED FRAME PER DRAWING 143N1018. THIS REPAIR IS A CATEGORY A, MAJOR.Oct 31, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201210233724Floor Skin · corrodedDURING REMOVAL OF CAPTIAN'S RT SEAT TRACK FOUND AREA OF CORROSION BS 245 TO 255 LBL 17 REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.Oct 23, 2012 · N998FD · Boeing 757230 · Fuselage Floor PanelSDR FDEA201210233723Floor Skin · corrodedDURING REMOVAL OF CAPTAIN'S RT FOOT HEATER PANEL FOUND AREAS OF CORROSION BS 205 TO 231 LBL-15. REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.Oct 23, 2012 · N998FD · Boeing 757230 · Fuselage Floor PanelSDR FDEA201210233722Structure · corrodedDURING REMOVAL OF CAPTAINS LT FOOT HEATER PANEL FOUND AREAS OF CORROSION BS 205 TO 231, LBL-24. REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.Oct 23, 2012 · N998FD · Boeing 757230 · Fuselage Main, StructureSDR FDEA201210233721Floor Skin · corrodedCOCKPIT FLOOR SKIN AT BS 239-247, LBL30-40 CORRODED. REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.Oct 23, 2012 · N998FD · Boeing 757230 · Fuselage Floor PanelSDR FDEA201210233718Floor Skin · corrodedCOCKPIT FLOOR SKIN AT BS 239 - 247, RBL 34 HAS SCRATCHES AND CORROSION. REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.Oct 23, 2012 · N998FD · Boeing 757230 · Fuselage Floor PanelSDR FDEA201210233717Floor Skin · corrodedFLT DECK FLOOR SKIN FROM BS 225 TO 231, RBL 36 - 40, HAS CORROSION. REPAIRED AREA IAW EA 5310-162556. REPAIR IS CLASSIFIED AS A MAJOR.Oct 23, 2012 · N998FD · Boeing 757230 · Fuselage Floor PanelSDR FDEA201210233726Fitting · damagedRIGHT WING, SIDE LINK FITTING HOLE "H" FOUND TO BE OVERSIZED. REPAIRED IAW EA F5740-162444. MAJOR REPAIR.Oct 23, 2012 · N998FD · Boeing 757230 · Wing, Attach FittingsSDR FDEA201210193694Crease Beam · corrodedRT INBD CREASE BEAM CORRODED UPPER & LOWER SURFACE, BS 660-680. REMOVED CREASEBEAM BS 660-755, IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02. CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DET. III. REPLACED CREASE BEAM IAW SRM 51-Oct 19, 2012 · N998FD · Boeing 757230 · Fuselage Main, StructureSDR FDEA201210193693Cargo Track · corrodedMAIN DECK CARGO TRACK AT STA 680 -780, LBL 24 HAS GOUGES AND CORROSIONS. REMOVED CORROSION IAW SRM 51-10-02. CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG 101, PG 102. R & R CARGO TRACK AT LBL24.75 STA 680-780 IAW SRM 51-40-02 AND DWG 1Oct 19, 2012 · N998FD · Boeing 757230 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210113596Frame · damagedFRAME, BS 1520, BETWEEN STRINGERS 4L -4R, HAS SEVERAL ELONGATED AND DOUBLE DRILLED HOLES. REPAIR ACCOMPLISHED IAW SRM 53-00-07, FIG 201, REPAIR 3. MAJOR REPAIR.Oct 11, 2012 · N998FD · Boeing 757230 · Fuselage Main, FrameSDR FDEA201210013521Crease Beam · corrodedMAIN CABIN AREA BETWEEN BS 1600 -1640 CREASE BEAM CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 101 SH 3 DETAIL III. REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 146N5590. FABRICATED IAW BOEING DRAWING 146NOct 1, 2012 · N998FD · Boeing 757230 · Fuselage Main, StructureSDR FDEA201209293515Floorbeam · mismanufacturedMAIN DECK FLOORBEAM BS 660 CAME SHORT AT LT END TO PICK UP CREASE BEAM OTBD CHORD FASTENER HOLE. REMOVED SHORT FLOORBEAM IAW SRM 51-40-02 & DWG 143N5012 SH 19. FABRICATED NEW FLOORBEAM IAW DWG 146N5012, SH 19, INSTALLED NEW FLOORBEAM IAW SRM 51-40-02 & DWG 1Sep 29, 2012 · N998FD · Boeing 757230 · Fuselage Main, Floor BeamSDR FDEA201209213384Seat Track · chafedSEAT TRACK HAS CHAFE MARKS AND PAINT CHIPPED FROM BS 400 - 900, LBL 45. REMOVED CHAFE MARKS, MAX CLEAN UP DEPTH .040" ALLOWED. CHAFFED AT .060", OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL IV. FABRICATED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND DRAWISep 21, 2012 · N998FD · Boeing 757230 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209203372Bracket · corrodedLT WING AILERON OTBD BONDING WIRE ATTACHMENT, HINGE BRACKET RIB CORRODED. REMOVED AND REPLACED RIB ASSY, WS 817.27, IAW SRM 51-40-02 AND DWG 113N1501 DUE TO OUT OF LIMITS PER SRM 57-51-09, FIG 101, DETAIL IV. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.Sep 20, 2012 · N998FD · Boeing 757230 · Wing, Attach FittingsSDR FDEA201209203367Seat Track · corrodedRBL 25.0 SEAT TRACK CORRODED BS 630 - 640. REMOVED CORROSION, MAX CLEANUP DEPTH IN BOTTOM OF TRACK .040", REMOVED .090" OF MATERIAL, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, PAGE 102. REMOVED AND REPLACED SEAT TRACK, RBL 25, BS 440-640, PER DSep 20, 2012 · N998FD · Boeing 757230 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209193353Crease Beam · corrodedRT INB CREASE BEAM CORRODED AT BS 646-665. REMOVED DAMAGED CREASEBEAM AND FABRICATED AND INSTALLED NEW CREASEBEAM, IAW DRAWING 143N5520 AND SRM 51-40-02, RT I/B CREASEBEAM, BS 450-665. REMOVED CORROSION IAW SRM 53-30-13, FIG. 101, DETAIL III; ORIGINAL MATERIASep 19, 2012 · N998FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA201209173339Floorbeam · corrodedFLOORBEAM UPPER TEE CORRODED, BS 324, LBL 20. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-10-08 FIG 101 DETAIL IX. REMOVED AND REPLACED FLOORBEAM UPPER TEE IAW SRM 51-40-02 AND DRAWING 141N2930. REPAIR IS CLASSIFIED AS MAJOR.Sep 17, 2012 · N998FD · Boeing 757230 · Fuselage Main, Floor BeamSDR FDEA201209133311Seat Track · gougedMAIN CARGO DECK SEAT TRACK AT BS 1180-1320, LBL 24.75 HAS AREAS WITH GOUGES, CORROSION AND DAMAGED DOME NUTS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I SHEET 2 OF 6. FABRICATED NEW SEAT TRACK IAW SRM 53-60-52 FIG 1 SH 2 OF 5 AND DWG 146N51Sep 13, 2012 · N998FD · Boeing 757230 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209123297Crease Beam · corrodedMAIN CARGO DECK LEFT INBD CREASE BEAM AND ANGLE BS 665-690 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, DETAIL III. R & R LT INBD CREASEBEAM IAW SRM 51-40-02 AND DWG 143N8324. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.Sep 12, 2012 · N998FD · Boeing 757230 · Fuselage Main, StructureSDR FDEA201209073252Crease Beam · corrodedRT INBD CREASE BEAM CORRODED, BS 774. FOUND TO BE OUT OF LIMITS AT BS 774 RBL 70 IAW SRM 53-30-13 DETAIL VIII FIG.101 PG.105. REMOVED AND REPLACED CREASE BEAM AT BS 760-900 RBL 70 IAW SRM 51-40-02 AND DRAWING 143N5520.Sep 7, 2012 · N998FD · Boeing 757230 · Fuselage Main, StructureSDR FDEA201209063244Floorbeam · corrodedFLOORBEAM UPPER TEE CORRODED, BS 344, BL 0 - LBL 25. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS AFTER REWORK FOUND FLOORBEAM UPPER TEE OUT OF LIMITS IAW SRM 53-00-510 DETAIL III. R & R FLOORBEAM TEE IAW SRM 51-40-02, AND REPAIR 3 OF SRM 53-00-51. THSep 6, 2012 · N998FD · Boeing 757230 · Fuselage Main, Floor BeamSDR FDEA201209063243Floorbeam · corrodedFLOORBEAM UPPER TEE CORRODED, BS 344, BL 0 - LBL 25.Sep 6, 2012 · N998FD · Boeing 757230 · Fuselage Main, Floor BeamSDR FDEA201209053231Floorbeam · corrodedFLOORBEAM UPPER CHORD BS 365, RBL52, CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 SH 4 DETAIL III. REPAIRED FLOORBEAM LBL 15.5 TO RBL 70 IAW SRM 53-00-51 FIG 201 SH 1-6 REPAIR 3. MAJOR REPAIRSep 5, 2012 · N998FD · Boeing 757230 · Fuselage Main, Floor BeamSDR FDEA201209053232Stiffener · corrodedMAIN DECK CARGO FRAME STIFFENER AT BS 1600, STR 16L-17L, HAS CORROSION. REMOVED CORROSION, ORIGINIAL THICKNESS .100, REMAINING THICKNESS .080, MATERIAL LOST .020. FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101, SH3 DETAIL I AND II AND SRM 51-10-02. REMOVED DASep 5, 2012 · N998FD · Boeing 757230 · Fuselage Miscellaneous StructureSDR FDEA201209053227Seat Track · corrodedRBL 45.0, SEAT TRACK CORRODED BS 600 - 640. FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. REPLACED SEAT TRACK IAW SRM 51-40-02, DWG 143N5149 AND DWG 143N5080. REPAIR CLASSIFIED AS MAJOR.Sep 5, 2012 · N998FD · Boeing 757230 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209043224Floorbeam · corrodedFLOORBEAM UPPER TEE CORRODED BS 377.7, LBL 45 - 60. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. REPAIRED UPPER TEE FROM LBL 70 TO RBL 35.75, BS 377.7, IAW SRM 53-00-51, REPAIR 3. MAJOR REPAIRSep 4, 2012 · N998FD · Boeing 757230 · Fuselage Main, Floor BeamSDR FDEA201209043219Floorbeam · corrodedCABIN FLOORBEAM BS 1640 HAS CORROSION ON UPPER ANGLE. UPPER AND LOWER SURFACES FROM LBL 58 TO RBL 58. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG. 101, DETAIL III. REMOVED, FABRICATED AND INSTALLED NEW FLOORBEAM IAW SRM 51-40-02 AND DRAWING 146N5089. Sep 4, 2012 · N998FD · Boeing 757230 · Fuselage Main, Floor BeamSDR FDEA201208243153Crease Beam · corrodedLEFT INBD CREASE BEAM CORRODED BS 1045 - 1080. REMOVED CORROSION ORIG .080 REMAINING .005 FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13, DETAIL VIII. R & R CREASE BEAM IAW SRM 51-40-02, SRM 51-10-02 AND DWG REF 14N5200. MAJOR REPAIR.Aug 24, 2012 · N998FD · Boeing 757230 · Fuselage Main, Structure
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