N992FD

Service difficulty reports · 113

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 = 'N992FD' 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 FDEA201109203978Skin · misrepairedFUSELAGE SKIN REPAIR AT BS 1640-1661, STR 20L, LAP SEAM MISREPAIRED. ACCOMPLISHED IAW-EA F-5330-152637, REF FAA FORM 8100-9, FIRST STAGE APPROVAL, DTA DUE WITHIN 24 MONTHS, "CAT A, MAJOR REPAIR".Sep 20, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201109193965Gate · corrodedL1 DOOR LOWER GATE BOTTOM EDGE IS CORRODED. REMOVED AND REPLACED LOWER GATE ON L1 DOOR, IAW-A.M.M-52-11-38, ADJUSTED DOOR ,IAW-AMM 52-11-00-5, OPS CHECKED GOOD. FOUND TO BE OUT OF LIMITS IAW SRM-52-10-02. CAT.A, MAJOR REPAIR.Sep 19, 2011 · N992FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201109143875Structure · corrodedCORROSION AT STA 425 STR 30 AT TOILET DUMP VALVE, INSIDE E/E BAY. DOT # 82149.Sep 14, 2011 · N992FD · Boeing 757232 · Fuselage Main, StructureSDR FDEA201109093825Skin · misrepairedSKIN REPAIR AT BS 1460-1480 BL 0, REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. REPLACED REPAIR IAW EA F-5330-147734, MAJOR REPAIR.Sep 9, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201108313600Gate · corrodedR-4 DOOR UPPER GATE UPPER EDGE HAS CORROSION. R & R R4 DOOR UPPER GATE ASSY IAW AMM 52-11-38. PERFORMED R4 DOOR ADJUSTMENT CHECK IAW AMM 52-11-00. CHECKED GOOD. ORIGINAL MATERIAL: .200", REMOVED: .050", REMAINING: .150", CORROSION FOUND OUT OF LIMITS IAAug 31, 2011 · N992FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201108303579Frame Splice · damagedFWD PIT,BS 760 S-27L, FRAME SPLICE BOTTOM FASTENER MISDRILLED. ACCOMPLISHED REPAIR IAW EA F-5310-147727. MAJOR REPAIR.Aug 30, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201108303581Gate · corrodedDOOR LOWER GATE BOTTOM EDGE FWD AND AFT CORNER ARE CHAFED. REMOVED CORROSION PER SRM 51-10-02. BEFORE: 0200", AFTER: .150", LOSS: .050", FOUND TO BE OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4. REMOVED AND REPLACED L4 DOOR LWR GATE ASSY PER AMM 52-Aug 30, 2011 · N992FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201108303580Gate · corrodedDOOR LOWER GATE BOTTOM EDGE CORRODED. REMOVED CORROSION PER SRM 51-10-02. ORIGINAL MATERIAL: .200", REMOVED: .015", REMAINING: .185", FOUND TO BE OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4. REMOVED AND REPLACED L2 LOWER GATE ASSY PER AMM 52-11-38Aug 30, 2011 · N992FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201108293567Gate · corrodedR2 DOOR LOWER GATE HAS CORROSION ON THE BOTTOM EDGE. FOUND OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4; EXCEEDS .100" FROM EDGE. REMOVED AND REPLACED R2 DOOR LOWER GATE ASSY PER AMM 52-11-38. PERFORMED R2 DOOR ADJUSTMENT CHECK PER AMM 52-11-00-5. ADJUSAug 29, 2011 · N992FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201108243459Frame Splice · misrepairedFRAME SPLICE REPAIR AT BS 720, S29L- S29R, REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. FRAME SPLICE REPAIR REPLACED IAW EA F-5310-147720. MAJOR REPAIR.Aug 24, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201108023428Stringer · corrodedSTRINGER 29R AT BS 1462, CORRODED. REMOVED AND REPLACED CORRODED STRINGER SECTION IAW SRM 53-00-03 REPAIR 2. MAJOR REPAIR.Aug 2, 2011 · N992FD · Boeing 757232 · Fuselage Main, Longeron/StringerSDR FDEA201108023386Gate · corrodedR1 DOOR LOWER GATE BOTTOM EDGE IS CORRODED. REMOVED CORROSION; ORIGINAL MATERIAL WAS: .200", REMAINING MATERIAL: .170", LOSS: .030". FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL 4. R & R R1 DOOR LOWER GATE ASSY IAW SRM 51-40-02, SRM 52-11-38,Aug 2, 2011 · N992FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201108023258Skin · misrepairedREPAIR DOUBLER ON R-4 SERVICE DOOR SKIN NOT REPAIRED IAW APPROVED DATA. R & R DOUBLER AND FILLER, IAW SRM 52-10-01, REPAIR NR 7, AND SRM 51-40-02. CAT. "B" MAJOR REPAIR.Aug 2, 2011 · N992FD · Boeing 757232 · Passenger/Crew DoorsSDR FDEA201108023194Skin · misrepairedFUSELAGE SKIN REPAIR DOUBLER AT STA 400, STR 14L-16L NOT IAW APPROVED DATA. R & R DOUBLER IAW SRM 51-40-02 & SRM 53-00-01. REPAIR 16, FABRICATED NEW DOUBLER.Aug 2, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201107262979Skin · damagedFOUND SCRIBE LINE AT BS 663.438 THROUGH BS 671.750 & S-19L LAP JOINT. COMPLIED WITH EX F-5330-147698, AD2007-19-07, & EO F-5330-7-5000, MAJOR REPAIR.Jul 26, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201107212884Skin · damagedFOUND SCRIBE LINE AT BS 759.531 TO BS 765.375, AT S14R LAP JOINT. ACCOMPLISHED EA F-5330-147702, PART 1 ONLY; VERIFICATION OF NO ADDITIONAL SCRIBE LINES AT BUTT JOINT, BS 720 TO BUTT JOINT, BS 781. PART 2 OF EA REQUIRED AT 1,500 FC AFTER PART 1 AND PART 3 OFJul 21, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201107142692Skin · gougedLT NACELLE STRUT RT SIDE NAC STA 100 FWD FAIRING UNDERNEATH SKIRT PANEL HAS DEEP GOUGE. COMPLIED WITH EA F-5450-147713. MAJOR REPAIR.Jul 14, 2011 · N992FD · Boeing 757232 · Nacelle/Pylon, Plate/SkinSDR FDEA201106232529Seat Track · out of alignmentSTA 640 LBL 24.75 SEAT TRACK WILL NOT JIG. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 610-640, LBL 24.75 IAW SRM 53-00-52, FIG 201, ITEM 2. RECEIVED NEW SEAT TRACK MAT BAC 1502-792 BATCH NR 001904663 IAW SRM 53-00-52, PG 203, FIG 201, SHT 3 OF 5. LOCATED ANDJun 23, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106232403Seat Track · out of toleranceSTA 640, RBL 24.75 SEAT TRACK WILL NOT JIG. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52 FIG 201 ITEM 2. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. APPLIED TOP COAT IAW SRM 51-20-00. INSTALLED SEAT TRJun 23, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106232585Unknown · corrodedFWD CARGO COMPT STA 750, STR 21R EXFOLIATED.Jun 23, 2011 · N992FD · Boeing 757232 · Fuselage Miscellaneous StructureSDR FDEA201106202386Frame · misrepairedFRAME SPLICE REPAIR AT STA 1300 STR 25R TO 26R REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APROVED DATA. REMOVED AND REPLACED FRAME IAW SRM-51-40-02, NEW FRAME FABRICATED AND INSTALLED NEW SPLICE ON FRAME IAW SRM-51-40-02. SPLICE FABRICATED. MAJOR REPJun 20, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106202346Frame · misrepairedFRAME AT STA 1340, STR 24R-26R MISREPAIRED. REMOVED AND REPLACED FRAME SPLICE IAW SRM 51-40-02 AND DWG.146N1042. MAJOR REPAIR.Jun 20, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106202389Frame · corrodedAFT CARGO PIT STA 1460, BL0 CORROSION ON FRAME. REMOVED FRAME BS 1460, S24L-S24R AND FOUND TO BE OUT OF LIMITS AT BL0' BEFORE: .063", AFTER: .053", LOSS: .010", AS PER SRM 53-00-07, DETAIL 2, FIG.101. REPLACED FRAME AND SPLICE AS PER SRM 51-40-02. MAJOJun 20, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106182333Frame · misrepairedEXISTING FRAME SPLICE REPAIR AT BS 1500, STR 24L-27L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. REMOVED AND REPLACED FRAME BS 1500 STR. 24L-24R, AS PER SRM 51-40-02 & DWG 146N1030. MAJOR REPAIR.Jun 18, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106182332Frame · misrepairedFRAME SPLICE REPAIR AT STA 1420, STR 24L-26L REQUIRES REPLACEMENT DUE NOT COMPLYING WITH APPROVED DATA. REMOVED FRAME AND PRODUCTION SPLICE PER SRM 51-40-02. FABRICATED FRAME AND SPLICE. INSTALLED NEW FRAME AND SPLICE PER SRM 51-40-02 AND DRAWING 146N1028. Jun 18, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106182331Frame · misrepairedFRAME SPLICE AT STA 1520, STR 23L-25L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R SPLICE, AND R & R FRAME, IAW SRM 51-40-02 AND SRM 51-10-02. MAJOR REPAIR.Jun 18, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106172321Frame · misrepairedFRAME SPLICE REPAIR AT STATION 1320, STR 23L-26L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R FRAME, AT STA 1320, STR. 24L TO STR 24R, IAW SRM-51-40-02. NEW FRAME FABRICATED AND INSTALLED. NEW SPLICE IAW-SRM-51-40-02, SPLICE FABRICATEJun 17, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106142239Skin · misrepairedEXISTING FUSELAGE SKIN EXTERNAL DOUBLER REPAIR AT STA 1710, STR 24L REQUIRES REPLACEMENT DUE TO NOT BEING IN COMPLIANCE WITH KNOWN APPROVED DATA. REMOVED EXISTING DOUBLER, CUT-OUT DAMAGE SKIN AND INSTALLED NEW DOUBLER/ FILLER, BS 1708-1718, S23L-S24L, IAWJun 14, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201106092301Frame · misrepairedFRAME SPLICE AT STA 1480, STR 23L- 26L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R FRAME STA 1480 FROM STR.24L-24R IAW SRM-51-40-02, AND SPLICE. "CAT A, MAJOR REPAIR".Jun 9, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106092299Frame · misrepairedFRAME SPLICE REPAIR AT STA 1440, STR 23L-26L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. REMOVED AND REPLACED FRAME AND SPLICE, BS 1440, S29R - S24L, PER SRM 51-40-02, AND DRAWING 146N1028.Jun 9, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201106092240Skin · misrepairedEXISTING EXTERNAL FUSELAGE REPAIR AT STA 1700-1720, STR 16L REQUIRES REPLACEMENT DUE TO NOT COMPLING WITH APPROVED DATA. REMOVED AND REPLACED DOUBLER PER SRM 53-00-01, REPAIR 15. MAJOR REPAIR, CAT. "B" .Jun 9, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201106092279Support Angle · corrodedL-2 DOOR SILL DRAIN PAN SUPPORT ANGLE HAS CORROSION APPROX BETWEEN STA 680 TO 730. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS; L=4", W=2", D=.071, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-13, FIG 101, DETAIL 2. REMOVED SUPPORT ANGLE IAW SRM 51-40-0Jun 9, 2011 · N992FD · Boeing 757232 · Fuselage Miscellaneous StructureSDR FDEA201106092245Skin · dentedBS 1711 S15R HAS A DENT IN SKIN. REMOVED DAMAGED SKIN IAW SRM 53-00-01, FABRICATED DOUBLER IAW SRM 53-00-01, TABLE I. REPAIR 16. HFEC CHECK CUT-OUT, HOLES IAW NDTM 51-00-19, NO CRACKS NOTED. INSTALLED DOUBLER IAW SRM 51-40-02, CATEGORY "B" MAJOR REPAIR.Jun 9, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201106092241Skin · misrepairedEXISTING EXTERNAL FUSELAGE SKIN REPAIR AT STA 1681, STR 2L-3L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R REPAIR DOUBLER IAW SRM 53-00-01, REPAIR NR 15, MAJOR REPAIR, CAT "B", AT BS 1681, S2L- S3L.Jun 9, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201106092189Angle · corrodedRIGHT SIDE WALL ANGLE BS 740, S24-27R CORRODED.Jun 9, 2011 · N992FD · Boeing 757232 · Fuselage Miscellaneous StructureSDR FDEA201106092185Frame · crackedRT ENG PYLON OTBD SIDE STA 193 FRAME CRACKED. REMOVED SUPPORT CLAMPS 4 EA HYDR LINES 3 EA TO BE FOM IAW AMM 20-10-09. FABRICATED NEW SUPPORT ANGLE FRAME ON TRAVELER. LOCATED AND DRILLED NEW SUPPORT ANGLE AND INSTALLED IAW SRM SRM 51-40-05 AND 51-40-02 INJun 9, 2011 · N992FD · Boeing 757232 · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201106092180Attach Angle · gougedFWD PIT RT SIDE WALL ATTACH ANGLE AT FRAME 640 S25R- S26R CORRODED AND GOUGED. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS OF SIDE WALL ANGLE AT FS 640 S25R-S26R. MATERIAL THICKNESS .050 REMOVED MAT .015 REMANING MAT .035 FOUND TO BE OUT OF LIMITS IJun 9, 2011 · N992FD · Boeing 757232 · Fuselage Main, Attach FittingsSDR FDEA201106092168Crease Beam · gougedRT CREASE BEAM INBD CHORD, STA 1180-1400 GOUGED AT AND AROUND NUMEROUS FASTENER HOLES EVALUATED DAMAGES ON CREASEBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13, FIG 101, SH 3, DETAIL 2 ( L= .5 W=.1 D=.015) ORIG .080 DAMAGED AREA .065 REMOVED CREASEBEAM RT Jun 9, 2011 · N992FD · Boeing 757232 · Fuselage Main, StructureSDR FDEA201106082151Seat Track · gougedRBL 45, SEAT TRACK, DIRTY AND GOUGED AT NUMEROUS SPOTS STA 1180 TO 1320. REMOVED CORROSION AND GOUGES IAW SRM 51-10-02 CHECKED LIMITS OF SEAT TRACK AT RBL 45, FS 1180-FS 1320 MATERIAL THICKNESS .230 REMOVED MAT .051 REMAINING MAT .179, FOUND TO BE OUT OF LJun 8, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106072145Skin · dentedDENT STA 1700 S23R RT SIDE SKIN. FOUND OUT OF LIMITS IAW SRM 53-00-01, PG 101, DET III. CUT-OUT DAMAGED SKIN. INSTALLED DOUBLER, FILLER IAW SRM 51-40-02 AND SRM 53-00-01 ZONE A,CAT B REPAIR. MAJOR REPAIR.Jun 7, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201106062136Floorbeam · noneFLOORBEAM STA 680 REQUIRES REPLACEMENT DUE TO INCOMING REPAIRS THAT WILL INTERFERE WITH SEAT TRACK INSTALL. REMOVED FLOORBEAM STA 680 IAW SRM 51-40-02. REMOVED BRACKETS STA 680 RBL 17-62 (4EA) AND LBL 24-62 (2EA) PER SRM 51-40-02. RECEIVED EXTRUSION PN BAJun 6, 2011 · N992FD · Boeing 757232 · Fuselage Main, Floor BeamSDR FDEA201106042118Seat Track · gougedMAIN DECK SEAT TRACK HAS NUMEROUS GOUGES AT RBL 24 BETWEEN BS 760 TO BS 785. REMOVED GOUGE IAW SRM 51-10-02 MEASURED OUT OF LIMITS ORIGINAL .300 REM .250 LOSS .050 DETAIL 1 FIG 101 PAGE 103 IAW SRM 53-00-52. FABRICATED SEAT TRACK IAW SRM 53-30-52. REMOVEJun 4, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106032106Skin · dentedDENT ON SKIN STA 521, STR 24R. REMOVED DAMAGE AND FOUND OUT OF LIMITS PER SRM 53-00-01, DETAIL 3, FIG.101. FABRICATED DOUBLER AND FILLER AS PER SRM 53-00-01, TABLE 1, P.203, FIG.201, REPAIR 15. HFEC CHECKED CUTOUT AND HOLES WITH NO CRACKS NOTED. INSTALLED DJun 3, 2011 · N992FD · Boeing 757232 · Fuselage Main, Plate/SkinSDR FDEA201106012079Stringer · crackedCHECKED LIMITS AND FOUND STRINGER CRACKED, OUT OF LIMITS IAW SRM 53-00-03, REPAIR 2, PG 102, FIG 101, DETAIL 1. R & R STRINGER IAW SRM 53-00-03, REPAIR 2. MAJOR REPAIRJun 1, 2011 · N992FD · Boeing 757232 · Fuselage Main, Longeron/StringerSDR FDEA201105312035Seat Track · wornMAIN CABIN SEAT TRACK BS 1090-1110 RBL 25 IS WORN. BLENDED WORN AREA WITH .032". REMOVED FROM TOP SURFACE. MAX ALLOWED IS .020". AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, SH 2, P 102. R & R SEAT TRACK IAW SRM 51-40-02, 51-20-01, 51-40-05May 31, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105282019Firewall · gougedAPU COMPARTMENT, FWD FIREWALL HAS GOUGES, 8" FROM BOTTOM EDGE OF WALL. FOUND GOUGE TO BE .003" DEEP, DETERMINED TO BE OUT OF LIMIT IAW SRM 53-80-01, FIG 101 DET IX PG 109, REPAIRED DAMAGE PER SRM 53-80-08, FIG 201, SHEET 1 PG 201. MAJOR REPAIR.May 28, 2011 · N992FD · Boeing 757232 · APU Cowling/ContainmentSDR FDEA201105251988Firewall · chafedAPU COMPARTMENT FWD FIRE WALL HAS CHAFING MARKS 20" FROM BOTTOM EDGE OF COMPARTMENT. CHAFE MARK FOUND TO .004" DEEP, DETERMINED TO BE OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL IX PG 109. REPAIRED DAMAGE IAW SRM 53-80-08, FIG 201, SHEET 1, PG 201, STA 18May 25, 2011 · N992FD · Boeing 757232 · APU Cowling/ContainmentSDR FDEA201105241960Floorbeam · gougedFLOORBEAM AT STA 1600 HAS NUMEROUS GOUGES BETWEEN RBL 60 TO LBL 60. REMOVED AND REPLACED FLOORBEAM, FOUND TO BE OUT OF LIMITS PER SRM 53-00-51 FIG.101 DETAIL 3. LOCATED AND DRILLED FASTENER HOLES IN NEW FLOORBEAM PER SRM 51-40-02. APPLIED TOP COAT PER SRM 51May 24, 2011 · N992FD · Boeing 757232 · Fuselage Main, Floor BeamSDR FDEA201105241968Seat Track · corrodedMAIN DECK STA 1155, RBL 45 SEAT TRACK CORRODED. REMOVED CORROSION WITH .070" MATERIAL LOSS. MAX ALLOWED IS .040". AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 4. R & R TRACK IAW SRM 51-40-01, 51-40-05, 51-40- 02. MAJOR REPAIR.May 24, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105241967Seat Track · corrodedMAIN DECK STA 1140, RBL 45 SEAT TRACK CORRODED.May 24, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
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