N921FD

Service difficulty reports · 121

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 = 'N921FD' 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 FDEA201208042853Door · obstructedATTEMPTED TO CLOSE L1 DOOR, UNABLE DUE TO INTERFERENCE. SECURED L1 DOOR CORD IAW AMM 52-11-00-2 . CHECKED GOOD. ACFT OK FOR SERVICE.Aug 4, 2012 · N921FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201205231940Flap System · malfunctionedON FINAL APPROACH, ON SELECTING FLAPS TO 20, FLAPS STOPPED AT APPROXIMATELY 17. RECEIVED T/E FLAP DISAGREE ALERT. RAN QRH, LANDED WITH FLAPS 20. LANDING UNEVENTFUL. FLAP SYS RETURNED TO NORMAL. FLAPS CYCLED NUMEROUS TIMES. NO FAULTS COULD BE DUPLICATED. May 23, 2012 · N921FD · Boeing 75723A · Trailing Edge Flap Control SystemSDR FDEA201108223401Skin · dentedPROTRUDING DENT BS 1675 BETWEEN STRINGER'S 26L AND 27L. DENT OUT OF LIMITS IAW SRM 53-00-01. CUT OUT DAMAGED AREA IAW SRM 53-00-01, FIG 201. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-00-01, FIG 201.Aug 22, 2011 · N921FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR FDEA201107293028Bottle · dischargedWHEN OPENING L1 DOOR THE DOOR ASSIST BOTTLE DEPRESSURISED.Jul 29, 2011 · N921FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201107293027Bottle · dischargedWHEN OPENING L1 DOOR THE DOOR ASSIST BOTTLE DEPRESSURISED. REMOVED L1 DOOR RESERVOIR BOTTLE IAW MM 52-11-30-4. NEW RESERVOIR BOTTLE IS BAD FROM STOCK. NO SERVICABLE BOTTLES IN MEM NIS.Jul 29, 2011 · N921FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201107242926Bulb · inoperativeON SHORT FINAL, RT MAIN GEAR LIGHT WAS INOP, SHOWED UNSAFE. NO LIGHT IN GEAR HANDLE OR DISAGREE LIGHT. FLEW LOW APPROACH, HAD GEAR VISUALLY INSPECTED BY TOWER, RAN QRH, REPLACED 1 LIGHT BULB, GEAR LIGHT WORKED SHOWING SAFE GEAR, LANDED WITHOUT FURTHER IJul 24, 2011 · N921FD · Boeing 75723A · Landing Gear Position and WarningSDR FDEA201105111828Spring · brokenHUB TRAINING KNOCKED GIRT BAR OFF EMERGENCY SLIDE ON L1 DOOR AGAIN. "MEL 52-11-01-A: L1 DOOR SLIDE - MISSING (IDENTIFY INOP OR MISSING)." GIRT BAR WOULD NOT ENGAGE OPERATING MECHANISM CORRECTLY, LEAF SPRINGS IN GIRT BAR BROKEN. REMOVED LI DOOR SLIDE, INSTALLEMay 11, 2011 · N921FD · Boeing 75723A · Emergency EquipmentSDR FDEA201104271651Fseu · bindingT/E FLAP DISAGREE "T/E FLAP DISAGREE". EICAS MSG ILLUMINATED DURING APPROACH WHILE SELECTING FLAPS FROM 5 TO 20. T/E FLAPS STUCK AT APPROX 18. RAN QRH PROCEDURES WHICH DICTATED ALT FLAP OPERATION. FLAPS MOVED TO 20 WITH ALT MODE. FLAPS LT AT 20 FOR BLOCKINApr 27, 2011 · N921FD · Boeing 75723A · Trailing Edge Flap Control SystemSDR FDEA201002230497Door Frame · crackedR1 DOOR SEAL MATING SURFACE ON FUSELAGE TOP FWD CORNER DAMAGED TRIMMED OUT BS 325.10 FRAME OTBD CHORD, REMOVED CRACK, MAINTAINED .50 R . HFEC INSPECTED TRIM OUT, NO CRACKS NOTED PERFORMED ENSURANCE CUT , FORMED BACK REMAINING PORTION IAW BAC5300, HFEC INSPECTEFeb 23, 2010 · N921FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA201002030313Gate · corrodedDOOR R1 LOWER GATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 ON LOWER GATE. CHECKED LIMITS IAW SRM 52-10-02, FIG. 101, DETAIL 12, AND FOUND TO BE OUT OF LIMITS; ORIGINAL MATL. .200"/ MATL. REMAINING .030". REMOVED LOWER GATE IAW AMM 52-11-38. REMOVEFeb 3, 2010 · N921FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201001260266Gate · corrodedDOOR L-2 LOWER GATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02. REMOVED LOWER GATE IAW AMM 52-11-38. INSTALLED NEW LOWER GATE L-2 DOOR IAW AMM 52-11-38. ADJUSTMENT CHECK GOOD IAW AMM 52-11-00. CATEGORY "Jan 26, 2010 · N921FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201001200198Skin · dentedDENT AT STA 1230 BETWEEN STR 25 AND 26 LT FUSELAGE ( INB OUT WITH CREASE ) CHECKED LIMITS AND FOUND OUT OF LIMITS DUE TO CREASE. REMOVED DAMAGE IAW SRM 53-00-01.INSPECTED W/ NO CRACKS FOUND. FABRICATED DOUBLER FILLER IAW SRM 53-00-01, LOCATED AND DRILLED IAWJan 20, 2010 · N921FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR FDEA201001190183Spar · damagedLT HORZ STAB L/E DAMAGED. REPAIR WAS ACCOMPLISHED IAW MAE EA NR 757-5510-16 A1923. CLASSIFIED AS A, "INTERIM" REPAIR, MAJOR.Jan 19, 2010 · N921FD · Boeing 75723A · Horizontal Stabilizer, Spar/RibSDR FDEA201001070041Skin · corrodedFOUND DENTED AREA WITH LIGHTENING STRIKE IN THE CTR & SEVERAL PIN HOLE PITS SURROUNDING THE AREA AT S14R BS 1247.5 IN LAP SEAM AREA. LENGTH OF DAMAGE .156, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01. DRILLED OUT DAMAGE WITH A .159 DRILL BIT IAW SRM 53-00-01Jan 7, 2010 · N921FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR FDEA201001050013Support Bracket · corrodedR3 DOOR FWD HINGE SUPPORT BRACKET LWR SURFACE CORRODED STA 1326, RBL 60. REMOVED SUPPORT BRACKET- TEE AND WEB IAW SRM 51-40-02. FABRICATED NEW BRACKET IAW SRM 51-30-01. INSTALLED NEW BRACKET AND WEB ASSY AT STA 1326, RBL 60. IAW SRM 561-40-02. CATEGORY "A',Jan 5, 2010 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200912154472Skin · dentedLT WING, NR 3 SLAT, T/E WEDGE UPPER SURFACE HAS SEVERAL DENTS FROM MID SECTION TO INBD EDGE. SEVERAL DENTS FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01, PAGE 103, PARA. M, DUE TO PROXIMITY TO EACH OTHER. DENTED AREA REPAIRED IAW SRM 51-70-10, BONDED DOUBLER, AT Dec 15, 2009 · N921FD · Boeing 75728A · Leading Edge DevicesSDR FDEA200912114417Skin · crackedFASTNER HOLE AT STA 1481 S-26L IS CRACKED. REMOVED DAMAGE SKIN IAW SRM 53-00-01. FABRICATED DOUBLER PN NR 2024-T3-.063, FILLER PN NR 2024-T3-.050 IAW SRM 53-00-01. INSTALLED DOUBLER AND FILLER ON FUSE SKIN STA 1477- 1484, S26L, AND CLIP STA 1480, IAW SRM 5Dec 11, 2009 · N921FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200912084386Strap · corrodedAPU INTAKE DOOR AFT FRAME LWR CORNER HAS CORROSION. REMOVED UPPER STRAP APU AFT FRAME FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08, REMOVED LOWER STRAP ALSO. FABED ON MAE TRAV NR T9/808706, TRAV NR T9/808707. INSTALLED NEW UPPER AND LWR STRAPS AND ATTACHING Dec 8, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200912074368Attach Angle · corrodedTHE CHANNEL CLIP, PN 146N8769-24, AND ATTACHING ANGLE, PN 146N8722-41, IN THE R4 DOOR LWR SILL, ARE CORRODED BEYOUND ALLOWABLE LIMITS AND BS 1645. THE CHANNEL CLIP. PN 146N8769-24 AND ANGLE, PN 146N8722-41, WERE REMOVED AND REPLACED AT BS 1645, R4 DOOR LWR Dec 7, 2009 · N921FD · Boeing 75723A · Fuselage Main, Attach FittingsSDR FDEA200912074367Channel · corrodedTHE 143N8328-60 CHANNEL IS CORRODED AT BS 1663, R4 DOOR LWR SILL. THE CHANNEL PN 143N8328-60 WAS REMOVED AND REPLACED AT BS 1663, R4 DOOR LWR SILL, IAW SRM 51-40-02. ORIG MATL THICKNESS; .063", AFTER REWORK; .031". FOUND OUT OF LIMITS IAW SRM 53-60-15. THISDec 7, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200912074366Stiffener · corrodedTHE 146N8722-60 STIFFNER IS CORRODED AT R4 DOOR LWR SILL, BS 1661. THE STIFFNER PN 146N8722-60 WAS REMOVED AND REPLACED AT R4 DOOR LWR SILL, BS 1661. IAW SRM 51-40-02. ORIG MATL THICKNESS; .071", AFTER REWORK; .046". OUT OF LIMITS IAW SRM 53-60-15. THIS REPADec 7, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200911204105Seat Track · crackedWEB BENEATH LBL 45 SEAT TRACK CRACKED ON BOTTOM FLANGE, STA 660 TO 680. REMOVED WEB AND SPLICE PLATE IAW SRM 51-40-02, FABRICATED NEW WEB IAW DWG 140N2506 AND SPLICE PLATE IAW DWG 140N2505, TREATED AND PRIMED AND TOP COATED IAW SRM 51-20-01 AND AMM 51-21-01. INov 20, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200911204090Frame · corrodedRT LWR FUSELAGE WING TO BODY FAIRING FRAME FS 900 CORRODED WITH CORRODED FASTENERS. REMOVED CORROSION WING TO BODY FRAME STA. 900 FOUND OUT OF LIMITS IAW SRM 53-00-71 DET. 7 REPLACED FRAME, DRILLED AND INSTALLED IAW SRM 51-40-02 THIS IS A MAJOR "A" REPAIR NO Nov 20, 2009 · N921FD · Boeing 75723A · Aerodynamic FairingsSDR FDEA200911204089Frame · dentedLWR FUSELAGE FS 900 WING TO BODY FRAME CORRODED AND CORRODED FASTENERS. REMOVED CORROSION AT F. STA 900 WING TO BODY FAIRING RBL 63 TO LBL 63 FOUND OUT OF LIMITS IAW SRM 53-00-71 DET. 7 , REMOVED AND REPLACED FRAME CORD IAW SRM 51-40-02 THIS IS A MAJOR "ANov 20, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200911204100Web · crackedMAIN CARGO DECK BS 1420-1440, RBL 64, WEB CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-40-02 AND 51-40-02, FABRICATED NEW WEB ON MAE TRAVELER T9/810194. REMOVED AND RE-INSTALLED SPLICES AND ANGLE 2 BS 1420-1430, S17R, RBL 64, TO FACILITATE REPAIR IAW SRM 51-4Nov 20, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200911204099Web · crackedMAIN CARGO DECK BS 1400-1420 RT SIDE BL 64 WEB CRACKED. REMOVED AND REPLACED WEB AT BS 1400-1420, RBL 64, IAW SRM 51-40-02. FABRICATED NEW WEB ON MAE TRAVELER T9/8140193, LOCATED AND DRILLED IAW SRM51-40-05. REMOVED AND RE-INSTALLED SPLICES AT BS 1400-1410, RNov 20, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200911204092Floorbeam · corrodedMAIN CABIN FLOOR STR STA 324 RBL 39 TO 46 FLOORBEAM UPPER SURFACE HAS AREAS OF CORROSION. REMOVED FLOOR T-CHORD, AND ATTACHING PARTS, FABRICATED NEW TEE , WEB, & EXTRUSION. INSTALLED NEW TEE, NEW WEB, NEW EXTRUSION AND ATTACHING PARTS STA 324- 344, LBL 60-RNov 20, 2009 · N921FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200911194067Support Bracket · misalignedINCOMING FASTENER PATTERN ON THE FRAME ASSY DOES NOT FACILITATE INSTALLATION OF SUPPORT BRACKET ASSY FOR PULLEY INSTALLATION AT STA 1640, BETWEEN S-2L AND S-3L AT BS 1640 FRAME, BETWEEN S-2L AND S-3L, THE EXISTING SHEAR TIE HOLE PATTERN CONFLICTED WITH THE ACCNov 19, 2009 · N921FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200911113926Crease Beam · corrodedRT CREASE BEAM STA 1240-1280 CORRODED. REMOVED CORROSION IAW SRM 53-60-13 ORIGINAL THICKNESS - .070", AFTER REWORK - .060", .010" MATERIAL REMOVED. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, DETAIL 1. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CRNov 11, 2009 · N921FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200911073887Seat Track · corrodedMAIN CABIN SEAT TRACK STA 640-780 RBL 24 HAS CORROSION AND GOUGES REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK P/N BAC 1520-792, IAW SRM 53-30-52. INSTALLED NEW SEAT TRACK STA 640-780, RBL 24, IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.Nov 7, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200911063880Crease Beam · corrodedMAIN CABIN STA 740-760 RT SIDE INBD CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION ON CREASE BEAM IAW SRM 53-30-13 ORIG THICKNESS .070, AFTER REWORK .006 WITHIN LIMITS , REMOVED CORROSION ON WEB FOUND OUT OF LIMITS IAW SRM 53-30-15 FIG. 101 DET 4, ORIG. MNov 6, 2009 · N921FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200911043851Seat Track · damagedSEAT TRACK FASTENER HOLES ELONGATED BS 1415 RBL 24.0. CHECKED LIMITS FOR SEAT TRACK BS 1415-1445,M RBL 24, AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG 101, DETAIL 4. REMOVED SEAT TRACK BS 1320-1540, RBL 24, IAW SRM 51-40-02. FEABRICATED NEW SEAT TRNov 4, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200911043850Seat Track · corrodedMAIN CABIN SEAT TRACK RBL 24 STA 1379-1384 UPPER LOBES HAVE AREAS OF CORROSION. REMOVED CORROSION AND CHECKED LIMITS OF SEAT TRACK @ BS 1379-1384, RBL 24, AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG. 101, DETAIL 4. FABRICATED NEW SEAT TRACK ON N/R Nov 4, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200911033802Floor Support · corrodedAFT PIT FLOORBOARD SUPPORT UPPER SURFACE HAS CORROSION APPROX FROM STA 1440 TO STA 1500 AT LBL 4. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS. ORIG MAT THICKNESS 0.063 AFTER REWORK 0.042. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-83. REMOVED FLOOR SUPNov 3, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200910313750Seat Track · corrodedMAIN CABIN SEAT TRACK STA 680-780 LBL 45 HAS CORROSION AND GOUGES. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK P/N 60-6549/24 IAW SRM 53-30-52. INSTALLED NEW SEAT TRACK STA 680-780, LBL 45, IAW SRM 53-30-52, 51-40-02. MAJOR REPAIR.Oct 31, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910313752Floor Support · corrodedMAIN CABIN FLOOR STR AT L-1 DOOR STA 324 TO 377 LBL 60 HAS AREAS OF CORROSION AROUND NUT PLATES. REMOVED CORROSION AT FLOOR STRUCTURE FROM F STA 324 TO 377 FOUND OUT OF LIMITS IN 3 EA FLOOR SUPPORTS LBL 60 IAW SRM 53-00-04. REMOVED AND REPLACED WITH NEW FLOOROct 31, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200910313751Seat Track · corrodedMAIN CABIN FLOOR STR STA 1620 TO 1640 LBL 24 SEAT TRACK WEB CORRODED. REMOVED CORROSION IAW SRM 51-10-02. AREA FOUND OUT OF LIMITS IAW SRM 53-00-04, FIGURE 101, DETAIL II. REMOVED ANGLE AND WEB IAW SRM 51-40-02. RECEIVED NEW ANGLE AND WEB FROM FAB SHOP TOct 31, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910303741Seat Track · gougedSTA 418-440, RBL 24 SEAT TRACK GOUGED REMOVED SEAT TRACK IAW SRM 51-40-00-02, FIG 101, DETAIL VII. RECEIVED NEW SEAT TRACK PN 60-6549/24. INSTALLED NEW SEAT TRACK STA 418 TO 440, RBL 24, IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.Oct 30, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910303737Seat Track · gougedSTA 418-440 RBL 45 SEAT TRACK GOUGED. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. OLD SEAT TRACK WAS FOUND OUT OF LIMITS DUE TO GOUGE BEING MORE THAN 20% OF MATERIAL THICKNESS. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-02. TREATED AND PRIMED NEW SESTOct 30, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910283717Seat Track · corrodedSEAT TRACK UPPER AND LWR SURFACE CORRODED LBL 24 BS 1570-1640. REMOVED SEAT TRACK PER SRM 51-40-02 ,FABED NEW TRACK, P/N. BAC1520-792 BATCH 1544829 PER SRM 53-60-52 LOCATED END DRILLED AND INSTALLED IAW SRM 51-40-02 AND 51-20-05, THIS IS A MAJOR "A" REAPAIR NOct 28, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910263677Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 345, LBL 45, HAS AREA OF CORRORSION. REMOVED CORROSION, FABRICATED TEE CHORD STRAPS ON MAE TRAV 3 T9/806490, AND FABRICATED ANGLES ON MAE TRAV T9/806501, INSTALLED TEE CHORD, ANGLES, STRAPS REPAIR PARTS STA 345, LBL 54- RBL 37, IAWOct 26, 2009 · N921FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200910263674Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 340 LBL 20 TO 27 HAS AREA OF CORROSION (OUT OF LIMITS). REMOVED FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED FLOOR SUPPORT ON MAE TRAV NR T9\807944. INSTALLED FLOOR SUPPORT MCD STA 333-340, LBL 20-31 IAW SRM 51-40-02.Oct 26, 2009 · N921FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200910263673Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 340 LBL 32 TO 37 HAS AREA OF CORRODED OUT OF LIMITS. REMOVED CORROSION MCD STR STA 340 LBL 32-37 IAW SRM 51-10-02 CHECKED LIMITS. ORIG MAT THICKNESS = .032, AFTER REWORK MAT THICKNESS .018, MAT LOSS= .012 FOUND TO BE OUT OF LIMITS IAWOct 26, 2009 · N921FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200910263672Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 340 LBL 29 TO 32 HAS AREA OF CORRODED OUT OF LIMITS. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04. REMOVED 4EA. NUTPLATES, 2EA. BRACKETS, AND FLOORBEAM IAW SRM 51-Oct 26, 2009 · N921FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200910263671Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 333 LBL 38 TO 44 HAS AREAS OF CORRODED OUT OF LIMITS IAW SRM 53-00-04. REMOVED FLOOR SUPPORT, BS 324-345, AND 2EA SUPPORT BRACKETS, BS 324, LBL 38 AND 40, IAW SRM 51-40-02. RECEIVED NEW FLOOR SUPPORT, BS 324-345, LBL 38-40, PN 141N51Oct 26, 2009 · N921FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200910263670Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STA 324 TO 345 LBL 20 HAS AREAS OF CORRODED OUT OF LIMITS. REMOVED CORROSION FROM MCD FLOOR STRUCTURE, BS 324-345, LBL 20, IAW SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-04; ORIG. MATL. THICKNESS; .055Oct 26, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200910263669Door Frame · corrodedAUXILLARY POWER UNIT INTAKE DOOR FWD & LOWER FRAME HAS CORROSION (OUT OF LIMITS) REMOVED CORROSION, CHECKED LIMITS APU INTAKE DOOR FRAME .090 ORIG THICKNESS, MAT LOSS .025 OUT OF LIMITS, LWR FRAME ORIG THICKNESS .080 MAT LOSS .020 FOUND OUT OF LIMITS IAW Oct 26, 2009 · N921FD · Boeing 75723A · APU Cowling/ContainmentSDR FDEA200910263668Support · corrodedAFT PIT LT TRANSISTION PANEL SUPPORT WEB IS CORRODED BETWEEN STA 1480 TO STA. 1500 AT S-26L OUT OF LIMITS. REMOVED SUPPORT ANGLE AND WEB IAW SRM 51-40-02. FABRICATED SUPPORT ANGLE AND WEB ON MAE TRAV NR T9/808232, T9/808163. INSTALLED SUPPORT ANGLE AND WEOct 26, 2009 · N921FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200910203616Seat Track · corrodedSEAT TRACK CORRODED LBL 44, BS 1600-1640. REMOVED CORROSION MULTIPLE AREAS, BS 1600-1640, LBL 45, AT CROWN. MAX CLEANUP TOP SURFACE OF TRACK; MAT. LOSS= .022", L=.250", W=.500" 2 BS 1612. FOUD TO BE OUT LIMITS PER SRM 53-00-52. FLAGE MAX. CLEANUP; MAT. LOOct 20, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910203614Seat Track · corrodedMAIN CABIN SEAT TRACK RBL 24 CORROSION FROM STA 1180 TO 1280 (OUT OF LIMITS). REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK P/N 1520-792 IAW SRM 53-60-52, 51-10-02. INSTALLED SEAT TRACK STA 1180-1280, RBL 24, IAW SRM 51-40-02. MAJOR REPAIR.Oct 20, 2009 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
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