N913FD

Service difficulty reports · 184

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 = 'N913FD' 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 FDEA202504020553Floor Support · misalignedSTA. 580 TO 600 LBL 45.5 BLOW OUT PANEL STRUCTURE IS MISSALIGNED. ACCOMPLISHED WITH EA# F5330-T0382716 P1, TITLE "FUSELAGE-FLOOR BEAMS REPAIR OF MISALIGNED FASTENER HOLES ON BLOWOUT PANEL STRUCTURE AT 580 AND 600 LBL 45.5" MAJOR REPAIR.Apr 2, 2025 · N913FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA202504020552Frame · damagedCABIN R/H FRAME HAS A FASTENER SHEARED AND THE HOLE IS ELONGATED AT STA 1640, BETWEEN STR 8R-9R DOT# 3521. ACCOMPLISHED REPAIR ON EA# F-5310-T0382395 P1 "FUSELAGE -MAINFRAME-STA1640, S-8R AND S-9R, FASTENER HEAD BROKE OFF AND MISSING, HOLE FOUND TO HAVE BEApr 2, 2025 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA202503290537Skin · not reportedWHILE ACCOMPLISHING GVI OF STRINER S-14L LAP SPLICE ON EO F-5330-E0344603 P1 STEP 3.A A SKIN REPAIR DOUBLER WAS FOUND INSTALLED AT STA. 1600-STA 1620 STRINGER S-12L TO S-14L ACCOMPLISHED WITH REPAIR ON EA F-5330-T0382552 P1 FUSELAGE-PLATES & SKINS-STA1600 Mar 29, 2025 · N913FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA202503280530Skin · corroded(DOT 38-24) RH LOWER FUSELAGE SKIN CORRODED STA 1788 APPROX 4" AREA, 3" ABOVE THE APU RH DOOR CUTOUT. COMPLIED WITH REPAIR ON EA F-5330-T0382463 P1 FUSELAGE-PLATES & SKINS-SKIN REPAIRS AT STA 1885 RHS AND STRINGER S-17R FOR CORROSION MAJOR REPAIRMar 28, 2025 · N913FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA202503240484Seat Track · corrodedMCD SEAT TRACK RBL 47.5 I/B FLANGE HAS CORROSION AT STA. 1460 AND 1520 REMOVED AND REPLACED DAMAGE SEAT TRACK FROM BS 1420 TO BS 1520 AT RBL 47.5 ON MATERIAL P/N BAC1520-792 BATCH # 0004362542 AND REPAIR SPLICE P/N; BAC1509-100449 BATCH # 0004189129 IAW SRMar 24, 2025 · N913FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503220474Seat Track · corrodedSEAT TRACK AT RBL 58.22 HAS CORROSION AT STA 1108, 1140, 1170, AND 1180- DOT 45-048 REMOVED AND REPLACED SEAT TRACK AT MAIN DECK, FROM STA 900 TO STA 1180 IAW SRM 51-40- 02 & 53-00-52-2R, PART MARKED IAW GMM 07-0-1001 MAJOR REPAIRMar 22, 2025 · N913FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503200464Strap · corrodedDOT 80-021 AFT CARGO COMPARTMENT F/S 1380-1460 CEILING AREA RH SIDE FLOOR BEAM STABILIZATION STRAP CORRODED. REMOVED AND REPLACED STABILIZATION STRAP AFT CARGO COMPARTMENT STA 1380-1540 IAW SRM 53-00-51-2R AND IAW SRM 51-40-02. FABRICATED STABILIZATION STRMar 20, 2025 · N913FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA202503150428Floor Panel · delaminated(DOT 38-31) MDC FLOOR PANEL 252MTF DELAMINATED BS1620-1640 RBL58.22 FABRICATED FLOOR PANEL 252 MTF ZONE 250 ON VTMAE TRAVELER #T25/1804424 IAW MAE DWG PL11864182 MAJOR REPAIRMar 15, 2025 · N913FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA202503150427Floor Panel · damagedFLOOR PANEL 232 MJF DAMAGED FABRICATED FLOOR PANEL 232 MJF ZONE 230 ON VTMAE TRAVELER #T25/1802791 IAW MAE DWG 11862181 REV. L MAJOR REPAIRMar 15, 2025 · N913FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA202503150426Floor Panel · damagedFLOOR PANEL 252 MSF DAMAGED FABRICATED FLOOR PANEL 252 MSF ZONE 250 ON VTMAE TRAVELER #T25/1802794 IAW MAE DWG PL 11864182 MAJOR REPAIRMar 15, 2025 · N913FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA202503140416Floor Panel · damagedFLOORBOARD 242MHF AT STA 1019 RBL 64.2 HAS INSERT PULLED OUT WITH SCREW STILL IN THE FLOOR STRUCTURE- DOT 45-045 FABRICATED FLOOR PANEL 242MHF ZONE 240 ON VTMAE TRAVELER #T25/1802598 IAW MAE DWG #PL11863182 REV A, MAJOR REPAIR, FASTENER REMOVED IAW SRM 51-Mar 14, 2025 · N913FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA202503140415Floor Panel · damagedFLOORBOARD PANEL 242MAF HAS INSERT PULLED OUT AND FASTENER STILL IN FLOOR STRUCTURE- DOT 45-048 FABRICATED FLOOR PANEL 242MAF ZONE 240 ON VTMAE TRAVELER #T25/1802793 IAW MAE DWG PL11863182 MAJOR REPAIR, FASTENER REMOVED IAW SRM 51-40-02-OG.Mar 14, 2025 · N913FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA202503140414Floor Panel · damagedFLOOR PANEL 222 BF DAMAGED FABRICATED FLOOR PANEL 222BF ZONE 220 ON VTMAE TRAVLER #T25/1802961 IAW BOEING DWG PL141N5361 REV. BC, MAJOR REPAIRMar 14, 2025 · N913FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA202503140413Floor Panel · damagedFLOORBOARD PANEL 241MPF HAS PULLED INSERT- DOT 45-052 FABRICATED FLOOR PANEL 241MPF ZONE 240 ON VTMAE TRAVELER #T25/1802792 IAW MAE DWG PL11863182, MAJOR REPAIR.Mar 14, 2025 · N913FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA202412131800Warning Message · false activationON FINAL (RWY 27 KMEM) 170 KIAS 1200AGL, FLAPS 20 TO 25, GEAR DOWN GOT TE FLAP DISAGREE EICAS. EXECUTED GO AROUND, RAN QRH, LANDED WITHOUT INCIDENT EMERGENCY DECLARED. PERFORMED PER 757 STEPS IN FIM 27-51 FAULT TREE 808. NO FAULTS FOUND AT THIS MOMENT. NODec 13, 2024 · N913FD · Boeing 75728A · Trailing Edge Flap Control SystemSDR FDEA202304170800Floorbeam · crackedFOUND CRACK ON FLOOR BEAM AT STA 580 AT LBL 45 ON UPPER FLANGE LOWER AREA WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A# F-5310-T0374058-FLOOR BEAM AT STA 580 AND LBL 45- CRACKED-REPAIR PER DRAWING SR 57-53-004-TRACKING MAJOR REPAIRApr 17, 2023 · N913FD · Boeing 757200 · Fuselage Structure (General)SDR FDEA202304160703Flap · damagedR/H WING INBD FLAP INNER SIDE NEAR MIDDLE SUPPORT HAS A SMALL HOLE "1/4 PERFORMED WET LAYUP REPAIR FOR MENTIONED AREA OF MAIN FLAP PER SRM 51-70-06,PARAGRAPH 5.B. REF. SRM 57-53-01-2R,FIG.201, DETAIL I,TABLE III.REP. DIM. : 5.5" X 5.5". REP. LOC.: 4" FROM TApr 16, 2023 · N913FD · Boeing 757200 · Wing StructureSDR FDEA202211302865Bulb · inoperativeL1 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. BULB REPLACED IAW AMM 33-51-06-2-1, REV 130.9, X1.Nov 30, 2022 · N913FD · Boeing 75728A · Emergency LightingSDR FDEA202211152785Bearing · misalignedAFTER LOADING, UNABLE TO LOCK MAIN CARGO DOOR, ONLY THE FWD CAM IS LOCKED, AFT CAM WOULD NOT MOVE. AMM: 52-32-00-5 DURING INSPECTION OF THE HOOK PIN, FOUND MISALIGNEMENT BETWEEN BOTH BEARING HOUSINGS, CAUSING POINT OF CONTACT AT WRONG LOCATION AND BLOCKING THNov 15, 2022 · N913FD · Boeing 75728A · Cargo/Baggage DoorsSDR FDEA202206291618Lamp · inoperativeFOUND ARM/DISARM LIGHT SWITCH BULB INOP. RELAMPED ARM/DISARM LIGHT SWITCH FROM P82 PANEL AS PER AMM 33-30-00-0. OPN CHECK GOOD. OK FOR FURTHER SERVICE.Jun 29, 2022 · N913FD · Boeing 757200 · Cargo Compartment LightingSDR FDEA202203230764Flap · dentedL/H WING OUTBD AFT FLAP FOUND SMALL DENT ON LOWER SURFACE CLOSE TO OUTBD END WITH ON DELAMINATION SIGHN PERFORMED WET LAYER REPAIR FOR MENTIONED AREA PER SRM 51-70-03, PAR. 5L REF. SRM 57-53-01-2R-1 REPAIR 1 FIG. 201 DETAIL 4, TABLE 2. REP. DIM. : 4" REPMar 23, 2022 · N913FD · Boeing 757200 · Trailing Edge FlapsSDR FDEA202203210912Seat Track · corrodedFOUND CORROSION ON SEAT TRACK UPPER FLANGE AT STA 880-860 AT RBL 45 WORK ACCOMPLISHED PER FEDEX E.A # F-5310-T0367599 CRACKED SEAT TRACK BTWN STA 860-880 LBL/RBL 45.50, ALTERNATE MATERIAL REQUEST FOR SRM REPAIR. MAJOR REPAIR.Mar 21, 2022 · N913FD · Boeing 757200 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202203210911Seat Track · noneFOUND MISSING PIECES OF UPPER FLANGE OF SEAT TRACK BETWEEN STA 880-860 AT LBL 45 WORK ACCOMPLISHED PER FEDEX E.A #F-5310-T0367599 CRACKED SEAT TRACK BTWN ST A860-880 LBL/RBL 45.50, ALTERNATE MATERIAL REQUEST FOR SRM REPAIR. MAJOR REPAIRMar 21, 2022 · N913FD · Boeing 757 · Fuselage Structure (General)SDR FDEA202202240930Floorbeam · corrodedFOUND CORROSION ON FLOOR BEAM UPPER T-CHORD AT STA 880 BETWEEN RBL 45-68 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A #F-5310-T0367576 B, FLOOR BEAM ASSY , STA 879, UPPER CHORD, BL 45-68, CORROSION, REPAIR MAJOR REPAIR.Feb 24, 2022 · N913FD · Boeing 75728A · Fuselage Structure (General)SDR FDEA202202240929Floorbeam · corrodedCORROSION WERE FOUND ON FLOOR BEAM UPPER T-CHORD LOCATED STA 880 LBL 45-60 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0367576 B, FLOOR BEAM ASSY, STA 879, UPPER CHORD, BL 45-68 CORROSION, REPAIR. MAJOR REPAIRFeb 24, 2022 · N913FD · Boeing 75728A · Standard Practices/StructuresSDR FDEA202202240834Floorbeam · corrodedCORRODED FLOOR BEAM UPPER T-CHORD LOCATED STA 1200 LBL 35-LBL 50 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0367712: FLOOR BEAM AT STA 1200 BTWN LBL24.75-45.5, UPPER CHORD CORROSION, PERMANENT REPAIR MAJOR REPAIRFeb 24, 2022 · N913FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA202202240779Skin · noneUNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON SKIN EMPENNAGE STA 1981.9-1941 11 O'CLOCK POSITION PERFORMED TAP TEST INSP. PER SRM 51-10-06 AND EVALUATED I.A.W CASCADE AEROSPACE WORK CARD 07765 NR0408 AND NR0407 AND NO DAMAGE OR DEVIATIONS NOTED. FOR RECORD Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240778Skin · unknownUNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON SKIN EMPENNSGE STA 1918.9-1941 12 O'CLOCK POSITION PERFORMED TAP TEST INSP PER SRM 51-10-06 AND EVALUATED I.A.W CASCADE AEROSPACE WORK CARD 07765 NR0408 AND NR0407 AND NO DAMAGE OR DEVIATION NOTED. FOR RECORD PUFeb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240767Skin · delaminatedFOUND CRACK AND DELAMINATION ON R/H WING LEADING EDGE SKIN UNDER SLAT #6 PERFORMED HOT BOND REPAIR FOR MENTIONED PANEL PER SRM 51-70-08, REF SRM 57-41-01- 2R, FIG.201 DETAIL I, TABLE II, REP. DIM. : 14"X27". REP. LOCATION : ISS 205.5 AND FROM FWD TO AFT EDFeb 24, 2022 · N913FD · Boeing 757200 · Wing StructureSDR FDEA202202240766Flap · noneUNDOCUMENTED COMPOSITE REPAIR ON L/H WING OUTER AFT FLAP LOWER SURFACE 11" FROM AFT EDGE 105" FROM OUTBD EDGE PERFORMED WET LAYUP REPAIR FOR MENTIONED AREA PER SRM 51-70-17, REF SRM 57-53-01- 2R-1 REPAIR 1, FIG.201 DETAIL IV TABLE II REP.DIM: 4". REP. LOCFeb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240763Skin · unknownUNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON STA 1963.8-1992.8 STR 6 O'CLOCK POSITION PERFORMED HOT BOND REPAIR PER SRM 51-70-10-2R, REF. SRM 53-80-01-2R, DETAIL 1. REP. DIM:5.5" REF. LOCATION: 6.5" FROM FWD EDGE OF PANEL AT 6 O'CLOCK. MAJOR REPAIRFeb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240741Seat Track · corrodedMULTIPE CORROSION WERE FOUND ON SEAT TRACK LOCATED STA 1180-1420 LBL 58 WORK ACCOMPLISHED PER FEDEX E.A # F-5300-T0367321. SEAT TRACK BTWN STA 1180-1420, LBL 58.22, CORROSION, PERMANENT REPAIR. MAJOR REPAIRFeb 24, 2022 · N913FD · Boeing 757200 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202202240740Seat Track · crackedCRACK ON SEAT TRACK LOCATED STA1580-1600 RBL 45 WORK ACCOMPLISHED PER FEDEX E.A # F-5300-T0367320: SEAT TRACK AT STA 1580-1600 RBL 58.22, CRACK, PERMANENT REPAIR MAJOR REPAIRFeb 24, 2022 · N913FD · Boeing 75728A · Standard Practices/StructuresSDR FDEA202202240708Channel · unknownUNDOCUMENTED REPAIR WERE FOUND ON 2 CHANNEL LOCATED STA 1380-1400 RBL 11 PERFORMED NEW SRM REPAIR PER SRM 53-60-52-2R, AND PER SRM 51-70-12 TYPICAL EXTRUDED REPAIR, THIS REPAIR IS A CAT. A REPAIR AND NO SUPPLIMENTAL INSP. ARE REQUIRED. MAJOR REPAIRFeb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240707Seat Track · corrodedCORROSION ON SEAT TRACK LOCATED STA 1540 LBL 45.5 PERFORMED SEAT TRACK REPAIR USING NEW SEAT TRACK SECTION , 2 EA ANGLES, AND STRAP PER SRM 53-00-52, FIG 201, REPAIR 1. THIS REPAIR IS A CATEGORY "A" REPAIR AND NO SUPPLEMENTARY INSP. ARE REQUIREDFeb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240642Channel · unknownUNDOCUMENTED SPLICE REPAIR WERE FOUND ON Z-CHANNEL OF FWD CARGO FLOOR STRUCTURE LOCATED STA 560-580 RBL 29 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 51-70-12 AND NO DAMAGE OR DEVIATIONS NOTED THIS IS A MAJOR REPAIRFeb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240641Channel · corrodedUNDOCUMENTED SPLICE REPAIR WERE FOUND ON Z-CHANNEL OF FWD CARGO FLOOR STRUCTURE LOCATED STA 560-580 LBL 8 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 51-70-12 AND NO DAMAGE OR DEVIATION NOTED. THIS IS A MAJOR REPAIRFeb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240640Seat Track · corrodedFOUND CORROSION ON SEAT TRACK UPPER CROWN AT STA 345-377 LBL 7 DAMAGED PART REMOVED AN NEW FABRICATED SEAT TRACK PER FEDEX EA # F-5310-T0367282 SUPERNUMERARY SEAT TRACK MATERIAL SUBSTITUTION, AND VENTURA PRODUCTION DWG INSTALLED PER SRM 51-40-02Feb 24, 2022 · N913FD · Boeing 757200 · Fuselage Structure (General)SDR FDEA202202240639None · noneMULTIPLE CORROSION ON SEAT TRACK BETWEEN STA 1280-1320 RBL 45 PERFORMED SEAT TRAK REPLACEMENT USING A NEW FABRICATED SEAT TRACK PER SRM 53- 00-52, FIG 201 REPAIR 1. AND FEDEX GMM 7-0-1001. THIS REPAIR IS A CATEGORY "A" REPAIR AND NO SUPPLEMENTARY INSP. ARFeb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/StructuresSDR FDEA202202240611Floorbeam · corrodedCORROSION ON EXISTING REPAIR UPPER T-CHORD LOCATED STA 1540 LBL 10 PERFORMED REPAIR TO ONE FLANGE OF THE FLOOR BEAM UPPER CHORD PER SRM 53-00-51-2R, FIG.201, REPAIR 5. THIS REPAIR IS A CAT. A REPAIR AND NO SUPPLEMENTAL INSPECTIONS ARE THIS IS MAJOR REPAIFeb 24, 2022 · N913FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA202202220742Beam · elongatedFLOOR BEAM UPPER T CHORD STA 1681 FOUND WITH ELONGATED HOLE AT LBL 4 AND 2EA UNUSED HOLES AT RBL 12 PERFORMED AFT DECK AND FLOOR BEAM REPAIRS PER SRM 53-60-51-2R REPAIR 2, AND REPAIR 3, FIG 201. THE REPAIRS ARE CAT. A REPAIRS, AND NO SUPPLIMENTAL INSPECTIFeb 22, 2022 · N913FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA202202220610Skin · unknownFOUND UNDOCUMENTED DOUBLER REPAIR AT DOOR 4R INNER SKIN ADJACENT TO STR 10R PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W EA F-5210-T0367359 AND NO DAMAGE OR DEVIATIONS NOTED THIS IS A MAJOR REPAIRFeb 22, 2022 · N913FD · Boeing 757200 · Passenger/Crew DoorsSDR FDEA202202220609Floorbeam · unknownFOUND UNDOCUMENTED UPPER T CHORD REPAIR AT STA 345 LBL 52-RBL52 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 53-00-51 AND MONARCH W/O 770838 NR AND NO DAMAGES OR DEVIATIONS FOUND FOR RECORDS PURPOSES ONLYFeb 22, 2022 · N913FD · Boeing 757200 · Passenger/Crew DoorsSDR FDEA202202170381Floor Panel · wornFLOOR PANEL P/N 11861182-16 AT STA 300 R/H FOUND WORN FABRICATED PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOCITION OF RFTA NO:02858-0204 P/N:N00236-T01-221MBF, B/N:20308927Feb 17, 2022 · N913FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202202170380Floor Panel · wornFLOOR PANEL P.N 11861182-15 AT STA 440 FOUND WORN FABRICATED THE PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOSITION OF RFTA NO:02858-0204. P/N:N00236-T02-221MAF, B/N:20308931Feb 17, 2022 · N913FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202202170379Floor Panel · wornFLOOR PANEL P/N 141N5361-213 AT STA 440 FOUND WORN FABRICATED THE PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOSITION OF RFTA NO:02858-0204 P/N:N00236-T03-221AF, B/N:20308935Feb 17, 2022 · N913FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202201300913Skin · gougedEVALUATE EXISTING REPAIR AT L/H WING O/B MAIN FLAP L/E PER EO F-5100-7-5001 PERFORMED DVI PER SRM 51-10-08 AND GOUGE FOUND ON EXISTING REPAIR. NEW REPAIR PERFORMED I.A.W EA F-5750-T0367457. L/H WING O/B MAIN FLAP GOUGE ON EXISTING REPAIR ON L/E SKIN REPAJan 30, 2022 · N913FD · Boeing 757200 · Trailing Edge FlapsSDR FDEA202110312703Warning Message · false activationON FINAL AT 160-170 KNOTS, GOT RUDDER RATIO EICAS. HYDRAULIC PRESSURE WAS NORMAL. COMPLIED WITH QRH, AND DIVERTED DUE TO WIND LIMITATIONS. TROUBLELSHOOTING CARRIED OUT ON BOTH RRCM 'S FOUND MODULE FAULT BALL S SHOWING ON BOTH RRCM'S ACCOMPLISHED FIM 27-Oct 31, 2021 · N913FD · Boeing 75728A · Rudder Tab Control SystemSDR FDEA202107231845Girt Bar · dirtyFORWARD ENTRY DOOR WILL NOT ARM. DOOR 1RH GIRT BAR MECHANISM INSPECTION PERFORMED I.A.W. AMM 52-11-25-5. FLOOR FITTINGS INSPECTED AND CLEANED. GIRT BAR RIPOSITIONED IN CORRECT POSITION AND GIRT BAR LEVER CHECKED FOR PROPER OPERATION SEVERAL TIME, SATISFACTJul 23, 2021 · N913FD · Boeing 75728A · Emergency EquipmentSDR FDEA202104230996Sensor · dirtyRH DOOR SLIDE LIGHT INOP. DOOR 1R GIRT BAR PROXY SENSOR CLEANED. OPS TEST ACC AMM 25-66-11-2 REV 127.9 (SUBTASK 25-66-11-822-045 046) SATIS. DOOR 1R GIRT BAR PROXY SENSOR CLEANED. OPS TEST ACC AMM 25-66-11-2 REV 127.9 (SUBTASK 25-66-11-822-045 046) SATApr 23, 2021 · N913FD · Boeing 75728A · Emergency Equipment
Back to N913FD