N915FD

Service difficulty reports · 213

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 = 'N915FD' 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 FDEA2019010113624Structure · corrodedWTB. CHORD CORRODED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-71 ALLOWABLE DAMAGE 1 FIG 101 DETAIL IV AND VII REV 125 REPAIRED CHORD IAW EA F-5340-T0344282 P1.Dec 31, 2018 · N915FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201812283615Door Frame · damagedBS 231.21 BL0 FRAME DAMAGED AT FWD ACCESS DOOR LATCH FITTING. REPAIRED FRAME AT BS 231.21 B/L0 IAW SRM 53-00-07 REPAIR 7 REV 125.Dec 28, 2018 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201812283614Mount · damagedFWD LAV UPPER I/B FWD MOUNT IS DAMAGED ON FRAME B/S 297 BETWEEN S2L AND S3L, REPLACEMENT REQD. FABRICATED AND INSTALLED NEW MOUNT P/N 232N2003-4 IAW SRM 51-40-02 REV 125 AND DRAWING 232N2003 REV A.Dec 28, 2018 · N915FD · Boeing 757236 · Fuselage, Equipment Attach FittingsSDR FDEA201812193558Crease Beam · damagedCREASE BEAM WEB DAMAGED BS 1016 RBL 64 REPLACEMENT REQD. REPLACED CREASE BEAM WEB IAW SRM 53-40-13-1A REV 125 AND DRAWING.Dec 19, 2018 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201812183543Tee Fitting · corrodedKEEL BEAM WEB TEE CORRODED OUT OF LIMITS IAW SRM 53-00-71-1A FIG 101 DETAIL III AND DETAIL VII REPLACE AS REQD. KEEL BEAM TEE REPLACED IAW SRM 51-40-02 REV 125 AND DRAWING 144N8140 REV E.Dec 18, 2018 · N915FD · Boeing 757236 · Fuselage Main, KeelSDR FDEA201812183535Gate · wornWEAR MARK ON DOOR 4L LOWER GATE AFT O/B. EDGE OUTSIDE PERMITTED LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACE DOOR GATE IAW AMM 52-11-38-4 REV 122.7.Dec 18, 2018 · N915FD · Boeing 757236 · Passenger/Crew DoorsSDR FDEA201812153506Floor Panel · dentedDENT FOUND ON FLOOR PANEL BSTA 560-680 LBL 25-45. FLOOR PANEL REPAIRED AT BSTA 560-680 LBL 25-45 IAW SRM 53-00-50-2R FIG 201 REV 125.Dec 15, 2018 · N915FD · Boeing 757236 · Fuselage Floor PanelSDR FDEA201812153503Gate · damagedWEAR MARK ON DOOR 4R LOWER GATE OUTSIDE OF ALLOWABLE LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACE DOOR GATE IAW AMM 52-11-38-4 REV 122.7.Dec 15, 2018 · N915FD · Boeing 757236 · Passenger/Crew DoorsSDR FDEA201812143500Gate · corrodedLOWER DOOR GATE 2R HAS CORROSION OUTSIDE ALLOWABLE LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACED DOOR GATE IAW AMM 52-11-38-4 REV 122.7.Dec 14, 2018 · N915FD · Boeing 757236 · Passenger/Crew DoorsSDR FDEA2018122163582Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRK BSTA 1204-1210 RBL 58.22 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085Dec 6, 2018 · N915FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201812040137Angle · corrodedLT WING, RIVETS DAMAGED ON OT/BD TRAILING EDGE WEDGE OF NR 5 LE SLAT REPLACED CORRODED CLOSURE ANGLE TO SLAT NR 5 T/E WEDGE O/B END IAW EA T F-5750-T0344281 A P1 "WING -FLIGHT SURFACES-OUTBD CLOSURE ANGLE - SLAT NR 5 - CORROSION. THIS REPAIR IS CLASSIFIED AS MDec 4, 2018 · N915FD · Boeing 757236 · Leading Edge DevicesSDR FDEA2018122143580Seat Track · corrodedSUSPECT CORROSION AT B/S 1180-1200 LBL 24.5 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MAX ALLOWABDec 4, 2018 · N915FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201812043528Fitting · corrodedFITTING ON NR 1 CARGO DOOR CUT-OUT LOWER SILL AT BS 612.7 CORRODED. EVA AND RECTIFY FITTING ON NR 1 CARGO DOOR CUT-OUT LOWER SILL AT BS 612.7 REPLACED IAW SRM 51-40-02 REV 125.Dec 4, 2018 · N915FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201812030123Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, 22" AFT OF FRONT SPAR AT WS 204.5 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND Dec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201812030122Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 269 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TODec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201812030121Skin · corrodedRT WING, CORROSION ON UPPR SURFACE, ABOVE REAR SPAR AT WS 361 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO Dec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201812030120Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, ABOVE FRONT SPAR, WS 642 TO WS 654 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 ANDec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201812030119Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, AS OF REAR SPAR WS 289-293 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TDec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201812030118Skin · corrodedRT WING CORROSION ON UPPR SURFACE AFT OF REAR SPAR, WS312 TO WS316 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUNDec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201812030112Skin · corrodedLT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 215 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FDec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201812030111Skin · corrodedLT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 300 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FODec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201812030110Skin · corrodedLT WING UPPER TE, EVIDENCE OF CORROSION ADJACENT TO FASTENER HEADS AT AREA 5 INCHES AFT OF REAR SPAR AND 67 INCHES OUTBOARD OF WING ROOT FAIRING 195AL REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DADec 3, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201811300155Skin · corrodedLT WING, UPPER SURFACE RSS 170 TO RSS 200 AT WING SKIN AND TRAILING EDGE PANEL JOING SUSPECT CORROSION. COROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE OF LIMITS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1 REV 125. REPAIR CARRIED OUT IAW EA #F-573Nov 30, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201811300109Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS.748 TO WS761, 2 INCHES FWD OF REAR SPAR AND TRILING EDGE PANEL JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 ANNov 30, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201811300108Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101 TABLE Nov 30, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201811300107Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125 EVALUATED BLEND OUT AND FOUND AREA TO BE OUT OF LIMITS IAW DUE TO LOCATION OF DAMAGE IAW Nov 30, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201811300005Crease Beam · corrodedEVIDENCE OF CORROSION ON CREASE BEAM BS907-936 RBL64. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-40-13-1A ALLOWABLE DAMAGE FIG 101 REV 125 AT BS 936 RBL 64. CREASE BEAM INBOARD CHORD REPLACED IAW SRM 51-40-02 REV 125, DRAWING 144N5152 DRAWING Nov 30, 2018 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201811300004Crease Beam · corrodedEVIDENCE OF CORROSION ON CREASE BEAM BSTA 1052-1180 RBL 64 CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-40-13-1A ALLOWABLE DAMAGE FIG 101 REV 125 AT BS 1052 AND BS 1145 RBL 64. CREASE BEAM INBOARD CHORD REPLACED IAW SRM 51-40-02 REV 125, DRAWINGNov 30, 2018 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201811303401Floor Panel · crackedFLOOR PANEL CRACKED 252MUF FLOOR PANEL REPAIRED IAW SRM 53-00-50 FIG 201 RPR # 00001. SHEET 001.Nov 30, 2018 · N915FD · Boeing 757236 · Fuselage Floor PanelSDR FDEA201811303581Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRK BS1180-1200 RBL 47 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MANov 30, 2018 · N915FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018122103579Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRK BS1188-1200 LBL 45 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MANov 30, 2018 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201811303400Floor Panel · crackedFLOOR PANEL 251 MXF CRACKED REPAIRED FLOOR PANEL 251 MXF I.A.W. 53-00-50-2R FIG 201 REV125Nov 30, 2018 · N915FD · Boeing 757236 · Fuselage Floor PanelSDR FDEA201811303402Bolt · shearedMAIN CARGO DOOR FWD HOOK LATCH ACTUATOR BELLCRANK WAS FOUND TO HAVE A SHEARED BOLT. REPLACED MAIN CARGO DOOR FWD HOOK AND ATTACHING BELLCRANK IAW CMM 52-32-03 REPLACED FWD HOOK ATTACH BOLTS IAW SRM 51-40-02 PRFORMED ADJUSTMENT CHECK OF MAIN CARGO DOOR FWDNov 30, 2018 · N915FD · Boeing 757236 · Cargo/Baggage DoorsSDR FDEA201811290068Skin · corrodedLT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. REV 125 ALLOWABLE MINIMUM REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.145" REPAIRNov 29, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201811290066Skin · corrodedRT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. ALLOWABLE MINIMUN REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.148 REPAIR CARRIED OUNov 29, 2018 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA2018082322170Power Supply · inoperativeDURING A DAILY CHECK, FOUND THE L1 DOOR INTERIOR EMERGENCY LIGHT WAS NOT WORKING WITH THE COCKPIT SWITCH OR TEST PB. REPLACED THE POWER SUPPLY IAW AMM 33-51-07-2. OPS CHECKED THE EMERGENCY LIGHTS, NORMAL.Aug 22, 2018 · N915FD · Boeing 757236 · Emergency LightingSDR FDEA201801300277Cam · deformedFOUND THE MAIN DECK CARGO DOOR CAM LATCH NR 7 LIP DEFORMED. REMOVED AND REPLACED THE CAM LATCH IAW MM 52-32-00-0-0. ADJUSTED AND TEST PERFORMED IAW MM 52-32-00-05. TESTED OK.Jan 30, 2018 · N915FD · Boeing 757236 · Cargo/Baggage DoorsSDR FDEA201710032848Light · inoperativeRIGHT DOOR SLIDE ARM LIGHT NOT ILLUMINATED WHEN FIRST OFFICER WENT TO DISARM THE DOOR. RT DOOR SLIDE ARM LIGHT FILLARMENTS REPLACED IAW AMM 33-20-00. OPS TESTED GOOD.Oct 3, 2017 · N915FD · Boeing 757236 · Passenger Compartment LightingSDR FDEA201709142571Girt Bar · contaminatedLEFT DOOR ARMING HANDLE IS STIFF TO MOVE TO THE ARM POSITION AMM 25-66-10-2. GIRT BAR FLOOR FITTINGS FOUND CONTAMINATED WITH DEBRIS. FITTINGS CLEANED AND DEBRIS REMOVED. DOOR ARMING NOW SATISFACTORY TO CREW.Sep 14, 2017 · N915FD · Boeing 757236 · Emergency EquipmentSDR FDEA201707272059Fmc · malfunctionedON TWO OCCASIONS DURING FLIGHT, RT FMC GAVE INCORRECT PITCH COMMANDS TO AUTOPILOT. R & R THE RT FMC IAW AMM 34-61-01-4-2.Jul 27, 2017 · N915FD · Boeing 757236 · Flight Management Computing Hardware SystemSDR FDEA201707031844Floor Panel · damagedMAIN CARGO COMPARTMENT FLOOR PANEL AT POSITION 6R IS DAMAGED. REPAIRED MAIN CARGO FLOOR PANEL AT POSITION 6R IAW SRM 53-00-50, REV 121.Jul 3, 2017 · N915FD · Boeing 757236 · Fuselage Floor PanelSDR FDEA201706301851Floor Panel · damagedMAIN CARO BAY FLOOR PANEL 6R IS DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50, REV 121.Jun 30, 2017 · N915FD · Boeing 757236 · Cargo CompartmentsSDR FDEA201706161681Controller · malfunctionedCABIN ALTITUDE EICAS WARNING AT FL380. COMPLIED WITH QRH, DESCENDED TO FINAL ALTITUDE FL250. RECOVERED CABIN PRESSURE IN AUTO 2 AT CABIN ALTITUDE 7500. NORMAL DESCENT AND PRESSURE UNTIL LFPG. REPLACED THE NR 1 CPC IAW MM 21-31-02-4, TESTED OK. COMPLYED WIJun 16, 2017 · N915FD · Boeing 757236 · Cabin Pressure Control SystemSDR FDEA201702100489Seal · damagedLOST ALL LT HYD FLUID AT LEVEL OFF FL 380. FOUND LT WHEEL WELL, FLAP/SLAT DEPRESS MODULE LEAKING FROM A CAP. FOUND SEAL DAMAGED, REPLACED THE SEAL IAW SMP. LEAK CHECK PERFORMED IAW AMM 29-00-00-6, NO LEAKS FOUND.Feb 10, 2017 · N915FD · Boeing 757236 · Hydraulic System, MainSDR FDEA201702030392Girt Bar · out of adjustR1 DOOR WON'T ARM. RIGHT DOOR GIRT BAR ADJUSTED AS PER AMM 25-66-10-2. OPS CHECK OK. DOOR CAN ARM NORMALLY.Feb 3, 2017 · N915FD · Boeing 757236 · Escape SlideSDR FDEA201612074354Proximity Sensor · malfunctionedVERBAL REPORT FROM FLIGHT CREW. RT DOOR 1 SLIDE ARMED LIGHT DOES NOT ILLUMINATE WHEN DOOR IS ARMED. TROUBLESHOT AND FOUND PROXIMITYSENSOR M10116 BAD, REPLACED THE SENSOR IAW MM 25-66-11-2, CHECKED OK. ACFT OK FOR SERVICE.Dec 7, 2016 · N915FD · Boeing 757236 · Door Warning SystemSDR FDEA201611294285Skin · corrodedRIGHT WING LOWER SKIN HAS CORROSION. REPAIRED IAW EA F-5730-T0329901.Nov 29, 2016 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR FDEA201611284274Skin · debondedLEFT ELEVATOR FOUND DEBONDED ON UPPER AND LWR SKIN AT PREVIOUS REPAIR AREA. REPLACED THE LEFT ELEVATOR IAW AMM 27-31-01.Nov 28, 2016 · N915FD · Boeing 757236 · Elevator, Plate/SkinSDR FDEA201611144254Skin · dentedTHE RT INBOARD MAIN FLAP DENTED 20 INCHES FROM OUTBOARD EDGE OF FLAP AND 23 INCHES FROM AFT EDGE OF FLAP. REPAIRED IAW SRM 57-53-01, 57-53-01 AND SRM 51-70-10.Nov 14, 2016 · N915FD · Boeing 757236 · Trailing Edge FlapsSDR FDEA201611104202Hinge · damagedFOUND NR 1 ENGINE INBD AFT HINGE BOLT HOLE DAMAGED. REPAIRED IAW EA TF-5450-T0328068P2.Nov 10, 2016 · N915FD · Boeing 757236 · Nacelle/Pylon, Main Frame
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