N925FD
Service difficulty reports · 119
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 = 'N925FD' 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.
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 = 'N925FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202604240494Lamp · no testON SERVICE CHECK FOUND LH EMERGENCY SLIDE LIGHT INOP. AMM 33-51-06-2-1 RELAMPED LH EMERGENCY SLIDE LIGHT AS PER 757 AMM 33-51-06-2-1. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. FACT 24APR26 03:02 GSO AMM 33-51-06-2-1 RELAMPED LH EMERGENCY SLIDE LIGHTSDR FDEA202509251832Floorbeam · corrodedAFTER GVI ON DECK PLATE BS 1681.8 BETWEEN LBL 24.75 TO LBL 45.50 FOUND CORROSION COMPLIED WITH FEDEX EA # F-5310-T0384883 P1 TITLE: FUSELAGE - MAINFRAME-FLOOR BEAM AND DECK PLATE STA 1681 LBL24-LBL45 CORROSION REPAIR.SDR FDEA202509181740Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGES WITH CORROSION BETWEEN BS 1620 TO 1420 LBL 58.22 REMOVED MAIN CABIN SEAT TRACK BETWEEN BS 1420-1620 LBL 58.22 IAW B757 SRM 51-40-02-0G TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK IAW B757 SRM 51-40-05-0G, 51-40-08-0G BOEING DSDR FDEA202509091678Seat Track · corrodedMAIN CABIN SEAT TRACK RT FLANGE AT BS 1540, RBL 45.5 CORRODED. REMOVED THE SEAT TRACK FROM BS 1320-1540, RBL 45.5 IAW SRM 51-40-02-0G. TRIMMED, LOCATED, AND DRILLED A NEW SEAT TRACK IAW SRM 51-40-05-0G, 51-40-08-0G, & DWG 146N5130, REV A. INSTALLED THE SEATSDR FDEA202509091677Seat Track · corrodedMAIN CABIN SEAT TRACK RT & LT FLANGES AT BS 1640, LBL 45.5 CORRODED. REMOVED THE SEAT TRACK BS 1540-1640 LBL 45.5 IAW SRM 51-40-02-0G. TRIMMED, LOCATED, AND DRILLED A NEW SEAT TRACK IAW SRM 51-40-05-0G, 51-40-08-0G, & DWG 146N5130, REV A. INSTALLED THE SEASDR FDEA202509091676Seat Track · corrodedMAIN CABIN SEAT TRACK LT FLANGE AT BS 1620 CRACKED RBL 45.5. REMOVED THE SEAT TRACK BS 1540-1640 RBL 45.5 IAW SRM 51-40-02-0G, TRIMMED, LOCATED, AND DRILLED A NEW SEAT TRACK IAW SRM 51-40-05-0G , 51-40-08-0G, AND DWG 146N5130, REV A. INSTALLED THE SEAT SDR FDEA202509091675Seat Track · corrodedCABIN SEAT TRACK AT B.S 770 RBL 58.22 WITH CORROSION. TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK MAIN CABIN STA 660-880 RBL 58.22 IAW B757 SRM 51-40-05-0G, 51-40-08-0G BOEING DWG # 657N3332 REV A. INSTALLED MAIN CABIN NEW SEAT TRACK FROM STA 660-880 RBL SDR FDEA202509081644Skin · corrodedLEFT WING INBOARD MAIN FLAP LOWER SKIN HAS CORROSION, (OUTBOARD FLAP TRACK AREA) UPON FURTHER EVALUATION ON LT WING INBD MAIN FLAP LOWER SKIN CORROSION FOUND OUT OF LIMITS IAW SRM 57-53-01-1A DETAIL I, FIG 101, SHEET 1, NOTE F AND APPLIED PERMANENT REPAIR IN SSDR FDEA202507311346Transmission · faultedTE FLAP DISAGREE CAUTION. COMPLIED WITH QRH. WITH FLAPS SELECTED TO 25, FLAPS WOULD NOT MOVE PAST 20. ALTN FLAPS SELECTOR USED TO SET FLAPS TO 25. EMERGENCY DECLARED. AMM: 27-51-06-4 WORKED IN CONJUNCTION WITH TSI 27-50-2326, REMOVED AND REPLACED #5 FLAP TSDR FDEA202504300694Ballscrew · lack of lubeON CONFIGURING AND SELECTING FLAPS 25 WE RECEIVED A TRAILING EDGE FLAP DISAGREE WARNING AND ASSOCIATED CAUTION LIGHT. WE DISCONTINUED THE APPROACH AND LANDED FLAPS 20. EMERGENCY DECLARED. FIM: 27-51, FT 808 AMM: 12-13-06-3 AMM: 12-21-09-3 AMM: 27-51-00SDR FDEA202411261739Flap System · malfunctionedSELECTING FLAPS 25 GOT TE FLAPS DISAGREE WITH FLAPS 20. AMM: 27-51-00-5 PERFORMED OPERATIONAL TEST OF FLAP SYSTEM IRW AMM 27-51-00-5. CYCLED THROUGH ALL POSITIONS TWICE. OPS CHECK GOODSDR FDEA202409041227Battery Pack · inoperativeDURING MX PRE-FLIGHT CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT SIGN (L31), AND L1 SLIDE LIGHT (L25)WILL ONLY STAY ILLUMINATED FOR APPROX 2 SECONDS. FACT 03SEP24 22:20 SWF AMM: 33-51-07-2 KEPT A/C POWERED UP FOR 3 HOURS AND ATTEMPTED EMERGENCY EXITSDR FDEA202311241893Gate · corrodedR1 DOOR LOWER GATE LOWER OUTER SKIN SHOWS SIGNS OF CORROSION REMOVED & REPLACED LOWER GATE HINGE IAW B757 SRM 51-40-02, RE-INSTALLED LIFTER ASSY IAW B757 AMM 20-11-00-2 & SRM 51-40-02. R-1 DOOR RIG ACCOMPLISHED ON NO. N00126, OPS 30126.SDR FDEA202311241892Wedge · delaminatedAD DISBOND INDICATION FOUND: #4 SLAT LOWER I/B SIDEE AT I/B STIFFENER, MARKED 5.5"L X 2.5"W COMPLETED PERMANENT REPAIR OF DISBOND FOUND ON #4 SLAT LOWER I/B SIDE AT I/B STIFFENER IAW FEDEX EA# F-5750-T0377026 TITLE WINGS - FLIGHT SURFACES.SDR FDEA202311221885Door · cracked#2RH DOOR - HINGE CUTOUT IS CRACKED. REPAIRED #2 DOOR HINGE CUTOUT IAW B757 SRM 52-10-02-2R.SDR FDEA202311171860Spoiler · crackedR/H WING LOWER SURFACE OF #11 SPOILER ACTUATOR ATTACH FITTING BARE METAL AND POSSIBLE CRACK. REMOVED AND REPLACED #11 SPOILER ASSY PER FEDEX B757 AMM 27-61-01-4, P/N 113N5501-40 S/N 776175SDR FDEA202311101850Support Angle · crackedFWD CARGO COMPARTMENT DOOR UPPER AFT CORNER SUPPORT ANGLE FROM AFT FRAME TP UPPER SUPPORT STRAP IS CRACKED. REMOVED AND REPLACED SUPPORT ANGLE ON FWD CARGO DOOR UPPER AFT CORNER PN: 69-53919U5 PO# 1074648.1 IAW BOEING DWG 69-53919 REV. B.SDR FDEA202311101846Support Angle · crackedFWD CARGO COMPARTMENT DOOR UPPER FWD CORNER SUPPORT ANGLE FROM FWD FRAME TO UPPER SUPPORT STRAP IS CRACKED . REMOVED AND REPLACED FWD CARGO COMPARTMENT DOOR FWD SUPPORT ANGLE PN: 69-53919U6 PO# 1074650.1 IAW BOEING DWG 69-53919 REV. BSDR FDEA202303310528Transmission · failedPDIS 925 27-80 0632 31MAR23 MEM OPEN U ON A 25 MILE FINAL APPROACH ATC SLOWED US TO 190 KNOTS. AT 210 KNOTS WE SELECTED FLAPS 1 AND GOT A TRAILING EDGE FLAP DISAGREE EICAS AND TRAILING EDGE LIGHT. RAN QRH AND USED ALTERNATE FLAPS FOR AN UNEVESDR FDEA202303290517Unknown · unknownON DOWNWIND AT 210 KNOTS SELECTED FLAPS 1 AND GOT TRAILING EDGE FLAPS LIGHT & EICAS. RAN QRH, USED ALTERNATE FLAPS/SLATS & LANDED UNEVENTFULLY WITH FLAPS 20. EMERGENCY DECLARED. EMERGENCY DECLARED. ACCOMPLISHED FLAP/SLAT ELECTRONIC UNIT BITE PROCEDURES PSDR FDEA202210112537Engine · power lossON TAKEOFF ROLL, F/O FLYING, ACFT TOOK A LOT OF RT RUDDER AT CLIMB OUT, LT ENG 5-10% LOWER N1 & SLIGHTLY LOWER EPR. INCREASED POWER ON LT ENG TO MATCH RT. RT ENG INCREASED SLIGHTLY ON IT`S OWN & GOT A COMPRESSOR STALL, 2 QUICK BANGS. RETARDED RT ENG POWER & SDR FDEA202203040774None · noneINTERIOR EMERGENCY LIGHTS TEST SWITCH ON L1 DOOR INOP. CONFIRMED FAULT, EMERGENCY LIGHTS WOULD NOT TEST FROM L1 DOOR TEST SWITCH. REMOVED AND REPLACED S10292 SWITCH (CPN: 3313573) REF WDM 33-51-12 SHEET 1 AND IPC 33-51-53-01. PERFORMED EMERGENCY SDR FDEA202202090255Seat Track · corrodedCOCKPIT CREW SEAT TRACK AT BARRIER WALL RBL 45, FWD END HAS CORROSION ALL THE WAY THROUGH TACK AS MARKED. REPAIRED SEAT TRACK RBL 45 STA 365 TO 377 PER EA # F-5310-T0366490 P1, FUSELAGE- MAINFRAME-COURIER AREA SEAT TRACK CORROSION-REPAIR, MAJOR REPAIR.SDR FDEA202202070240Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION ON SEVERAL NUT PLATE HOLES LOCATED BET STA 1140 AND STA 1200 LBL 45. REMOVED AND REPLACED SEAT TRACK FROM STA 1180-1240 LBL 45 IAW SRM 51-40-02, MAJOR REPAIR.SDR FDEA202202010173Slat · none#9 SLAT COVE SKIN CRACKED AT O/B MAIN TRACK ATTACH FITTING. REMOVED AND REPLACED #9 CRACKED COVE SKIN AT O/B MAIN TRACK ATTACH FITTING IAW SRM 51-40-02 AND DWG.114N4078 AND SRM 57-43-01-OI, FIG.1, MAJOR REPAIR.SDR FDEA202202010172Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION ON SEVERAL NUT PLATE HOLES LOCATED BET STA 1100 AND STA 1180 RBL 45. REMOVED CORROSION IAW SRM 51-10-02, ORIGINAL MATERIAL 0.080", MATERIAL LOSS 0.018", REMAIN 0.062", FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FABRICATED SDR FDEA202201310170Slat · cracked#3 SLAT COVE SKIN CRACKED AT O/B MAIN TRACK ATTACH FITTING. REMOVED AND REPLACED #3 SLAT COVE SKIN AT O/B MAIN TRACK ATTACH FITTING IAW SRM 51- 40-02, MAJOR REPAIR AND DWG. #114N4077 AND SRM 57-43-01-OI, FIG.1..SDR FDEA202201260146Floor Panel · delaminatedCOURIER AREA FLOOR BOARD 221MBF IS DELAMINATED. FABRICATED FLOOR BOARD 221MBF ON VTMAE TRAVELER # T22/1594116 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202201260145Floor Panel · delaminatedCOURIER AREA FLOOR BOARD 222AF DELAMINATED. FABRICATED FLOOR BOARD 222AF ON VTMAE TRAVELER # T22/1594121 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202201260144Floor Panel · delaminatedCOURIER AREA FLOOR BOARD 222MAF IS DELAMINATED. FABRICATED FLOOR BOARD 222MAF ON VTMAE TRAVELER # T22/1594128 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA2020072381577Bulb · inoperativeR1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED R1 DOOR SLIDE LIGHT BULB, P/N 767 . LIGHT CHECKED GOOD REF B757 AMM 33-51-06-2-1. OK FOR SERVICESDR FDEA2020012740224Skin · chafedWEAR MARK AT LEFT IN-BOARD FLAP LEADING EDGE. ALL WORK ACCOMPLISHED IAW EA F-5750-T0352020 P1 WING - FLIGHT SURFACES - LT INBOARD MAIN FLAP LEADING EDGE SKIN REPAIR.SDR FDEA202001170161Skin · corrodedPROTUDING FASTENERS APPROX AT STA-400 BETWEEN S14L ALL WORK ACCOMPLISHED IAW EA F-5330-T0351895 P1. FUSELAGE - PLATES & SKINS - CORROSION AT STA 394, STRINGER S-14L.SDR FDEA202001160150Doubler · crackedR2 DOOR UPPER HINGE CUTOUT PREVIOUS DOUBLER IS CRACKED. R2 DOOR WAS REMOVED AND REPLACED IAW AMM 52-11-01-4. OP'S CHECK OF DOOR GOOD IAW AMM 52-11-01-4.SDR FDEA2019111192914Battery Pack · failedMDIS 925 33-50 8137 09NOV19 DAY FACT U L1 DOOR AND LEFT SLIDE LIGHT INOP R/I 09NOV19 02:04 DAY U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 2013-1A POS: 1 SRL: 72660 TAG NBR: H733SDR FDEA201910172677Lamp · inoperativeNOSE GEAR LIGHT DID NOT ILLUMINATE WHEN GEAR WAS DOWN AND LOCKED. NOSE GEAR LIGHT DID NOT TEST. VERIFIED LIGHTS WOULD NOT TEST FOR NOSE GEAR LIGHT. RE-LAMPED PER SWPM 20-84-15 AND PERFORMED PSEU BITE PER FIM 32-09 FIG 104. AND ALL TESTS PASSED. OK FOR SDR FDEA201909242336Hydraulic Line · leakingAT 3000', 170KT IAS, PUT GEAR HANDLE DOWN AND FLAPS TO 20 FOR BEFORE LANDING CHECK LIST. NOSE GEAR DID NOT GO DOWN (NO LIGHT) AND LEFT HYDRAULIC SYSTEM PRESSURE EICAS WITH GEAR DISAGREE MSG. COMPLIED WITH QRH, EMERGENCY DECLARED. FOUND NOSE GEAR STEERING PRESSSDR FDEA201807201792Eva System · failedWHILE PERFORMING EO F-2560-E0323178 FOUND CAPT'S EVAS BLOWER NOT TESTING. R&R CAPT'S EVAS TESTS GOOD REF MM25-62-00-4.SDR FDEA201701060064Door · damagedPOST FLIGHT, FOUND RT MLG STRUT DOOR LEADING EDGE DAMAGED. REPAIRED IAW EA F-5280-T0330701 REV B PART 3.SDR FDEA201604011137Light · inoperativeSERVICE CHECK R1 DOOR ESCAPE SLIDE LIGHT INOPERATIVE. RELAMPED RT SLIDE LIGHT. OPERATIONS CHECKED GOOD. OK FOR SERVICE IAW MM 33-51-06-2-1.SDR FDEA201603180953Light · inoperativeL1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED L1 DOOR ESCAPE SLIDE LIGHT, L25, OPERATIONS CHECKED GOOD.SDR FDEA201512194037Bracket · corrodedUPON REMOVAL OF ACCESS DOOR 313AL LT & 313AL RT, DOOR STOP PAD ATTACH BRACKETS FOUND CORROSION AT LOWER AFT STRAP AREA BS 885.2, LBL 2-8 & RBL 1-6. REMOVED DAMAGED LOWER INNER AFT STRAP BS 1885.2, FABRICATED NEW STRAP. INSTALLED NEW STRAP IAW SRM 51-40-02, 5SDR FDEA201512184028Door Frame · crackedDURING ACCOMPLISHMENT OF EO F-5210-7-5003 PT 4, INSPECTION OF THE INNER CHORD OF THE R2 DOOR FRAME AT THE UPPER CUT OUT WAS FOUND TO BE CRACKED. COMPLIED WITH REPAIR ON NR 2 RT DOOR FRAME AT UPPER HINGE CUT OUT IAW SRM 52-10-02-2R REPAIR 1& EA F-5210-T0322267SDR FDEA201512113978Frame · damagedFORWARD ACCESSORY COMPARTMENT INTERIOR FRAME AT BS 231.25, BL 0 HAS A HOLE WORN THROUGH RADIUS. COMPLIED WITH EA F-5310-TO322113 P1.SDR FDEA201410012884Light · inoperativeON WALK AROUND FOUND EXTERIOR RT SIDE EMER LIGHT INOPERATIVE. CHECKED VOLTAGE AT LAMP SOCKET, CHECKED GOOD. RELAMPED, OPERATIONS CHECKED GOOD IAW AMM 33-51-06-2-1. ACFT OK TO CONTINUE.SDR FDEA201408152180Window · crackedRIGHT OUTER WINDSHIELD SHATTERED IN FLIGHT AT FL 380. REMOVED AND INSTALLED A NEW WINDOW PER MM 56-11-01-4. SECOND TORQUE DUE NOT BEFORE 15:45 Z. STILL WAITING ON AERODYNAMIC SEALANT TO ARRIVE. FINAL TORQUE C/W, AND SEALANT HAS BEEN APPLIED. A/C IS READY SDR FDEA201408142173Window · crackedLEFT FWD WINDOW SHATTERED DURING CRUISE FLIGHT AT 400, NO LEAKS. CONTINUED AFTER CONSULTING WITH GOC. REPLACED WINDOW IAW AMM.SDR FDEA201403260585Light · inoperativeR1 DOOR SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMP ON R1 SLIDE LIGHT IAW 33-51-06. ACFT OK TO CONT.SDR FDEA201309192251Power Supply · inoperativeDURING SERVICE CHECK, THE RT SIDE EMERGENCY LIGHTS INOPERATIVE DURING TEST. R & R RT POWER SUPPLY FOR THE EMERGENCY LIGHTS IAW MM REF 25-22-02. OP`S CHECKED GOOD.SDR FDEA201307171580Structure · damagedCLIMBING THROUGH 11,000 MSL, HEARD A LOUD PRESSURIZATION BUMP. CABIN RATE CLIMBING AT 2000 FPM AND CABIN ALT CLIMBING. LEVELED AT APPROX 14000 MSL AND STARTED DESCENT TO 10,000 AT APPROX 11000 MSL CABIN, ALT 1 EICAS. COMPLIED WITH QRH, SELECTED AUTO 2 AND
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