N937FD
Service difficulty reports · 178
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 = 'N937FD' 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 = 'N937FD' 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 FDEA202609141333Gust Lock · failedWHILE CLOSING THE L-1 DOOR, RAMP WAS UNABLE TO RELEASE THE GUST LOCK. FOUND HOLD OPEN DOOR COLLAR DAMAGED AND WILL REQUIRE REPLACEMENT. PART NIS AT FLL. AMM 52-11-08-8 REMOVED AND REPLACED L1 DOOR HOLD OPEN SPLIT COLLAR ASSY IAW AMM 52-11-08-8. L1 DOORSDR FDEA202607150927Collar · brokenL1 DOOR GUST LOCK FOUND BROKEN DURING POST FLIGHT CHECK UPON FLIGHT ARRIVAL. REINSTALLED NEW AND SERVICEABLE GUST LOCK AS REQUIRED, OPS CHECK GOOD IAW AMM 52-11-08-8.SDR FDEA202605280640Gust Lock · damagedL1 DOOR HOLD OPEN LOCK IS BROKEN. TROUBLESHOOTING REQUIRED PRIOR TO INSTALLING IPC EFFECTIVITY VERIFICATION IS ALSO REQUIRED. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR AND OPS CHKD GOOD IAW AMM 52-11-08-4.SDR FDEA202601060008Skin · corrodedENG. #2 NACELLE STRUT AFT ACCESS PANEL 443LL INSIDE SKIN AREA IS WITH CORROSION AREA WITH CORROSION AT ENG. #2 NACELLE STRUT AFT ACCESS PANEL 443LL INSIDE SKIN AREA WAS REPAIRED PER FEDEX E.A. #: F-5430-T0385801 P1 WITH TITLE: NACELLES / PYLONS - - SKIN / SDR FDEA202601060007Crease Beam · crackedRH LOBE INTERIOR BETWEEN BS 1720 AND STR 17 HAS CREASE BEAM WITH CRACK 2 INCH APROX. ACCOMPLISHED REPAIR ON ADDITIONAL DAMAGE FOUND: CRACK IN THE HOLE AT AFT PRESSURE BULKHEAD STA 1720 PER FEDEX E.A.#: F-5310-T0385818 P1 WITH TITLE: FUSELAGE - MAINFRAME - SDR FDEA202512302297Skin · corrodedNR 1 ENGINE NACELLE STRUT PP STA 174.30 R/H FWD BULKHEAD INTERNAL SIDE SKIN WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A.#: F - 5430 - T0385806 P1 WITH TITLE: NACELLES/PYLONS - SKIN/PLATES/PANELS - RN 1 PYLON INBD SIDE SKIN INNER SURFACE CORROSSDR FDEA202512302296Skin · corrodedNR 1 ENGINE NACELLE STRUT ACCESS PANEL 433JR CUTOUT WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A F- 5430 - T0385806 P1SDR FDEA202512292295Stringer · corrodedMEC BETWEEN BS 418 - 440, S24R CORRODED. PERMANENTLY REPAIRED STRINGER 24R IAW SRM 53-00-03-2R, REP 2, FIG 201.SDR FDEA202512272292Skin · corrodedNO 1 ENGINE NACELLE BETWEEN ACCESS PANEL 433 HR AND 433 JR INTERNAL SKIN WITH CORROSION. JOBS FOR NR W/O 91519, N00437 AND N00438 WAS INCLUDED AND ACCOMPLISHED UNDER FEDEX EA F-5430-T0385806 P1SDR FDEA202512222284Crease Beam · corrodedMAIN CABIN. CREASE BEAM. (RH) STA 1200 CORRODED. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT CREASE BEAM INBOARD CHORD AT STA 1200 RBL 64 WAS REPAIRED IAW B-757 SRM 53-00-13-2RSDR FDEA202512222283Crease Beam · corrodedMCC FLOOR BTWN STA 440 - 460 (RH CREASE BEAM) RBL 64.5 APROX WAS FOUND ON LOCATION WITH CORROSION. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT, CREASE BEAM INBOARD CHORD BTW STA 440-460 RBL 64.40 WAS REPAIRED IAW B-757 SRM 53-00-13-2RSDR FDEA202512222282Crease Beam · corrodedMAIN CARGO BAY, FLOOR INBOARD CHORD HAS SURFACE CORROSION AROUND NUTS PLATE BETWEEN BS 860 AND 879 CORROSION OUT OF LIMITS AT MAIN CARGO BAY CREASE BEAM INBOARD CHORD BTW STA 860 - 879 RBL 64 WAS REPAIRED IAW SRM 53-00-13-2R.SDR FDEA202512192264Skin · corrodedENG NR 2 NACELLE STRUT FWD ACCESS PANEL 443AR INSIDE SKIN IS WITH CORROSION. (INNER AREA.) ENG. NR 2 NACELLE STRUT OTBD SIDE FWD ACCESS PANEL 443AR SKIN OUT OF LIMITS WAS REPLACED IAW SRM 51-41-02-0G AND DWG 311N5041 REV. K.SDR FDEA202512172260Deck Plate · corrodedPOINTS NR 2 AND 3 WITH CORROSION OUT OF LIMITS AT DECK PLATE AREA, BS 1681, BTW RBL 13 - 23, OUT OF LIMITS AT CABIN DECK PLATE. REPAIRED IAW SRM 53-60-51-2R, REPAIR 2, ALTERNATIVE II.SDR FDEA202512172259Skin · corrodedNR 2 NACELLE STRUT FWD ACCESS PANEL 443GL INSIDE SKIN AREA IS WITH CORROSION. NR 2 NACELLE STRUT INBD SIDE FWD ACCESS PANEL 443GL SKIN OUT OF LIMITS WAS REPLACED IAW SRM 51-41-02-0G AND DWG 311N5041, REV. KSDR FDEA202512122247Shear Web · corrodedCABIN FLOOR SHEAR WEB HAD MULTIPLES SPOTS OF CORROSION, BS 1680 - 1720, AREA OUT OF LIMITS. BS 1697, LBL 08 IAW SRM 53-60-51-1A. REPAIRED IAW SRM 53-60-51-2R, REPAIR 2, ALTERNATIVE II.SDR FDEA202512122246Seat Track · corrodedMAIN CARGO BAY SEAT TRACK 45.50 RBL BETWEEN BS 1100 -1140 HAS MULTIPLE AREAS WITH CORROSION. REMOVED SEAT TRACK BS 1076 TO 1180, RBL 45.50 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 51-40-05-0G, SRM 51SDR FDEA202512122245Seat Track · corrodedMAIN CARGO BAY, SEAT TRACK 45.50 LBL BETWEEN BS 1180 - 1200 WITH CORROSION IN MULTIPLES AREAS. REMOVED SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO BAY BS 1180 TO 1240, LBL 45.50 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED NEW SEAT TRACK REPLACSDR FDEA202512122244Seat Track · corrodedMAIN CARGO BAY FLOOR SEAT TRACK HAS SURFACE CORROSION BETWEEN BS 680 & 720, RBL 58.22. REMOVED SEAT TRACK SECTION OUT LIMITS AT MAIN CARGO BS BS 640 - 880, RBL 58.22 IAW SRM 51-40-02-0G. TRIMED, LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-05SDR FDEA202512122243Seat Track · corrodedMAIN CABIN. SEAT TRACK, RBL 58.22 BTW BS 1180 TO 1200 CORRODED REMOVED SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO COMPARTMENT BS 1180 TO 1420 RBL 58.22 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED A NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 5SDR FDEA202512122242Seat Track · corrodedMAIN CARGO BAY SEAT TRACK LBL 58.22, BS 1180 - 1420 WITH CORROSION IN MULTIPLE AREAS. REMOVED THE SEAT TRACK SECTION IAW SRM 51-40-02-0G. TRIMMED, LOCATED, DRILLED AND INSTALLED A NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 51-40-05-0G, SRM 51-40-08-0G, SRMSDR FDEA202512122241Seat Track · corrodedMAIN CARGO COMPARMENT SEAT TRACK LBL BETWEEN BS 1180 - 900 WITH CORROSION IN MULTIPLE AREAS. REMOVED THE SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO BAY BS 900 - 1180, LBL 58.22 IAW SRM 51-40-02-0G; TRIMMED, LOCATED, DRILLED AND INSTALLED A NEW SEAT TRACSDR FDEA202512122240Skin · delaminatedLEFT WING OTBD MAIN FLAP T/E UPPER SURFACE HAD POSSIBLE DELAMINATION. APPLIED PERMANENT REPAIR ON AREAS WITH DELAMINATION AT LT WING OTBD MAIN FLAP T/E UPPER SURFACE BTW WBL 471 - WBL 501 IAW SRM 57-53-01-2R, TABLE III, AND SRM 51-70-07-0G.SDR FDEA202512112237Crease Beam · corrodedMAIN CARGO BAY FLOOR CREASE BEAM HAS SURFACE CORROSION BETWEEN BS 760 AND 780. REMOVED CREASE BEAM INBD CHORD SECTION OUT OF LIMITS AT MAIN CARGO COMPARTMENT LBL 64.20 BS 760 TO 900 IAW B757 SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED AND INSTALLED NEW CREASE SDR FDEA202512102230Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN HAD REPAIR DAMAGE AT LOWER INTERNAL SURFACE, HSS 104.248 & 128.248, DENT WITH DELAMINATION AT LT HORIZONTAL STAB UPPER SKIN ON LOWER INTERNAL SURFACE WAS APPLIED PERMANENT REPAIR IAW SRM 55-10-01-1A, TABLE 1, NOTE I, & SRM 51-SDR FDEA202512102229Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN HAD FIVE DENTS BETWEEN HSS 81.249 AND 104.248, APPLIED PERMANENT REPAIR AT LT HORIZONTAL STAB UPPER SKIN IAW SRM 55-10-01-1A, TABLE I NOTE I & SRM 51-70-10-2RSDR FDEA202408301193Transmission · dirtyTE FLAP DISAGREE ON APPROACH. FLAPS STUCK BETWEEN 20-25 DEGREES. EMERGENCY DECLARED. PERFORMED TROUBLESHOOTING PER FIM. FOUND FAULT CODE 305 (FLAP DISAGREE) ON FSEU-1. PERFORMED VISUAL INSPECTION OF ALL FLAP DRIVE TRANSMISSIONS AND JACKSCREWS. FOUND FLAP #5SDR FDEA202406280877Battery · no testLEFT SIDE EMERGENCY LIGHTS DO NOT TEST. R & R LT EMERGENCY LIGHTS POWER SUPPLY REF 757 AMM 33-51-07-2. OPS CHECK GOOD, OK FOR SERVICE.SDR FDEA202406120794Battery · no testDURING EMERGENCY EXIT LIGHT TEST R/H EXIT LIGHT INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW ABOVE REF. R/H EXIT LIGHT OPS CHK SERVICEABLE. OK TO CONTINUE.SDR FDEA202402210206Fitting · damagedDURING ACCOMPLISHED W/C EF-5730-E0340076 P11 STEP #3 PAGE 5 OF 13. FOUND #8 HOLE 2ND OVERSIZED. REMOVED & REINSTALLED #1 ENG IB & OB FAN COWLS, #1 PYLON BULLNOSE, IB TORQUE TUBE BTWN SLAT 4 & 5, Y-DUCT, LUBE FITTING, FUEL SUPPLY LINE & UPPER LINK IAW B757SDR FDEA202401240105Skin · dentedDENT FOUND AT FUSELAGE SKIN BTW STA 480-500, STR 22-R TO 23R. EVALUATED DENT ON FUSELAGE SKIN BETWEEN STA 480-500, STR 22R TO 23R FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-01-1A, FIG 101 DETIAL III, CUT DAMAGED AREA IAW B757 SRM 53-00- 01-2R PAR 4 D, PERSDR FDEA202401230102Skin · gougedMAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 497 1 1/8" BELOW S-10 IAW B757-200 SRM 52-30-01-1A FIG 101 SHEET 1 TO 5 FOUND IN LIMIT. SEE EA F-5330-T0377806 A P1 FOR TERMINATINSDR FDEA202401230101Skin · gougedMAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 490 0.787" BELOW S-10 IAW B757-200 SRM 52-30-01-1A FIG 101 SHEET 1 TO 5 FOUND OUT OF LIMIT. SEE EA F-5330-T0377806 A P1 FOR TERMINSDR FDEA202401190091Floor Panel · dentedMAIN CABIN FOUND DENTS ON FLOORBOARD PANEL #232 MJF BETWEEN STA 560 TO STA 680 RBL 58.22 TO RBL 63.5.SDR FDEA202312151940Gust Lock · crackedL1 DOOR GUST LOCK (COPPER GUIDE UNDER YELLOW LATCH) IS BROKEN. REMOVED AND REPLACED LEFT FORWARD ENTRY DOOR HOLD OPEN LOCK COLLAR REF B757 AMM 52-11-08-8. OPS CHECKED GOOD.SDR FDEA202302250344None · nonePDIS 937 29-30 1782 24FEB23 ONT FACT U LOGPAGES:381829 ON PUSH BACK IN ONT WE STARTED THE LEFT ENGINE AND THEN THE RIGHT ENGINE. ONCE THE RIGHT ENGINE STARTED WE RECEIVED " R HYD SYS PRESS" EICAS, AND "SYS PRESS" DISCRETE LIGHT, AND "BRAKE SOSDR FDEA202302240342Pressure Switch · failedPDIS 937 29-30 1780 24FEB23 ONT FACT U R HYD SYS PRESS EICAS AND DISCRETE LIGHT ALONG WITH BRAKE SOURCE IN FLIGHT. RAN THE QRH CHECKLIST, DECLARED AN EMERGENCY AND PREFORMED FLAPS 20 LANDING IN ONT. AMM: 29-11-17-4 REMOVED AND REPLACED RSDR FDEA202208151986Bracket · brokenON #2 ENGINE DURING REMOVAL AND REPLACEMENT OF COLD STREAM ACOUSTIC LINER FOUND MOUNTING BRACKET BROKEN OFF SUPPORT SHROUD LOCATED AT APPROX 9:00 POSITION AFT OF FAN. REPAIRED #2 ENG GAS GENERATOR FAIRING PER RB211 EM TASK 72-03-01-300-136 (FRS7712, REPAIR SDR FDEA202206281611Door · intermittentL1 DOOR EXTERIOR HANDLE WILL NOT LATCH DOOR. UPPER AND LOWER GATES ARE NOT CLOSING FULLY. WORKS NORMALLY FROM THE INSIDE. CYCLED INSIDE AND OUTSIDE L1 DOOR HANDLE CLOSED L1 DOOR SEVERAL TIMES USING EXTERIOR HANDLE L1 DR CKS GOOD REF B757 MM 52-11-00SDR FDEA202202170318Frame · noneWHILE ACCOMPLISHING EO F-5310-E0347443P1 FOUND EXSISTING REPAIR @ 1480 WHICH NEEDS EVALUATION FOR AMOC APPROVAL. COMPLIED WITH E.A. F-5310-154748 PART 4 FUSE-MAINFRAME AFT CARGO COMPARTMENT FRAME FLANGE DENT @ STA 1480 S26L FRAME REPAIR, MAJOR.SDR FDEA202202170317Frame · crackedAFT PIT LH BS 460 FRAME FREE FLANGE CRACKED BETWEEN STR-26 AND STR-27 COMPLIED WITH E.A. #F-5310-T0366660 P1 TITLE; FUSELAGE-MAINFRAME-STA. 1460 FRAME, BETWEEN S-26L AND S-27L CRACKED. MAJOR REPAIR.SDR FDEA202202150301Frame · crackedRH 1640 FUSELAGE FRAME WEB AND STR 14 LWR INBD AND OUTBD HOLES HAVE CRACK INDICATIONS. COMPLIED WITH EA# F-5310-T0366253 PT1 FUSELAGE - MAINFRAME. STA 1640, S-14R EO# F- 5310- E0344602 CRACK INDICATIONS, REPAIR - PARTIAL FRAME REPLACEMENT, PART MARKED RESDR FDEA202202110280Frame · damagedAFT CARGO AT STA 1300 LH S25-27L FRAME EXISTING REPAIR FOUND PER EO F-5310--E0347443 B PT1 REMOVED AND REPLACED EXISTING REPAIR AT STA 1300 LH SIDE S25-27L PER EA F-5310- T0366461 PT 1 TITLE: FUSELAGE - MAINFRAME - EXISTING FRAME REPAIR AT STA 1300 FRAME SDR FDEA202202030205Seat Track · corrodedMAIN CARGO DECK @STA. 1640 SEAT TRACK RBL 45.50 HAS CORROSION. REMOVED CORROSION IAW SRM 53-00-52-1A D=0.40" FOUND TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02-0G, BATCH # 0002663579 MAT. BAC 1520-792A, MAJOR REPAIR.SDR FDEA202201200109Floor Panel · delaminatedCOURIER AREA FLOOR BOARD 221 MBF IS DELAMINATED. FABRICATED FLOOR BOARD 221 MBF ON VTMAE TRAVELER #T22/1593564 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202201200108Floor Panel · delaminatedFLOOR BOARD 221AF IS DELAMINATED. FABRICATED FLOOR BOARD 221AF ON VT MAE TRAVELER #T22/1593560 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202201200107Floor Panel · delaminatedFLOOR BOARD 222AF IS DELAMINATED. FABRICATED FLOOR BOARD 222AF ON VTMAE TRAVELER #T22/1594130 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIRSDR FDEA202201200106Floor Panel · delaminatedFLOOR BOARD 221 MAF IS DELAMINATED. FABRICATED FLOOR BOARD 221 MAF ON VTMAE TRAVELER # T22/1593569 IAW DWG SRZ-25- 005 REVISION R, MAJOR REPAIR.SDR FDEA202103090606Handle · failedL1 DOOR HARD TO OPEN AND CLOSE FROM EXTERIOR PART. IDENTIFIED PARTS DOOR HANDLE. REMOVED AND REPLACED CENTER SHAFT AND CLUTCH COLLAR ON L1 PAX DOOR HANDLE MECHANISM UP TO STEP E(2)(L). REF B757 AMM 52-11-13-2. COMPLETED INSTALL OF CENTER SHAFT AND CLUTSDR FDEA202012173176Bottle · emptyL1 DOOR EMERGENCY ASSIST BOTTLE READING 0 PSI. REPLACED EMERGENCY POWER RESERVOIR BOTTLE. IAW AMM 52-11-30-4. AIRCRAFT OK FOR SERVICE.
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