# Service difficulty reports: N937FD

A list on [N937FD](https://openairdocs.org/aircraft/N937FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 178 reports

- [SDR FDEA202609141333](https://openairdocs.org/sdr/FDEA202609141333.md): Gust Lock · failed · Sep 14, 2026 · N937FD · Boeing 7572T7 · Passenger/Crew Doors
  > WHILE 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 DOOR
- [SDR FDEA202607150927](https://openairdocs.org/sdr/FDEA202607150927.md): Collar · broken · Jul 15, 2026 · N937FD · Boeing 7572T7 · Passenger/Crew Doors
  > L1 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 FDEA202605280640](https://openairdocs.org/sdr/FDEA202605280640.md): Gust Lock · damaged · May 28, 2026 · N937FD · Boeing 7572T7 · Passenger/Crew Doors
  > L1 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 FDEA202601060008](https://openairdocs.org/sdr/FDEA202601060008.md): Skin · corroded · Jan 6, 2026 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > ENG. #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 FDEA202601060007](https://openairdocs.org/sdr/FDEA202601060007.md): Crease Beam · cracked · Jan 6, 2026 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > RH 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 FDEA202512302297](https://openairdocs.org/sdr/FDEA202512302297.md): Skin · corroded · Dec 30, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > NR 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 CORROS
- [SDR FDEA202512302296](https://openairdocs.org/sdr/FDEA202512302296.md): Skin · corroded · Dec 30, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE NACELLE STRUT ACCESS PANEL 433JR CUTOUT WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A F- 5430 - T0385806 P1
- [SDR FDEA202512292295](https://openairdocs.org/sdr/FDEA202512292295.md): Stringer · corroded · Dec 29, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Longeron/Stringer
  > MEC BETWEEN BS 418 - 440, S24R CORRODED. PERMANENTLY REPAIRED STRINGER 24R IAW SRM 53-00-03-2R, REP 2, FIG 201.
- [SDR FDEA202512272292](https://openairdocs.org/sdr/FDEA202512272292.md): Skin · corroded · Dec 27, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > NO 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 P1
- [SDR FDEA202512222284](https://openairdocs.org/sdr/FDEA202512222284.md): Crease Beam · corroded · Dec 22, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > MAIN 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 53-00-13-2R
- [SDR FDEA202512222283](https://openairdocs.org/sdr/FDEA202512222283.md): Crease Beam · corroded · Dec 22, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > MCC 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 53-00-13-2R
- [SDR FDEA202512222282](https://openairdocs.org/sdr/FDEA202512222282.md): Crease Beam · corroded · Dec 22, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > MAIN 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 FDEA202512192264](https://openairdocs.org/sdr/FDEA202512192264.md): Skin · corroded · Dec 19, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > ENG 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 FDEA202512172260](https://openairdocs.org/sdr/FDEA202512172260.md): Deck Plate · corroded · Dec 17, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > POINTS 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 FDEA202512172259](https://openairdocs.org/sdr/FDEA202512172259.md): Skin · corroded · Dec 17, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > NR 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. K
- [SDR FDEA202512122247](https://openairdocs.org/sdr/FDEA202512122247.md): Shear Web · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous Structure
  > CABIN 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 FDEA202512122246](https://openairdocs.org/sdr/FDEA202512122246.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 51
- [SDR FDEA202512122245](https://openairdocs.org/sdr/FDEA202512122245.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 REPLAC
- [SDR FDEA202512122244](https://openairdocs.org/sdr/FDEA202512122244.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 51-40-05
- [SDR FDEA202512122243](https://openairdocs.org/sdr/FDEA202512122243.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 5
- [SDR FDEA202512122242](https://openairdocs.org/sdr/FDEA202512122242.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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, SRM
- [SDR FDEA202512122241](https://openairdocs.org/sdr/FDEA202512122241.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 TRAC
- [SDR FDEA202512122240](https://openairdocs.org/sdr/FDEA202512122240.md): Skin · delaminated · Dec 12, 2025 · N937FD · Boeing 7572T7 · Trailing Edge Flaps
  > LEFT 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 FDEA202512112237](https://openairdocs.org/sdr/FDEA202512112237.md): Crease Beam · corroded · Dec 11, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > MAIN 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 FDEA202512102230](https://openairdocs.org/sdr/FDEA202512102230.md): Skin · dented · Dec 10, 2025 · N937FD · Boeing 7572T7 · Horizontal Stabilizer, Plate/Skin
  > LEFT 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 FDEA202512102229](https://openairdocs.org/sdr/FDEA202512102229.md): Skin · dented · Dec 10, 2025 · N937FD · Boeing 7572T7 · Horizontal Stabilizer, Plate/Skin
  > LEFT 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 51-70-10-2R
- [SDR FDEA202408301193](https://openairdocs.org/sdr/FDEA202408301193.md): Transmission · dirty · Aug 30, 2024 · N937FD · Boeing 7572T7 · Trailing Edge Flap Actuator
  > TE 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 #5
- [SDR FDEA202406280877](https://openairdocs.org/sdr/FDEA202406280877.md): Battery · no test · Jun 28, 2024 · N937FD · Boeing 7572T7 · Emergency Lighting
  > LEFT 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 FDEA202406120794](https://openairdocs.org/sdr/FDEA202406120794.md): Battery · no test · Jun 12, 2024 · N937FD · Boeing 7572T7 · Emergency Lighting
  > DURING 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 FDEA202402210206](https://openairdocs.org/sdr/FDEA202402210206.md): Fitting · damaged · Feb 21, 2024 · N937FD · Boeing 7572T7 · Wing Main, Frame Structure
  > DURING 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 B757
- [SDR FDEA202401240105](https://openairdocs.org/sdr/FDEA202401240105.md): Skin · dented · Jan 24, 2024 · N937FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
  > DENT 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, PER
- [SDR FDEA202401230102](https://openairdocs.org/sdr/FDEA202401230102.md): Skin · gouged · Jan 23, 2024 · N937FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
  > MAIN 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 TERMINATIN
- [SDR FDEA202401230101](https://openairdocs.org/sdr/FDEA202401230101.md): Skin · gouged · Jan 23, 2024 · N937FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
  > MAIN 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 TERMIN
- [SDR FDEA202401190091](https://openairdocs.org/sdr/FDEA202401190091.md): Floor Panel · dented · Jan 19, 2024 · N937FD · Boeing 7572T7 · Fuselage Floor Panel
  > MAIN CABIN FOUND DENTS ON FLOORBOARD PANEL #232 MJF BETWEEN STA 560 TO STA 680 RBL 58.22 TO RBL 63.5.
- [SDR FDEA202312151940](https://openairdocs.org/sdr/FDEA202312151940.md): Gust Lock · cracked · Dec 15, 2023 · N937FD · Boeing 757200 · Passenger/Crew Doors
  > L1 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 FDEA202302250344](https://openairdocs.org/sdr/FDEA202302250344.md): None · none · Feb 25, 2023 · N937FD · Boeing 757200 · Hydraulic Indicating System
  > PDIS 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 SO
- [SDR FDEA202302240342](https://openairdocs.org/sdr/FDEA202302240342.md): Pressure Switch · failed · Feb 24, 2023 · N937FD · Boeing 757200 · Hydraulic Indicating System
  > PDIS 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 R
- [SDR FDEA202208151986](https://openairdocs.org/sdr/FDEA202208151986.md): Bracket · broken · Aug 15, 2022 · N937FD · Boeing 757200 · Engine (Turbine/Turboprop)
  > ON #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 FDEA202206281611](https://openairdocs.org/sdr/FDEA202206281611.md): Door · intermittent · Jun 28, 2022 · N937FD · Boeing 757200 · Cargo/Baggage Doors
  > L1 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 52-11-00
- [SDR FDEA202202170318](https://openairdocs.org/sdr/FDEA202202170318.md): Frame · none · Feb 17, 2022 · N937FD · Boeing 757200 · Fuselage Main, Structure
  > WHILE 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 FDEA202202170317](https://openairdocs.org/sdr/FDEA202202170317.md): Frame · cracked · Feb 17, 2022 · N937FD · Boeing 757200 · Fuselage Main, Structure
  > AFT 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 FDEA202202150301](https://openairdocs.org/sdr/FDEA202202150301.md): Frame · cracked · Feb 15, 2022 · N937FD · Boeing 757200 · Fuselage Main, Structure
  > RH 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 RE
- [SDR FDEA202202110280](https://openairdocs.org/sdr/FDEA202202110280.md): Frame · damaged · Feb 11, 2022 · N937FD · Boeing 757200 · Fuselage Main, Structure
  > AFT 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 FDEA202202030205](https://openairdocs.org/sdr/FDEA202202030205.md): Seat Track · corroded · Feb 3, 2022 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 FDEA202201200109](https://openairdocs.org/sdr/FDEA202201200109.md): Floor Panel · delaminated · Jan 20, 2022 · N937FD · Boeing 757200 · Fuselage Floor Panel
  > COURIER 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 FDEA202201200108](https://openairdocs.org/sdr/FDEA202201200108.md): Floor Panel · delaminated · Jan 20, 2022 · N937FD · Boeing 757200 · Fuselage Floor Panel
  > FLOOR BOARD 221AF IS DELAMINATED. FABRICATED FLOOR BOARD 221AF ON VT MAE TRAVELER #T22/1593560 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202201200107](https://openairdocs.org/sdr/FDEA202201200107.md): Floor Panel · delaminated · Jan 20, 2022 · N937FD · Boeing 757200 · Fuselage Floor Panel
  > FLOOR BOARD 222AF IS DELAMINATED. FABRICATED FLOOR BOARD 222AF ON VTMAE TRAVELER #T22/1594130 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR
- [SDR FDEA202201200106](https://openairdocs.org/sdr/FDEA202201200106.md): Floor Panel · delaminated · Jan 20, 2022 · N937FD · Boeing 757200 · Fuselage Floor Panel
  > FLOOR 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 FDEA202103090606](https://openairdocs.org/sdr/FDEA202103090606.md): Handle · failed · Mar 9, 2021 · N937FD · Boeing 7572T7 · Passenger/Crew Doors
  > L1 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 CLUT
- [SDR FDEA202012173176](https://openairdocs.org/sdr/FDEA202012173176.md): Bottle · empty · Dec 17, 2020 · N937FD · Boeing 7572T7 · Emergency Equipment
  > L1 DOOR EMERGENCY ASSIST BOTTLE READING 0 PSI. REPLACED EMERGENCY POWER RESERVOIR BOTTLE. IAW AMM 52-11-30-4. AIRCRAFT OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N937FD/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N937FD/reports

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