# Service difficulty reports: N934FD

A list on [N934FD](https://openairdocs.org/aircraft/N934FD.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 11 · 539 reports

- [SDR FDEA202609091291](https://openairdocs.org/sdr/FDEA202609091291.md): Flap System · faulted · Sep 9, 2026 · N934FD · Boeing 75721B · Trailing Edge Flap Control System
  > TE FLAP DISAGREE WHEN GOING FROM FLAPS 20 TO 25. RAN QRH. DECLARED EMERGENCY ***EMERGENCY DECLARED*** CARRIED OUT FIM TASK 27-51 808 ON TRAILING EDGE FLAP SYSTEM. NO DEFECTS NOTED OK FOR CONTINUED SERVICE.
- [SDR FDEA202608201185](https://openairdocs.org/sdr/FDEA202608201185.md): Engine · damaged · Aug 20, 2026 · N934FD · Boeing 75721B · Fuel Controlling System
  > ON CLIMB AT ABOUT 18000 FT RIGHT ENGINE EGT WENT INTO YELLOW RANGE. ENTERED HOLDING TO RUN ENGINE LIMIT OR SURGE OR STALL QRH. ENGINE WAS UNRESPONSIVE TO POWER SETTINGS AT TIMES. AFTER CYCLING BLEED PER QRH ENGINE WAS WITHIN NORMAL RANGES. UPON DIVERSION TO
- [SDR FDEA202606160765](https://openairdocs.org/sdr/FDEA202606160765.md): Not Reported · not reported · Jun 16, 2026 · N934FD · Boeing 75721B · Wing, Attach Fittings
  > WRI 57-40-5108 FACTED IN ERROR. EA: F-5740-T0387288 P1. CREATED WRI 5740-5115 FOR SDR OF WRI 5740-5108 BEING FACTED IN ERROR. REF MAJOR REPAIR E.A. F-5740-T0387288 P1.
- [SDR FDEA202601280090](https://openairdocs.org/sdr/FDEA202601280090.md): Battery · failed · Jan 28, 2026 · N934FD · Boeing 75721B · Emergency Lighting
  > ON SERVICE CHECK, NOTED CENTER GALLEY EXIT SIGN & R1 DOOR EXIT SIGN, & R1 DOOR SLIDE LIGHT NOT ILLUMINATING ON TEST. R & R FWD GALLEY EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM 33-51-07-2.CENTER GALLEY EXIT LIGHT R1 DOOR EXIT LIGHT & R1 DOOR SLIDE LIGHT OP
- [SDR FDEA202506271069](https://openairdocs.org/sdr/FDEA202506271069.md): Stringer · corroded · Jun 27, 2025 · N934FD · Boeing 75721B · Fuselage Main, Longeron/Stringer
  > DOT 80-059 AFT CARGO COMPARTMENT STR 27R/H JUST AFT OF F/S 1300 @ DOME NUT STRINGER EXFOLIATED. CORROSION FOUND TO BE OUT LIMITS IAW SRM 53-00-03 FIG 101 ACCOMPLISHED WITH 02 E/A STRINGER REPAIR BETWEEN BS 1260 TO BS1280 STR 27 R/H AND BS 1320 STR 27 R/H I
- [SDR FDEA202506271068](https://openairdocs.org/sdr/FDEA202506271068.md): Strap · corroded · Jun 27, 2025 · N934FD · Boeing 75721B · Fuselage Miscellaneous Structure
  > DOT 86-117 AFT CARGO STA 1420, STABILIZER STRAP IN CEILING AT RBL 45, CORRODED. REMOVED STABILIZER STRAP IN CEILING AT RBL 45 AND PEFORMED REPAIR IAW SRM 53-00-51-2R, FABRICATED STRAP ON VTMAE TRAVELER # T25/1820128 IAW SRM 53-00-51-2R, MAJOR REPAIR.
- [SDR FDEA202506251047](https://openairdocs.org/sdr/FDEA202506251047.md): Skin · corroded · Jun 25, 2025 · N934FD · Boeing 75721B · Trailing Edge Flaps
  > DOT 86-84 RH WING IB MAIN FLAP, CORROSION ON UPPER SURFACE EDGE, AT OB JUNCTION OF AFT FLAP. REMOVED, REPAIRED AND REINSTALLED RH WING MAIN FLAP UPPER SURFACE EDGE (WEDGE) AT O/B JUNCTION AT AFT FLAP IAW SRM 51-40-02, SRM 51-70-10-2R REPAIR 4 & SRM 57-53-0
- [SDR FDEA202506241038](https://openairdocs.org/sdr/FDEA202506241038.md): Seat Track · corroded · Jun 24, 2025 · N934FD · Boeing 75721B · Fuselage, Seat/Cargo Attach Fittings
  > UNDER CABIN FLOOR PNL. 242MAF, AROUND MANY SCREWHOLES HAVE SURFACE CORROSION, ON FLOOR STRUCTURE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED AND REPLACED SEAT TRACK FLANGE RBL 24.5 STA. 900-1080 AND FABRICATED SEAT TRACK FLAN
- [SDR FDEA202506211022](https://openairdocs.org/sdr/FDEA202506211022.md): Floor Panel · broken · Jun 21, 2025 · N934FD · Boeing 75721B · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 251 MWF IS BROKEN AND MISSING CORRECT INSERT. FABRICATED MAIN CABIN FLOOR PANEL 251 MWF ON VTMAE TRAVELER T25/1818647 PER DWG 11864182, MAJOR REPAIR.
- [SDR FDEA202506211021](https://openairdocs.org/sdr/FDEA202506211021.md): Floor Panel · damaged · Jun 21, 2025 · N934FD · Boeing 75721B · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252 MWF IS BROKEN AND HAS ALL WRONG INSERTS NOT FLUSH WITH THE PANEL ARE INSTALLED ALL THE WAY THROUGH THE PANEL, NEEDS THE VERY SHALLOW INSERTS PER THE BUILD PRINT FOR THE PANEL. DOT 4-139. FABRICATED MAIN CABIN FLOOR PANEL 252 MWF
- [SDR FDEA202506211020](https://openairdocs.org/sdr/FDEA202506211020.md): Floorboard · damaged · Jun 21, 2025 · N934FD · Boeing 75721B · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 251MVF IS BROKEN. FABRICATED MAIN CABIN FLOORBOARD 251MVF ON VTMAE TRAVELER T25/1818699 PER DWG 11864182, MAJOR REPAIR.
- [SDR FDEA202506191011](https://openairdocs.org/sdr/FDEA202506191011.md): Seat Track · corroded · Jun 19, 2025 · N934FD · Boeing 75721B · Fuselage, Seat/Cargo Attach Fittings
  > CORR. FOUND ON SEAT TRACK LBL 45 FROM 1180 TO 1280 REMOVED, FABRICATED NEW & INSTALLED MAIN CABIN SEAT TRACK FROM STA 1180-1280 LBL 45 PER DWG BAC 1520-792 & SRM 51-40-02, PART MARKED IAW GMM 7-1-1001, MAJOR REPAIR
- [SDR FDEA202506191008](https://openairdocs.org/sdr/FDEA202506191008.md): Strap · damaged · Jun 19, 2025 · N934FD · Boeing 75721B · Fuselage Miscellaneous Structure
  > BROKEN FLANGE STRAP UNDER CABIN FLOOR PNL #222 MDF B STA 396 DOT# 204-16 REMOVED & REPLACED STRAP UNDER FLOOR PANEL #222 MDF AT STA 396 IAW SRM 53-10-51-2R- 1, PARTMARK PER GMM 7-1-1001, STRAP FABRICATED ON VTMAE TRAVELER #T25/1818344 MAJOR REPAIR.
- [SDR FDEA202506191007](https://openairdocs.org/sdr/FDEA202506191007.md): Seat Track · corroded · Jun 19, 2025 · N934FD · Boeing 75721B · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT STA 1189 RBL 58.2 HAS CORROSION AT FASTENER HOLES. DOT 4-142 REMOVED AND REPLACED NEW SEAT TRACK PER DWG BAC1520-792, BATCH #0004393834 FROM BS 920 TO BS 1200 RBL 58.2, TREATED AND PRIMED IAW DWG# BAC1520-792 AND SRM 51-40-02, PART
- [SDR FDEA202506191006](https://openairdocs.org/sdr/FDEA202506191006.md): Crossbeam · corroded · Jun 19, 2025 · N934FD · Boeing 75721B · Fuselage Main, Structure
  > DOT 86-160 STA 1060-1100, LBL 0-24 CORROSION AROUND SCREWHOLES. CROSSBEAM AT BS 1060-1100, BL0-LBL24 CORROSION BEYOND ALLOWABLE LIMITS, REMOVED DAMAGE CROSSBEAM AND REPLACED WITH FABRICATED CROSSBEAM IAW DWG #144N5005, SRM 53-40-51 DETAIL 1 AND SRM 51-40-0
- [SDR FDEA202506130929](https://openairdocs.org/sdr/FDEA202506130929.md): Seat Track · corroded · Jun 13, 2025 · N934FD · Boeing 75721B · Fuselage, Seat/Cargo Attach Fittings
  > DOT 86-158 FLOOR TRACK AT LBL24, STA 1057, CORROSION ON LH FLANGE AT SCREWHOLE. REMOVED AND REPLACED FLOOR TRACK AT LBL 24 STA 1057 IAW SRM 51-40-02 & DWG 111N5202, PARTMARKED PER GMM 7-1-1001, MAJOR REPAIR
- [SDR FDEA202506110921](https://openairdocs.org/sdr/FDEA202506110921.md): Repair · corroded · Jun 11, 2025 · N934FD · Boeing 75721B · Fuselage Main, Structure
  > DOT 80-065 AFT CARGO COMPARTMENT CEILING STRUCTURE. FLOOR BEAM LOWER FLANGE. F/S 1560 APPROX 10 INCHES FROM R/H SIDEWALL BEAM CORRODED REMOVED DAMAGES AT AFT CARGO LWR FLANGE F/S IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A. REPAIRED FLO
- [SDR FDEA202506100886](https://openairdocs.org/sdr/FDEA202506100886.md): Strap · corroded · Jun 10, 2025 · N934FD · Boeing 75721B · Fuselage Miscellaneous Structure
  > DOT 86-118 AFT CARGO STA 1420, STABILIZER STRAP IN CEILING AT RBL 24, CRRODED. REMOVED AND REPLACED STABILIZER IN CEILING STRAP IAW SRM 51-40-02, FABRICATED ON VTMAE TRAVELER T25/1811436 IAW SRM 53-11-51-2R RBL 24 STA 1360-1440, PART MARK PER GMM 7-0-1001,
- [SDR FDEA202506100885](https://openairdocs.org/sdr/FDEA202506100885.md): Seat Track · corroded · Jun 10, 2025 · N934FD · Boeing 75721B · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS CORROSION A STA 1180 TO 1200 RBL 45, DOT 4-141 REMOVED, FABRICATED & INSTALLED NEW MAIN CABIN SEAT TRACK PER DWG BAC 1520-792 STA 1120-STA 1200 RBL 45, P.M. IAW GMM 7-0-1001, MAJOR REPAIR.
- [SDR FDEA202501080035](https://openairdocs.org/sdr/FDEA202501080035.md): Bulb · inoperative · Jan 8, 2025 · N934FD · Boeing 75721B · Door Warning System
  > SLIDE LIGHT WOULD NOT ILLUMINATE WHEN RIGHT ENTRY DOOR WAS ARMED. REPLACED R1 DOOR SLIDE LIGHT BULBS, READY FOR SERVICE.
- [SDR FDEA202401160079](https://openairdocs.org/sdr/FDEA202401160079.md): Probe · failed · Jan 16, 2024 · N934FD · Boeing 757200 · Engine (Turbine/Turboprop)
  > DURING CLIMB OUT AFTER TURNING OFF ENGINE ANTI-ICE THE LEFT ENGINE APPEARED TO NOT PRODUCE THE SAME POWER AS THE RIGHT ENGINE. 7 DEGREES RIGHT RUDDER REQUIRED. EGT WAS NEAR LIMIT WITH ALL OTHER ENGINE INDICATIONS MUCH LESS THAN THE RIGHT. EMERGENCY DEC
- [SDR FDEA202309081563](https://openairdocs.org/sdr/FDEA202309081563.md): Power Supply · failed · Sep 8, 2023 · N934FD · Boeing 757200 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT ABOVE DOOR AND SLIDE LIGHT FAILED TO ILLUMINATE DURING TEST. REMOVED AND REPLACED L1 DOOR POWER SUPPLY AS REQUIRED OPS CKS NORMAL OK FOR SERVICE.
- [SDR FDEA202307181233](https://openairdocs.org/sdr/FDEA202307181233.md): Cylinder · failed · Jul 18, 2023 · N934FD · Boeing 757200 · Emergency Exits
  > L FWD ENT DOOR ARMED FLAG DID NOT FUNCTION. UPON OPENING DOOR THE SLIDE PARTIALLY DEPLOYED. FOUND L1 DOOR OPEN WITH SLIDE HANGING OUT OF DOOR AND ATTACHED TO GIRT BAR, SLIDE WAS NOT DEPLOYED. L1 DOOR ASSIST BOTTLE IS EMPTY. RELEASED FOR SERVICE PE
- [SDR FDEA202306301130](https://openairdocs.org/sdr/FDEA202306301130.md): Unknown · corroded · Jun 30, 2023 · N934FD · Boeing 757200 · Fuselage Main, Structure
  > MAIN CABIN - SEAT TRACK AT STA565 TO 575 LBL24 HAS CORROSION BY FLOOR PANELS HOLES CORROSION ON MAIN SEAT STA 565 TO STA 575 LBL 24 FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A. REMOVED SEAT TRACK FROM STA 440-680 LBL24 IAW B757 SRM 53-00-52-2R, REMO
- [SDR FDEA202306281124](https://openairdocs.org/sdr/FDEA202306281124.md): Skin · worn · Jun 28, 2023 · N934FD · Boeing 757200 · Trailing Edge Flaps
  > L.WING O/B FWD FLAP I/B L/E REINFORCING DOUBLER IS WORN. REPAIRED L/E SKIN ON L.WING O/B MAIN FLAP PER B757 SRM 57-53-01-2R, REPAIR 5
- [SDR FDEA202306261109](https://openairdocs.org/sdr/FDEA202306261109.md): Attach Angle · corroded · Jun 26, 2023 · N934FD · Boeing 757200 · Wing, Attach Fittings
  > L.WING L/E #3 SLAT IS CORRODED ON THE LOWER ATTACH ANGLE FOR COVE SKIN.. REMOVED AND REPLACE #3 SLAT ASSY ON FEDEX N/R N00374 AND HAECO N/R 22374. PER B757 AMM 27-81-02-4.
- [SDR FDEA202306241092](https://openairdocs.org/sdr/FDEA202306241092.md): Slat · dented · Jun 24, 2023 · N934FD · Boeing 757200 · Leading Edge Devices
  > LH WING #5 SLAT LOWER SURFACE OF T/E WEDGE IS DENTED JUST O/B OF I/B AUX TRACK REPAIRED LH WING #5 SLAT LOWER SKIN BY REMOVING DAMAGE AREA AND BONDING FILLER AND DOUBLER REPAIR IAW B757 SRM 57-43-02-2R AND 51-70-10-2R AND FEDEX EA# F-5750-T0374880-P1 - WIN
- [SDR FDEA202306211070](https://openairdocs.org/sdr/FDEA202306211070.md): Panel · cracked · Jun 21, 2023 · N934FD · Boeing 757200 · Wing Miscellaneous Structure
  > LEFT WING FIXED LEADING EDGE SKIN UPPER SURFACE CRACKED IN TWO EACH AREAS AT INBD END OF #3 SLAT. REPAIRED L/H WING FIXED LEADING EDGE SKIN UPPER SURFACE IS CRACKED IN 2 EACH LOACTIONS AT INBD END OF #3 SLAT IAW FED EX B757 SRM 57-41-01-0I, 57-41-01-2R REP
- [SDR FDEA202306181055](https://openairdocs.org/sdr/FDEA202306181055.md): Slat · dented · Jun 18, 2023 · N934FD · Boeing 757200 · Leading Edge Devices
  > LH #5 SLAT, INNER SKIN IS DENTED JUST OUTBD OF INBD AUX TRACK. REPAIRED L/W #5 SLAT COVE PANEL SKIN DENTED AND PUNCTURED IAW B757 SRM 57-43-01-2R REPAIR 3
- [SDR FDEA202306171045](https://openairdocs.org/sdr/FDEA202306171045.md): Skin · burned · Jun 17, 2023 · N934FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE AT STA 1547 BETWEEN S23R & S24R EVALUATED LIGHTNING STRIKE @ STA 1547 BETWEEN S23R & S24R MATL LOSS.010 MATL REMAINING.030 ORIGINAL MATL.040 FOUND TO BE OUT OF LIMITS PER BAC DWG 146N3430 REV - & B757 SR
- [SDR FDEA202306141035](https://openairdocs.org/sdr/FDEA202306141035.md): Flap · delaminated · Jun 14, 2023 · N934FD · Boeing 757200 · Trailing Edge Flaps
  > RIGHT WING I/B FWD FLAP I/B END UPPER SKIN DISBONDED. ACCOMPLISHED PERMANENT REPAIR OF DISBONDED UPPER SKIN ON R/W INBD FLAP BONDED PART 113N2324 IAW B757 57-53-01-2R FIG 201 DETAIL 3 AND SRM 51-70-10-2R-0G.
- [SDR FDEA202306141034](https://openairdocs.org/sdr/FDEA202306141034.md): Door · cracked · Jun 14, 2023 · N934FD · Boeing 757200 · Landing Gear Doors
  > RMLG BODY DOOR IS CRACKED AT THE FWD INBD CORNER OF THE DOOR TANG. REPAIRED RMLG DOOR FWD INBD CORNER OF THE DOOR TANG IAW B757 SRM 52-80-02-2R FIG 201 SHEET 6, SRM51-70-06-0G FIG 1 SHEET 1 AND BOEING DWG 149N6003 #DL PSDL REV -.
- [SDR FDEA202306141033](https://openairdocs.org/sdr/FDEA202306141033.md): Panel · damaged · Jun 14, 2023 · N934FD · Boeing 757200 · Fuselage Structure (General)
  > MAIN CABIN - FLOOR PANEL IS SATURATED WITH HYDRAULIC FLUID AT STA 560 TO STA680 LBL24 TO LBL45. REMOVED AND REPLACED FLOOR PANEL AT STA 560 - 680 LBL 24 - LBL45 IAW B757 AMM 53-01-01-4 AND FEDEX DWG SRZ-25-005 REV R
- [SDR FDEA202306141032](https://openairdocs.org/sdr/FDEA202306141032.md): Panel · damaged · Jun 14, 2023 · N934FD · Boeing 757200 · Fuselage Structure (General)
  > MAIN CABIN - FLOOR PANEL IS SATURATED WITH HYDRAULIC FLUID AT STA 560 TO STA680 LBL 0 TO LBL 24. REMOVED AND REPLACED FLOOR PANEL AT STA 560-680 LBL 0 - LBL 24 IAW B757 AMM 53-01-01-4 AND FEDEX DWG SRZ-25-005 REV R.
- [SDR FDEA202209212353](https://openairdocs.org/sdr/FDEA202209212353.md): Case · corroded · Sep 21, 2022 · N934FD · Boeing 75721B · Turbine Engine Reduction Gear
  > #2 ENGINE LPC CASE HAS EVIDENCE OF CORROSION UNDER THE KEVLAR CONTAINMENT RING OUTER SLEEVE AT THE REAR EDGE FROM APPROX 7:00 POSITION TO THE APPROX 12:00 POSITION 0000280794: SHAEFFER, DAVID C - 21-SEP-2022 22:07 EVALUATED CORROSION AND REPAIRED TEFLON S
- [SDR FDEA202208252049](https://openairdocs.org/sdr/FDEA202208252049.md): Girt Bar · unsecure · Aug 25, 2022 · N934FD · Boeing 75721B · Emergency Equipment
  > FOUND L1 DOOR GIRT BAR LAYING ON CREW STAIRS. FACT 24AUG22 18:26 BNA REINSTALLED L1 DOOR GIRT BAR ASSY. PER AMM 25-66-10-2, ALL OPS CKS GOOD PER AMM
- [SDR FDEA202202020179](https://openairdocs.org/sdr/FDEA202202020179.md): Oil System · overserviced · Feb 2, 2022 · N934FD · Boeing 75721B · Turbine Engine Oil System
  > SUSPECTED FUME EVENT. STRONG DIRTY SOCK SMELL DESCENDING THROUGH 10,000 FT. WHICH LASTED APPROXIMATELY 3 MINUTES. REMOVED HEPA FILTER PERFOMED GVI IT WAS CLEAN AND NO SIGNS OF OIL OR CONTAMINATION. REINSTAILLED HEPA FILTER AFTER VISUAL INSPECTION IAW
- [SDR FDEA2022020320179](https://openairdocs.org/sdr/FDEA2022020320179.md): Unknown · fumes · Feb 2, 2022 · N934FD · Boeing 75721B · Air Distribution System
  > SUSPECTED FUME EVENT. STRONG DIRTY SOCK SMELL DESCENDING THROUGH 10,000 FT. WHICH LASTED APPROXIMATELY 3 MINUTES.
- [SDR FDEA202109162317](https://openairdocs.org/sdr/FDEA202109162317.md): Annunciator · failed · Sep 16, 2021 · N934FD · Boeing 75721B · Landing Gear Position and Warning
  > PDIS 934 32-60 1456 16SEP21 MEM OPEN U ON FINAL 36R KMEM AT 1300 AGL 150 KIAS WITH GEAR LEVER - DOWN RIGHT MAIN NO INDICATION, LEFT MAIN AND NOSE GEAR- DOWN/ GREEN. RAN QRH USED ALT GEAR EXTENSION. ALL 3 GEAR- DOWN/ GREEN. LANDED WITHOUT INC
- [SDR FDEA202107271877](https://openairdocs.org/sdr/FDEA202107271877.md): Dome Nut · corroded · Jul 27, 2021 · N934FD · Boeing 75721B · Fuselage Main, Attach Fittings
  > DAMAGED AND CORRODED DOME NUT PLATES UNDER FLOOR PANEL 242MGF REMOVED DAMAGED CROWN SUPPORT IAW SRM 51-40-02, FABED NEW CROWN SUPPORT IAW BOEING DWG 111N5207 AND SRM 51-10-02, INSTALLED NEW CROWN SUPPORT IAW BOEING DWG 111N5201 AND SRM 51-40-02 STA. 900-10
- [SDR FDEA202107151790](https://openairdocs.org/sdr/FDEA202107151790.md): Floor Panel · damaged · Jul 15, 2021 · N934FD · Boeing 75721B · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VTMAE TRAVELER # T21/1560980 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202107151789](https://openairdocs.org/sdr/FDEA202107151789.md): Floor Panel · damaged · Jul 15, 2021 · N934FD · Boeing 75721B · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 221BF IS BROKEN. FABRICATED ZONE 220 FLOOR BOARD 221BF ON VTMAE TRAVELER # T21/1561021 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202107151788](https://openairdocs.org/sdr/FDEA202107151788.md): Floor Panel · damaged · Jul 15, 2021 · N934FD · Boeing 75721B · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VTMAE TRAVELER # T21/1560977 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202107141775](https://openairdocs.org/sdr/FDEA202107141775.md): Floorboard · delaminated · Jul 14, 2021 · N934FD · Boeing 75721B · Fuselage Floor Panel
  > ZONE 200 FLOOR BOARD 222MDF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MDF ON VT MAE TRAVELER # T21/1560978 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR.
- [SDR FDEA202107141776](https://openairdocs.org/sdr/FDEA202107141776.md): Floorboard · delaminated · Jul 14, 2021 · N934FD · Boeing 75721B · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELERE # T21/1560979 IAW DWG SRZ-25- 005 REV R. MAJOR REPAIR
- [SDR FDEA202103300801](https://openairdocs.org/sdr/FDEA202103300801.md): Adc · failed · Mar 30, 2021 · N934FD · Boeing 75721B · Air Data Computer
  > DECLARED EMERGENCY WITH ATC. LIGHTNING STRIKE, UNRELIABLE AIRSPEED ON CAPT/LEFT SIDE. RAN UNRELIABLE AIRSPEED QRH. LANDED FLAPS 20 REF20.RECEIVED MULTIPLE RANDOM EICAS MSGS ASSOCIATED WITH UNRELIABLE AIRSPEED AND NOT ASSOCIATED WITH URELIABLE AIRSPEED.
- [SDR FDEA202102030299](https://openairdocs.org/sdr/FDEA202102030299.md): Girt Bar · damaged · Feb 3, 2021 · N934FD · Boeing 75721B · Emergency Equipment
  > GIRT BAR NEEDED REPAIR. PIECE FELL OFF DURING CLOSURE ON L1 DOOR. RMV & INSTALL NEW L1 DOOR GIRT BAR IF PLACE REF B757 AMM 25-66-10-2. STILL REQ 52-11-25 25-5 NO. 1 PASS DR GIRT BAR MECHANISM-ADJ/TEST DUR ADJ OF GIRT BAR FND PLAY IN BOTH THE FWD & AFT
- [SDR FDEA202102030275](https://openairdocs.org/sdr/FDEA202102030275.md): Girt Bar · no test · Feb 3, 2021 · N934FD · Boeing 75721B · Emergency Equipment
  > L-1 DOOR FAILED STEP 3 OF E.O. F-5220-7-5000 REV NO. B PS PT3 REF 757 AMM 52-11-20-5, WHILE PERFORMING STEP 3. E.(2), WHEN OUTSIDE HANDLE IS EXTENDED (WITH MODE
- [SDR FDEA202010302721](https://openairdocs.org/sdr/FDEA202010302721.md): Control Unit · worn · Oct 30, 2020 · N934FD · Boeing 75721B · Elevator Control System
  > EXCESSIVE ELEVATOR PLAY, FIRST FEW INCHES OF ELEVATOR YOLK INPUT, A DEAD SPOT WAS NOTED, WHERE THERE WAS VERY LITTLE RESISTANCE OR FEEL. VERY NOTEABLE DURING TO AND LANDING PHASE. PERF CAT I AUTOLAND AS FUNCTION CHECK AND OPERATIONS CHECKED GOOD. REMOVED A
- [SDR FDEA201907031471](https://openairdocs.org/sdr/FDEA201907031471.md): Floorbeam · cracked · Jul 3, 2019 · N934FD · Boeing 75721B · Fuselage Main, Floor Beam
  > CRACK STA. 580 FLOORBEAM LBL 45.50 UPPER CHORD AFT FLANGE. DOT 88-42 COMPLIED WITH EA #: F-5310-T0347950 P1 TITLE: FUSELAGE- MAINFRAME- STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.

Next page: https://openairdocs.org/aircraft/N934FD/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 = 'N934FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N934FD/reports

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