# Service difficulty reports: N939FD

A list on [N939FD](https://openairdocs.org/aircraft/N939FD.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 3 · 141 reports

- [SDR FDEA202608201198](https://openairdocs.org/sdr/FDEA202608201198.md): Battery Pack · failed · Aug 20, 2026 · N939FD · Boeing 75723A · Emergency Lighting
  > INTERIOR EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED FWD BATTERY POWER SUPPLY IAW ABOVE REF. AFTER REPLACMENT FOUND CTR EXIT LIGHT AND R1 EXIT LIGHT OPS CHK SERVICEABLE. L1 DOOR OVERHEAD EXIT LIGHT AND FLT DECK EMER LIGHT INOP. PRESSED COURIER TEST BUT
- [SDR FDEA202606240800](https://openairdocs.org/sdr/FDEA202606240800.md): Unknown · odor · Jun 24, 2026 · N939FD · Boeing 75723A · Air Distribution System
  > AFTER LOWERING MLG THERE WAS A DISTINCT ELECTRICAL BURNING ODOR. EXPERIENCED THIS ABOUT 2 WEEKS AGO ON THIS SAME ACFT. AMM 32-61-00-5 PINNED GEAR & CYCLED GEAR HANDLE WITH HYD APPLIED. ALL INDICATIONS NORMAL IAW AMM, NO ODOR OF OZONE PRESENT. INSPECTED BEH
- [SDR FDEA202605080570](https://openairdocs.org/sdr/FDEA202605080570.md): Skin · damaged · May 8, 2026 · N939FD · Boeing 75723A · Ailerons
  > LH OUTBOARD AILERON TRAILING EDGE HAS DAMAGE, MARKED WITH TAPE. REPAIRED DAMAGE ON L/H O/B AILERON AT WS 796.26 IN REF TO B757 SRM 57-60-01-2R FIG 201 SH 2 AND B757 SRM 51-70-05-0G FIG 5. CALCULATED NEW BALANCE MOMENT FOR L/H O/B AILERON TO BE -12.30 POUND
- [SDR FDEA202604180469](https://openairdocs.org/sdr/FDEA202604180469.md): Fseu · failed · Apr 18, 2026 · N939FD · Boeing 75723A · Trailing Edge Flap Control System
  > WHILE CONFIGURING FOR LANDING, AS WE SELECTED FLAPS 25, WE RECEIVED A TE FLAPS DISAGREE ON EICAS. INDICATOR REMAINED AT FLAPS 20. COMPLIED WITH QRH. RETRACTED FLAPS USING ALTERNATE METHOD. UNEVENTFUL LANDING IN HNL. EMERGENCY DECLARED. RAN FLAPS THROUGH F
- [SDR FDEA202603190358](https://openairdocs.org/sdr/FDEA202603190358.md): Fseu · failed · Mar 19, 2026 · N939FD · Boeing 75723A · Trailing Edge Flap Control System
  > UPON SELECTING FLAPS 25 RECEIVED A TE FLAP DISAGREE EICAS. FLAP HANDLE WAS AT 25 BUT THE FLAPS WERE AT 20. RAN QRH, RETRACTED FLAPS TO UP USING ALT FLAPS AND DIVERTED TO HNL. UNEVENTFUL FLAPS 20 LANDING USING ALT FLAPS. EMERGENCY DECLARED. INTERROGAT
- [SDR FDEA202404030435](https://openairdocs.org/sdr/FDEA202404030435.md): Lamp · burned out · Apr 3, 2024 · N939FD · Boeing 75723A · Emergency Lighting
  > L1 MAIN ENTRY DOOR SLIDE LIGHT IS BURNT OUT. REMOVED AND REPLACED BOTH BULBS AND PERFORMED ADJUSTMENT TEST IAW AMM 52-11-00-2-0, TEST SATIS, A/C OK FOR SERVICE.
- [SDR FDEA202311101847](https://openairdocs.org/sdr/FDEA202311101847.md): Reservoir · leaking · Nov 10, 2023 · N939FD · Boeing 757200 · Emergency Equipment
  > DURING POST FLIGHT INSPECTION, FOUND LEFT PASSENGER DOOR (#1) EMERGENCY POWER RESERVOIR WITH LESS THAN 2000PSI. REPLACED NO. 1 PASSENGER DOOR EMERGENCY POWER RESERVOIR IAW AMM 52-11-30-4. REMOVED PART DETAILS - NAME: RESERVOIR ENTRANCE DOOR EMERGENCY
- [SDR FDEA202309111573](https://openairdocs.org/sdr/FDEA202309111573.md): Fitting · cracked · Sep 11, 2023 · N939FD · Boeing 757200 · Nacelle/Pylon Structure
  > #1 ENG PYLON DRAG FITTINGS REMOVAL REQUIRED PER EA F-5730-T0375771 REPAIR PERFORMED PER EA #F-5730-T0375771 P1 EA TITLE WINGS-PLATES AND SKINS-LH WING UPPER SKIN AT INBOARD PYLON DRAG FITTING, CRACK AND CORROSION INDICATION IN HOLES #1-5,7, AND 9, DURING I
- [SDR FDEA202309111571](https://openairdocs.org/sdr/FDEA202309111571.md): Fitting · cracked · Sep 11, 2023 · N939FD · Boeing 757200 · Nacelle/Pylon Structure
  > #2 ENG PYLON DRAG FITTINGS REMOVAL PER EA ORDER # F-5730-T0375772 REPAIR PERFORMED PER EA # F-5730-T0375772 EA TITLE WINGS-PLATES AND SKINS-RH WING UPPER SKIN AT PYLON DRAG FITTINGS, CRACK AND CORROSION INDICATIONS IN HOLES #3,4,8,9,12,13 AND 15. MAJOR REP
- [SDR FDEA202211292855](https://openairdocs.org/sdr/FDEA202211292855.md): Bulb · inoperative · Nov 29, 2022 · N939FD · Boeing 75723A · Door Warning System
  > MAIN CARGO DECK DOOR CANOPY POSITION LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW SMP, PERFORMED CANOPY POSITION INDICATOR TEST IAW AMM 52-72-02-2. OPS CHECKED OK.
- [SDR FDEA202208121971](https://openairdocs.org/sdr/FDEA202208121971.md): Probe · dirty · Aug 12, 2022 · N939FD · Boeing 757200 · Engine Indicating System
  > PDIS 939 77-15 0226 11AUG22 CDG FACT U ON CLIMB OUT LEFT ENGINE PRODUCED APPROX. 1/3 LESS POWER THAN RIGHT ENGINE. CONTACTED GOC/MOC WITH PARAMETERS AND CONTINUED TO CDG. SHGN 12AUG22 02:09 CDG U FRMFIMFX1 73-21-00-3-0-R PERFORMED: FAULT C
- [SDR FDEA202102050296](https://openairdocs.org/sdr/FDEA202102050296.md): Apu · odor · Feb 5, 2021 · N939FD · Boeing 75723A · Airborne Auxiliary Power Unit (APU) System
  > PDIS 939 21-70 8622 05FEB21 LGG OPEN U LOGPAGES:3301364 OBSERVED AN ACRID, BURNING OIL SMELL DURING ALL PHASES OF FLIGHT WITH MARKED INTENSITY ON APU BLEED, CLIMB AND DESCENTS. EXPIRIENCED WHAT IS DESCRIBED AS A FUME EVENT. SHGN 05FEB21 01:2
- [SDR FDEA202101130073](https://openairdocs.org/sdr/FDEA202101130073.md): Lock · loose · Jan 13, 2021 · N939FD · Boeing 75723A · Emergency Equipment
  > LEFT FWD ENTRY DOOR GIRT BAR IS LOOSE AND NEEDS TO BE RESTOWED. REINSTALLED L/H DOOR GIRT BAR AND GIRT BAR SLIDER WITH HIS PROX SWITCH TARGET AS PER AMM 25-66-10-2. TESTED AS PER SAME AMM, TEST PASSED.
- [SDR FDEA202010122531](https://openairdocs.org/sdr/FDEA202010122531.md): Panel · delaminated · Oct 12, 2020 · N939FD · Boeing 75723A · Horizontal Stabilizer, Plate/Skin
  > DELAMINATION FOUND ON RT HORIZ STAB UPPER PANEL, FWD TORQUE BOX UPPER INBOARD PANEL. PERFORMED A CATEGORY C REPAIR, RESIN INJECTION TO UPPER SUFACE OF RT HORIZ STAB INBOARD PANEL 22" FORM INBOARD EDGE, 5" FROM FWD EDGE, IAW SRM 51-70-10 REPAIR 5.
- [SDR FDEA202008252031](https://openairdocs.org/sdr/FDEA202008252031.md): Seal · leaking · Aug 25, 2020 · N939FD · Boeing 75723A · Aircraft Fuel Distribution System
  > DURING REFUELING FOUND RUNNING FUEL LEAKAGE FROM CENTER TANK (RIGHT WING TO AIR CONDITIONING FAIRING), IAW ENGINEERING (EMAIL) GVI DONE AROUND THE LEAK AREA, NO STRUCTURAL DAMAGE FOUND. ALSO PERFORM CHECK TO FASTENERS FROM OUTSIDE OF THE CENTER TANK AROUND
- [SDR FDEA2020030520480](https://openairdocs.org/sdr/FDEA2020030520480.md): Computer · failed · Mar 2, 2020 · N939FD · Boeing 75723A · Central Computers
  > ON TAXI OUT WE RECEIVED MULTIPLE WARNING AND CAUTIONS TO INCLUDE: GEAR NOT DOWN, SPOILER, APU FIRE, FWD CARGO FIRE. MULTIPLE CAUTIONS WERE PRESENT. THEY LASTED APPROX 1 MIN, THEN STOPPED. APPROX 2 MINS LATER THEY CAME BACK AGAIN. AT THIS POINT WE DECIDED
- [SDR FDEA2019101762663](https://openairdocs.org/sdr/FDEA2019101762663.md): Stringer · damaged · Oct 16, 2019 · N939FD · Boeing 75723A · Fuselage Main, Longeron/Stringer
  > STRINGERS 1 AND 2R @ BS1513 AND BS1507 HAVE INCORRECTLY DRILLED HOLES FOUND DURING ACCOMPLISHMENT OF E.A.#F-2560-150815D.
- [SDR FDEA2019101102589](https://openairdocs.org/sdr/FDEA2019101102589.md): Bracket · cracked · Oct 10, 2019 · N939FD · Boeing 75723A · Nacelle/Pylon, Main Frame
  > NR 2 PYLON AFT LOWER PAN HAD TWO MOUNT BRACKETS CRACKED. REPLACED THE MOUNT BRACKETS IAW SRM 51-40-02.
- [SDR FDEA2019101092531](https://openairdocs.org/sdr/FDEA2019101092531.md): Panel · delaminated · Oct 9, 2019 · N939FD · Boeing 75723A · Horizontal Stabilizer, Plate/Skin
  > DELAMINATION FOUND ON AFT CORNER OF LEFT HORIZONTAL STABILIZER TE PANEL 335EB. REPAIRED THE TE PANEL IAW SRM 51-70-17-0G, PARAGRAPH 4A(2), AND FIG 23 SRM REV 128.
- [SDR FDEA2019101092530](https://openairdocs.org/sdr/FDEA2019101092530.md): Retainer · corroded · Oct 9, 2019 · N939FD · Boeing 75723A · Wing Main, Frame Structure
  > RIGHT WING UPPER FIXED TE AREA OUTBOARD OF AILERON ACTUATORS, FIXED TE SEAL RETAINER CORRODED. THE SEAL RETAINER WAS REPLACED IAW DRAWING 113N1640 AND GMM 7-0-1001.
- [SDR FDEA2019101082492](https://openairdocs.org/sdr/FDEA2019101082492.md): Support Angle · damaged · Oct 8, 2019 · N939FD · Boeing 75723A · Cargo/Baggage Doors
  > FORWARD CARGO DOOR ANGLE SUPPORT DAMAGED AT LOWER FORWARD DOORSTOP AREA. REPLACED ANGLE SUPPORT (BRACKET) IAW SRM 51-40-02, BOEING DRAWING 140N2891 AND GMM 07-0-1001.
- [SDR FDEA201910072482](https://openairdocs.org/sdr/FDEA201910072482.md): Support Bracket · cracked · Oct 7, 2019 · N939FD · Boeing 75723A · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON AFT FAIRING AREA SUPPORT BRACKET CRACKED, BELOW FLOW LIMITER, REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, REV 128, AND DRAWING 313N5021.
- [SDR FDEA201910072481](https://openairdocs.org/sdr/FDEA201910072481.md): Floor Panel · damaged · Oct 7, 2019 · N939FD · Boeing 75723A · Fuselage Floor Panel
  > FLOOR PANEL, BS 560 - 680, RT OTBD WAS DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50, REV 128.
- [SDR FDEA201910072480](https://openairdocs.org/sdr/FDEA201910072480.md): Skin · scratched · Oct 7, 2019 · N939FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > SURFACE SCRATCHES ON THE FUSELAGE SKIN AT BS 900 - 920. FOUND TO BE OUTSIDE PERMITTED LIMITS. REPAIRED IAW EA F-5330-T0349853 P (1).
- [SDR FDEA201909262602](https://openairdocs.org/sdr/FDEA201909262602.md): Beam · corroded · Sep 26, 2019 · N939FD · Boeing 75723A · Fuselage Main, Structure
  > FWD CARGO DOOR LOWER EDGE BEAM AND SPLICES FOUND CORRODED REMOVED CORROSION IAW SRM 52-30-02-1A FIG 101 DETAIL IV AND FOUND TO BE OUT OF LIMITS.MAX ALLOWABLE BLENDOUT = 0.012" ACTUAL BLENDOUT =.029". REPLACED LOWER EDGE BEAM AND SPLICES IAW SRM 51-40-02 A
- [SDR FDEA2019101122585](https://openairdocs.org/sdr/FDEA2019101122585.md): Skin · corroded · Sep 26, 2019 · N939FD · Boeing 7572T7 · Cargo/Baggage Doors
  > FWD CARGO DOOR LOWER SKIN CORROSION ON INTERNAL SKIN REMOVED CORROSION ON LOWER INNER SKIN AT LOCATIONS 12" AND 18" FROM FORWARD EDGE AND 12" FROM AFT EDGE AND FOUND TO BE OUTSIDE LIMITS IAW SRM 52-30-01-1A FIG 101 DETAIL V, MAX ALLOWABLE BLEND = 0.006"
- [SDR FDEA201909172293](https://openairdocs.org/sdr/FDEA201909172293.md): Gate · corroded · Sep 17, 2019 · N939FD · Boeing 75723A · Passenger/Crew Doors
  > DOOR 2L UPPER GATE HAS EVIDENCE OF PITTING AT HINGE LINE AT EXTERIOR SURFACE. DOOR 2L UPPER GATE REPLACED IAW DWG #146N6105.
- [SDR FDEA2019101462611](https://openairdocs.org/sdr/FDEA2019101462611.md): Skin · delaminated · Sep 16, 2019 · N939FD · Boeing 75723A · Horizontal Stabilizer, Plate/Skin
  > RIGHT STAB HAS UPPER SURFACE DELAMINATION IN AREA JUST ADJACENT TO THE FUSELAGE, RT HORIZONTAL STABILIZER UPPER INBOARD FIXED LE PANEL MPN.185N3001-50 REPAIRED IAW EA F-5510-T0349726.
- [SDR FDEA2019091432634](https://openairdocs.org/sdr/FDEA2019091432634.md): Skin · delaminated · Sep 13, 2019 · N939FD · Boeing 75723A · Trailing Edge Flaps
  > THE R/H I/B MAIN FLAP LOWER SURFACE PANEL 113N2402-4 HAS DELAM AND REQUIRES REPAIR REPAIRED THE R/H I/B MAIN FLAP LOWER SURFACE PANEL IAW SRM 57-53-01-0I FIG 1, SRM 57-53-01-2R FIG 201 AND SRM 51-70-10-2R FIG 201 DETAIL A USING INSTRUCTIONS IN REPAIR P
- [SDR FDEA2019101092534](https://openairdocs.org/sdr/FDEA2019101092534.md): Skin · worn · Sep 13, 2019 · N939FD · Boeing 75723A · Trailing Edge Flaps
  > RIGHT WING OTBD FLAP UPPER INBD PANEL WAS WORN FROM MAKING CONTACT WITH THE NUMBER 10 SPOILER. REPAIRED IAW EA F-5750-T0349728 P1.
- [SDR FDEA201909132356](https://openairdocs.org/sdr/FDEA201909132356.md): Skin Panel · corroded · Sep 13, 2019 · N939FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS EVIDENCE OF CORROSION ON INNER SURFACE AT APU INLET DOOR PANEL FORWARD ATTACHMENT AREA CORROSION FOUND TO BE OUTSIDE LIMITS,SKIN PANEL REPLACED IAW BOEING DWG # 148N3105 AND SRM 51-40-02.
- [SDR FDEA201909132355](https://openairdocs.org/sdr/FDEA201909132355.md): Support Angle · corroded · Sep 13, 2019 · N939FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > APU INLET DOOR PANEL SUPPORT ANGLE CORRODED AT LOWER FORWARD CUTOUT BS1792 APU INLET DOOR PANEL SUPPORT ANGLE REPLACED IAW BOEING DWG #148N3105 AND SRM 51-40-02, DUE TO CORRODED BEYOND LIMITS.
- [SDR FDEA2019101402612](https://openairdocs.org/sdr/FDEA2019101402612.md): Skin · dented · Sep 10, 2019 · N939FD · Boeing 75723A · Leading Edge Devices
  > NR 5 SLAT LEADING EDGE DAMAGED. REPAIRED IAW SRM 57-43-01-2R REPAIR 9 FIG 201 DETAIL VII AND EA F-5750-T0349924 P1.
- [SDR FDEA2019101192588](https://openairdocs.org/sdr/FDEA2019101192588.md): Support · corroded · Sep 9, 2019 · N939FD · Boeing 7572T7 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR EVIDENCE OF BULGING OF LEVELING COMPOUND AT LOWER DOOR AREA REMOVED LEVELLING COMPOUND, CORROSION FOUND AT LOWER DOOR INNER SKIN,EDGE BEAM AND SPLICES, AND TEE SUPPORTS AT BS 580, BS 589 AND BS 600. COROSION REMOVED AT DOOR INNER SKIN
- [SDR FDEA2019101192587](https://openairdocs.org/sdr/FDEA2019101192587.md): Tee Fitting · corroded · Sep 9, 2019 · N939FD · Boeing 7572T7 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR EVIDENCE OF CORROSION ON DOOR INNER SKIN AT LOWER CUTOUT AREA 12" FROM FORWARD EDGE OF CARGO DOOR COROSION REMOVED AT DOOR INNER SKIN AT LOWER CUTOUT AREA LOCATED 12" FROM FORWARD EDGE OF DOOR AND,AREA FOUND TO BE OUTSIDE LIMITS IAW SRM
- [SDR FDEA2019101192586](https://openairdocs.org/sdr/FDEA2019101192586.md): Skin · corroded · Sep 9, 2019 · N939FD · Boeing 7572T7 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR EVIDENCE OF CORROSION ON DOOR INNER SKIN AT LOWER CUTOUT AREA 12" FROM AFT EDGE OF CARGO DOOR COROSION REMOVED AT DOOR INNER SKIN AT LOWER CUTOUT AREA LOCATED 12" FROM AFT EDGE OF DOOR AND,AREA FOUND TO BE OUTSIDE LIMITS IAW SRM 52-30-01
- [SDR FDEA201909092475](https://openairdocs.org/sdr/FDEA201909092475.md): Skin · gouged · Sep 9, 2019 · N939FD · Boeing 75723A · Horizontal Stabilizer, Plate/Skin
  > LEFT STAB CUT-OUT LOWER SKIN HAD GOUGES AT 10.5, 22, 33, AND 43.5 INCHES FROM THE FWD EDGE. EVALUATED AND FOUND THE GOUGES AT 10.5 AND 22 INCHES WERE OUT OF LIMITS IAW SRM 53-80-70-1A, FIG 101, DETAIL VI. REPAIRED IAW SRM 53-80-70-2R, REPAIR 2.
- [SDR FDEA2019100792445](https://openairdocs.org/sdr/FDEA2019100792445.md): Rib · corroded · Sep 9, 2019 · N939FD · Boeing 75723A · Wing, Rib/Bulkhead
  > RIGHT AILERON ATTACHMENT RIB AT WING STA 810 WAS CORRODED AT BONDING LEAD ATTACHMENT. CORROSION REMOVED IAW SRM 51-10-02 AND EVALUATED IAW SRM 57-51-09-1A FIG 101 SHEET 5,NOTE K,DETAIL IV AND VI AND FOUND TO BE OUTSIDE SRM LIMITS,ORIGINAL THICKNESS = 0.
- [SDR FDEA201909092349](https://openairdocs.org/sdr/FDEA201909092349.md): Skin · gouged · Sep 9, 2019 · N939FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > BLEND IN FUSELAGE SKIN AROUND FASTENER AT BS1350 BETWEEN S5L AND S6L MEASURED AND EVALUATED PREVIOUS BLEND ON FUSELAGE SKIN AT BS 1350 BETWEEN S.5L AND S.6L IAW SRM 53-00-01-1A, FIG 101 DETAIL III AND FOUND TO BE OUT OF LIMITS. CARRIED OUT SMALL HOLE FLUSH
- [SDR FDEA2019100762476](https://openairdocs.org/sdr/FDEA2019100762476.md): Skin · worn · Sep 6, 2019 · N939FD · Boeing 75723A · Horizontal Stabilizer, Plate/Skin
  > WEAR FOUND ON THE SKIN PANEL FWD SIDE OF HORIZONTAL STAB CUT OUT LT SIDE AT THE BRACKET MOUNTED ON LWR LONGERON. EVALUATED THE SKIN PANEL AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-80-70-1A DETAIL VI. AREA REPAIRED IAW SRM 53-80-70-2R, REPAIR 4.
- [SDR FDEA2019101042495](https://openairdocs.org/sdr/FDEA2019101042495.md): Bracket · corroded · Sep 4, 2019 · N939FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > BRACKET ON AFT SIDE OF BULKHEAD BS 1787, UPPER SIDE OF APU INTAKE DUCT WAS CORRODED. BRACKET FABRICATED IAW DWG 148N3141 AND INSTALLED IAW SRM 51-40-02.
- [SDR FDEA201909042358](https://openairdocs.org/sdr/FDEA201909042358.md): Support Angle · corroded · Sep 4, 2019 · N939FD · Boeing 75723A · Fuselage Main, Attach Fittings
  > STRAP ON LOWER SIDE OF APU INTAKE DUCT BS 1787-1825 IS CORRODED RECTIFY REMOVED AND REPLACED APU INTAKE LOWER SUPPORT ANGLE (STRAP), IAW BOEING DWG #148N3105 AND SRM 51-40-02.
- [SDR FDEA2019100732456](https://openairdocs.org/sdr/FDEA2019100732456.md): Skin · cracked · Sep 3, 2019 · N939FD · Boeing 75723A · Passenger/Crew Doors
  > UPPER HINGE CUTOUT R2 DOOR HAD A SUPECTED CRACK ON THE LOWER CORNER. A REPAIR WAS CARRIED OUT IAW SRM 52-10-02-2R, REPAIR 1, FIG 201, AND EA F-52-10-T0349827 P1.
- [SDR FDEA201909032111](https://openairdocs.org/sdr/FDEA201909032111.md): Filler · nicked · Sep 3, 2019 · N939FD · Boeing 75723A · Fuselage Main, Frame
  > SMALL MARK (NICK) FOUND ON UPPER AFT EDGE OF FRAME AT BSTA 231.25 BL 0. REMOVED DAMAGED FILLER OF PREVIOUS REPAIR AND REPLACED FILLER IAW SRM 53-00-07 REPAIR 7.
- [SDR FDEA201904260925](https://openairdocs.org/sdr/FDEA201904260925.md): Warning Message · false activation · Apr 26, 2019 · N939FD · Boeing 75723A · Cabin Pressure Control System
  > CLIMBING OUT OF FL 300 WE RECEIVED AN EICAS "CAB ALT" MESSAGE. CABIN ALTITUDE EXCEEDED 10,000 FT. AS INDICATED BY THE CABIN ALT INDICATOR, WE COMPLIED WITH PHASE ONE ITEMS, DONNEP THE OXYGEN MASKS AND INITIATED A DESCENT TO 10,000 FT. WE COMPLIED WITH CAB
- [SDR FDEA201902130401](https://openairdocs.org/sdr/FDEA201902130401.md): Counterbalance · defective · Feb 13, 2019 · N939FD · Boeing 75723A · Passenger/Crew Doors
  > L1 DOOR IS BINDING WHEN OPENING UNSAFE. R&R COUNTERBALANCE ASSY PER MM 52-11-11-4. ALSO R&R SNUBBER ASSY ROTARY PER MM 52-11-10-4.
- [SDR FDEA201901170163](https://openairdocs.org/sdr/FDEA201901170163.md): Not Reported · malfunctioned · Jan 17, 2019 · N939FD · Boeing 75723A · Passenger/Crew Doors
  > PDIS 939 52-10 6607 17JAN19 VIE OPEN U LOGPAGES:3019080 ENTRY DOOR 1L WOULD NOT FULLY OPEN MEL 17JAN19 20:56 VIE U RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 20JAN19 "MEL 52-11-01-A: L1 DOOR - INOP C/7171035 L1 FACT
- [SDR FDEA201811263371](https://openairdocs.org/sdr/FDEA201811263371.md): Hinge · lack of lube · Nov 26, 2018 · N939FD · Boeing 75723A · Passenger/Crew Doors
  > DURING TRANSIT CHECK UNABLE TO OPEN L1 ENTRY DOOR MORE THAN 45 DEGREES. PERFORMED A VISUAL INSPECTION OF R1 DOOR IAW AMM 52-11-00-6. LUBRICATED HINGE POINTS AND MECHANISMS, PERFORMED DOOR FAST CHECK IAW AMM 52-11-00-6. ALL TEST OK AND DOOR OPEN AND CLOSED NOR
- [SDR FDEA201809192592](https://openairdocs.org/sdr/FDEA201809192592.md): Intercostal · corroded · Sep 19, 2018 · N939FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 1037-1060 AT BL 65 LT SIDE IS CORRODED. REPLACED INTERCOSTAL AT BS 1037-1060 AT BL 65 LT SIDE IAW SRM 51-40-02 REV 125.
- [SDR FDEA201809192591](https://openairdocs.org/sdr/FDEA201809192591.md): Bracket · cracked · Sep 19, 2018 · N939FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > 198AR FWD BRACKET HAS SUSPECT CORROSION EVA OF BRACKET WAS FOUND TO BE CRACKED AND OUT OF LIMITS PER SRM 51-40-02. FABRICATED NEW BRACKET PN:149N7553-26 IAW GMM 7-0-1001 REV 150 AND DRAWING 149N7553 SHEET 2 REV A AND AMM 51-21-00 REV 122. INSTALLED NEW BRACKET

Next page: https://openairdocs.org/aircraft/N939FD/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 = 'N939FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N939FD/reports

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