# Service difficulty reports: N938FD

A list on [N938FD](https://openairdocs.org/aircraft/N938FD.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 2 · 87 reports

- [SDR FDEA202310301815](https://openairdocs.org/sdr/FDEA202310301815.md): Static Inverter · burned · Oct 30, 2023 · N938FD · Boeing 757200 · AC Inverter
  > MDIS 938 24-22 9631 30OCT23 IND FACT U UPON POWERING UP AIRCRAFT, NOTICED AN ACRID SMELL IN COCKPIT WITH ASSOCIATED STBY INVERTER EICAS MSG. PART 30OCT23 16:24 MC1 U IDENTIFIED PARTS STATIC INVERTER MPN: 1-002-0102-2090 CPN: 2413802
- [SDR FDEA202307271317](https://openairdocs.org/sdr/FDEA202307271317.md): Unknown · sheared · Jul 27, 2023 · N938FD · Boeing 757200 · Landing Gear System
  > MDIS 938 32-42 9432 27JUL23 BUR FACT U AT PUSHBACK #7 MLG TIRE BLEW, UPON INSPECTION FOUND EIGHT TIE BOLTS HAD SHEARED OFF. 5 R/I 27JUL23 04:06 BUR U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 160N0001-38
- [SDR FDEA202304070588](https://openairdocs.org/sdr/FDEA202304070588.md): Skin · damaged · Apr 7, 2023 · N938FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > R/H EXTERIOR FUSELAGE SKIN DOUBLER HAS 2EA DENTS BETWEEN BS 540 AND BS 560 AND STRINGER S-22R AND STRINGER S23R REPAIRED PER FEDEX EA # F-5330-165083-P3
- [SDR FDEA202304060575](https://openairdocs.org/sdr/FDEA202304060575.md): Angle · corroded · Apr 6, 2023 · N938FD · Boeing 757200 · Fuselage Structure (General)
  > AREA OF AFT CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE AND NUTSTRIP ARE CORRODED BETWEEN STA 1701 AND 1720 APPROX RBL 13 REMOVED AND REPLACED ANGLE (FLOOR SUPPORT) AND NUTPLATE STRIP IAW BAC DWG 146N5300 REC C 140N2524 REV A, B757 SRM 51-40-02
- [SDR FDEA202304060573](https://openairdocs.org/sdr/FDEA202304060573.md): Angle · corroded · Apr 6, 2023 · N938FD · Boeing 757200 · Fuselage Structure (General)
  > AREA OF THE BULK CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE AND NUTSTRIP ARE CORRODED BETWEEN STA 1701 AND 1720 APPROX LBL5 REMOVED AND REPLACED ANGLE ( FLOOR SUPPORT) WITH NUTPLATE STRIP IAW BAC DWG 146N5300 REV C 140N2524 REV A B757 SRM
- [SDR FDEA202304060572](https://openairdocs.org/sdr/FDEA202304060572.md): Angle · corroded · Apr 6, 2023 · N938FD · Boeing 757200 · Fuselage Structure (General)
  > AREA AFT OF THE BULK CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE & NUT STRIP ARE CORRODED BETWEEN STA 1701 & 1720 APPROX RBL 5 REMOVED AND REPLACED FLOOR SUPPORT AND NUTPLATE STRIP IAW B757 SRM 51-40-02-0G AND BAC DWG 146N5300 REV C AND 140N2524
- [SDR FDEA202304060571](https://openairdocs.org/sdr/FDEA202304060571.md): Panel · delaminated · Apr 6, 2023 · N938FD · Boeing 757200 · Wing, Plate/Skin
  > R.WING L/E PANEL 611DB HAS COMPOSITE DAMAGE ON MULTIPLE AREAS. ACCOMPLISHED PERMANENT REPAIR ON R/W L/E PANEL 611DB COMPOSITE DAMAGE PER B757 SRM 57-41-01-4R, 51-70-08-0G AND FIG 201, AND BOEING DWG 114N1523 REV D
- [SDR FDEA202304060570](https://openairdocs.org/sdr/FDEA202304060570.md): Panel · delaminated · Apr 6, 2023 · N938FD · Boeing 757200 · Nacelle/Pylon Structure
  > #1 PYLON PANEL 432AL AFT 2 CORNERS ARE DELAMINATED AND DAMAGED. ACCOMPLISHED PERMANENT REPAIR OF PANEL PER B757 SRM 51-40-02, 54-50-70-0G, 51-70-17-0G AND BOEING DWG 313N5003.
- [SDR FDEA202303300525](https://openairdocs.org/sdr/FDEA202303300525.md): Strap · cracked · Mar 30, 2023 · N938FD · Boeing 757200 · Engine Thrust Reverser
  > #2 ENG I/B T/R L/E RADIAL STRAP IS CRACKED AT APPROX 8 0CLOCK POS. REMOVED AND REPLACED PER B757 AMM 78-31-20-8
- [SDR FDEA202302090243](https://openairdocs.org/sdr/FDEA202302090243.md): Unknown · unknown · Feb 9, 2023 · N938FD · Boeing 757200 · Passenger/Crew Doors
  > PDIS 938 52-10 9099 09FEB23 PHX FACT U ON FO S PRE-FLIGHT FO DISCOVERED R1 DOOR SLIDE CABLE EXPOSED. CALLED MX TO VERIFY AND CHECK THAT IT WOULD NOT CATCH ON THRESHOLD, AND POTENTIALLY DEPLOY SLIDE. FACT 09FEB23 17:52 MEM U AMM: 25-66
- [SDR FDEA202206011356](https://openairdocs.org/sdr/FDEA202206011356.md): Survival Kit · out of position · Jun 1, 2022 · N938FD · Boeing 757200 · Emergency Equipment
  > R1 DOOR EMERGENCY SLIDE SURVIVAL KIT STRAP NOT STOWED PROPERLY. REMOVED SLIDE COVER AND PROPERLY STOWED THE R1 DOOR EMERGENCY SLIDE SURVIVAL KIT STRAP AND INSTALLED THE SLIDE COVER IAW B757 AMM: 25-66-01-4.
- [SDR FDEA202205101167](https://openairdocs.org/sdr/FDEA202205101167.md): Girt Bar · dirty · May 10, 2022 · N938FD · Boeing 75723A · Emergency Equipment
  > PDIS 938 25-60 8387 10MAY22 SJO FACT U ENTRY DOOR KNUCKLE BUSTER WILL NOT DEPLOY WHEN ARMING DOOR. FACT 10MAY22 01:43 SJO U INSPECTED L1 ENTRY DOOR AND REMOVED DEBRIS FROM GIRT BAR, PERFORMED OPS CK IAW AMM 25-66-10-2. ALL CKS NORM
- [SDR FDEA202203030406](https://openairdocs.org/sdr/FDEA202203030406.md): Hose · failed · Mar 3, 2022 · N938FD · Boeing 757200 · Hydraulic System, Main
  > L HYD QTY L HYD SYS PRESS TE FLAP DISAGREE COMPLIED WITH QRH, DECLARED EMERGENCY. LANDED RWY 31, SHUTDOWN ON RWY. PERFORMED EDP INSPECTION/CHECK REF AMM 29-11-05-6...NO CONTAMINATION FOUND...REPLACED EDP PRESSURE & CASE DRAIN FILTERS REF AMM 29-11-00-
- [SDR FDEA202105051128](https://openairdocs.org/sdr/FDEA202105051128.md): Seat Track · corroded · May 5, 2021 · N938FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > DOT# 106-12, MAIN CARGO COMPT APPROX. STA. 1340, RBL 45.50 SEAT TRACK HAS CORROSION. CUT OUT DAMAGE SEAT TRACK FROM STA 1300 TO STA 1350 RBL 45.5 IAW SRM 53-00-52-2R, REPAIR SEAT TRACK IAW SRM 53-00-52-2R. (INSTALLED NEW SEAT TRACK SECTION) MAJOR REPAIR.
- [SDR FDEA202105051119](https://openairdocs.org/sdr/FDEA202105051119.md): Floor Panel · delaminated · May 5, 2021 · N938FD · Boeing 75723A · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221BF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221BF ON VTMAE TRAVELER #T21/1548308 IAW FEDEX DWG. DWG. NO. SRZ-25-005 REV. R CAT "A" MAJOR REPAIR.
- [SDR FDEA202105051118](https://openairdocs.org/sdr/FDEA202105051118.md): Floor Panel · delaminated · May 5, 2021 · N938FD · Boeing 75723A · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221AF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221AF ON VTMAE TRAVELER #T21/1548307 IAW FEDEX DWG DWG NO. SRZ-25-005 REV R. CAT "A" MAJOR REPAIR.
- [SDR FDEA202105051117](https://openairdocs.org/sdr/FDEA202105051117.md): Floor Panel · delaminated · May 5, 2021 · N938FD · Boeing 75723A · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222MAF DELAMINATED. FABRICATED FLOOR PANEL 222MAF ON VTMAE TRAVELER #T21/1548305 IAW DWG SRZ-25-005 REV REV R CAT "A" MAJOR REPAIR.
- [SDR FDEA202105051116](https://openairdocs.org/sdr/FDEA202105051116.md): Floor Panel · delaminated · May 5, 2021 · N938FD · Boeing 75723A · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221MBF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221MBF ON VTMAE TRAVELER #T21/1548304 IAW DWG SRZ- SRZ-25-005 REV R CAT "A" MAJOR REPAIR.
- [SDR FDEA202105051114](https://openairdocs.org/sdr/FDEA202105051114.md): Floor Panel · delaminated · May 5, 2021 · N938FD · Boeing 75723A · Fuselage Floor Panel
  > COURIER 222AF FLOOR PANEL DELAMINATED. FABRICATED 222AF COURIER FLOOR PANEL ON VTMAE TRAVELER #T21/1548306 IAW DWG SRZ-25- SRZ-25-005 REV R, CAT "A" MAJOR REPAIR.
- [SDR FDEA2020071311485](https://openairdocs.org/sdr/FDEA2020071311485.md): Unknown · malfunctioned · Jul 11, 2020 · N938FD · Boeing 75723A · External Power System
  > DURING POWER TRANSFER ON SHUTDOWN, ALL SCREENS WENT BLANK AND LEFT ENGINE POWER WAS INCREASING WITH THE THRUST LEVER AT IDLE. BLOCK IN FUEL 10.0 CREW DEBRIEFED AND STATED EXTERNAL POWER LATCHED ON AT FIRST AND BECAME UNSTABLE, THEN STABILIZED. PERFORMED BPCU
- [SDR FDEA2020021070284](https://openairdocs.org/sdr/FDEA2020021070284.md): Valve · leaking · Feb 7, 2020 · N938FD · Boeing 75723A · Cabin Pressure Control System
  > 30 MINUTES INTO FLIGHT AT FL340 EXPERIENCED "CABIN ALTITUDE" ALERT. NOTED A DIFFERENTIAL OF 6.0 WITH CABIN ALT OF 11,000. RAN QRH AND PROCEEDED TO KICT AT 10.000 FT.. MODE SELECTOR WAS IN AUTO 1 WHEN THIS OCCURED.
- [SDR FDEA202002070280](https://openairdocs.org/sdr/FDEA202002070280.md): Selector · failed · Feb 7, 2020 · N938FD · Boeing 75723A · Cabin Pressure Control System
  > CABIN ALTITUDE WARNING ANNUNCIATED AT CRUISE FL370. VERIFIED CABIN ALT, DON MASKS. QRH COMPLIED WITH DECENT TO 15,000. CABIN PRES STABILIZED. CLIMBED TO FL250 CABIN REMAINED STABLE. WITH OUTFLOW VALVE SHOWING FULL CLOSED, CABIN STILL CLIMBED USING AUTO1 O
- [SDR FDEA201904180847](https://openairdocs.org/sdr/FDEA201904180847.md): Stringer · gouged · Apr 18, 2019 · N938FD · Boeing 75723A · Fuselage Main, Longeron/Stringer
  > STRINGER 1 HAS EXISTING GOUGE NEAR HILOCK COLLAR APPOX STA. 1505 AND ELONGATED FASTENER HOLE AT EXISTING HILOCK APPROX STA. 1515. CUT OUT DAMAGED SECTION OF MAIN CABIN STRINGER 1 FROM STA.1505 TO STA.1554, FABRICATED NEW STRINGER SECTION & REPAIR SPLICES 2EA,
- [SDR FDEA2018102973033](https://openairdocs.org/sdr/FDEA2018102973033.md): Shutoff Valve · malfunctioned · Oct 27, 2018 · N938FD · Boeing 75723A · Pneumatic Distribution System
  > CABIN ALT WANING -LOSS OF PRESSURIZATION AT FL310 ON CLIMB OUT. HAD MEL 77-12-03 (N3 TACHOMETER NR 1 ENG) AND RAN QRH FOR L ENG BLEED OFF EICAS MSG. APPROX 10 MINS LATER LOSS ALL CABIN PRESS, AFTER EMERG DESCEND TO 12000 (FOR TERRAIN). I TURNED L PACK BACK ON-
- [SDR FDEA201710213022](https://openairdocs.org/sdr/FDEA201710213022.md): Control Unit · failed · Oct 21, 2017 · N938FD · Boeing 75723A · Drag Control System
  > SPOILER ALERT ILLUMINATED ON THE EICAS AND OVERHEAD. ALL HYDRAULICS GOOD. NO ROLL OR BUFFET. PERFORMED BITE TEST OF THE SMCS AND FOUND 2R SCM FAULT ON THE LAST 2 FLIGHT LEGS IAW FIM 27-09, FT807. REMOVED AND REPLACED THE R2 SCM IAW AMM 27-09-00-2. OPS CH
- [SDR FDEA201710132926](https://openairdocs.org/sdr/FDEA201710132926.md): Actuator · missing · Oct 13, 2017 · N938FD · Boeing 75723A · Emergency Equipment
  > SLIDE LIGHT ABOVE THE R1 DOOR FOUND INOPERATIVE WITH DOOR CLOSED AND SLIDE HANDLE IN ARMED POSITION. FOUND THE PROXIMITY SENSOR -A S10216. PROXIMITY ACTUATOR MISSING FROM THE GIRT BAR. INSTALLED A NEW PROXIMITY ACTUATOR. OPS CHECKED GOOD IAW AMM 25-66-11-
- [SDR FDEA201706131635](https://openairdocs.org/sdr/FDEA201706131635.md): Indicator · obstructed · Jun 13, 2017 · N938FD · Boeing 75723A · Emergency Equipment
  > ARMING INDICATION IS NOT POPPING OUT CORRECTLY. IT WAS CORRECTLY INDICATING AT PUSH BACK. BUT TOOK A FEW TRIES. FOUND THAT THE L1 DOOR ARM INDICATOR STICKER WAS SNAGGING ON THE DOOR COVER EDGE. CLEANED STICKER AND CLEANED THE OPENING EDGE ON THE DOOR L
- [SDR FDEA201704281295](https://openairdocs.org/sdr/FDEA201704281295.md): Stiffener · cracked · Apr 28, 2017 · N938FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > RT WW AFT PRESSURE BULKHEAD LWR INBD STIFFENER CRACKED. REMOVED THE STIFFENER LOCATED, DRILLED NEW AND INSTALLED IAW SRM 51-40-02-0G AND SRM 51-40-05-0G.
- [SDR FDEA201704281293](https://openairdocs.org/sdr/FDEA201704281293.md): Stiffener · cracked · Apr 28, 2017 · N938FD · Boeing 757223 · Fuselage Miscellaneous Structure
  > LEFT MLG WW AFT PRESSURE BULKHEAD LOWER INBD STIFFENER CRACKED. REMOVED THE STIFFENER. LOCATED, DRILLED A NEW STIFFENER AND INSTALLED IAW SRM 51-40-02-0G, AND SRM 51-40-05-0G.
- [SDR FDEA201704201244](https://openairdocs.org/sdr/FDEA201704201244.md): Skin · dented · Apr 20, 2017 · N938FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS THREE PROTUDING DENTS IN EXTERNAL SKIN LOWER FUSELAGE AT BS 520 AND TWO INCHES INBD OF STRINGER 26L. SKIN REPAIRED IAW EA F-5330-T0332752 P1.
- [SDR FDEA201612304580](https://openairdocs.org/sdr/FDEA201612304580.md): Module · inoperative · Dec 30, 2016 · N938FD · Boeing 75723A · Autopilot System
  > DURING DECENT, AUTOPILOT FAILED TO CAPTURE ALTITUDE (5000'). ALT WARNING WORKED. R&R THE STAB TRIM ASSY MODULE, PASSES MCDP TEST 65 AS WELL AS MCDP GROUND TEST 30 AND AUTOLAND TEST 40. RESET 30 DAY TIMER, OK FOR SERVICE. IAW AMM 27-09-00-2, 22-00-00-2.
- [SDR FDEA201507082177](https://openairdocs.org/sdr/FDEA201507082177.md): Switch · stuck · Jul 8, 2015 · N938FD · Boeing 75723A · Door Warning System
  > WHILE TROUBLESHOOTING ACARS SYS, FOUND L1 DOOR SWITCH S10094 STUCK IN THE CLOSED POSITION. OPERATIONS CHECKED OK.
- [SDR FDEA201504161244](https://openairdocs.org/sdr/FDEA201504161244.md): Doubler · damaged · Apr 16, 2015 · N938FD · Boeing 75723A · Fuselage Main, Bulkhead
  > APU FWD BULKHEAD RT SIDE HAS A DAMAGED AND GOUGED PREVIOUS REPAIR. REMOVED DAMAGE DOUBLER IAW SRM 51-40-02, FABRICATED NEW DOUBLER IAW SRM 53-80-08-2R, INSTALLED NEW DOUBLER AFT APU FWD BULKHEAD RH SIDE IAW SRM 51-40-02 AND 53-80-08-2R.
- [SDR FDEA201407111715](https://openairdocs.org/sdr/FDEA201407111715.md): Slide Raft · partial deploy · Jul 11, 2014 · N938FD · Boeing 75723A · Escape Slide
  > AFTER DISARMING CREW ENTRY DOOR 1R SLIDE PARTIALLY DEPLOYED UPON OPENING DOOR. REMOVED AND REPLACED THE R1 DOOR SLIDE/RAFT
- [SDR FDEA201407111714](https://openairdocs.org/sdr/FDEA201407111714.md): Handle · loose · Jul 11, 2014 · N938FD · Boeing 75723A · Passenger/Crew Doors
  > L1 DOOR HANDLE PLASTIC, TOP RT IS LOOSE. SECURED THE L1 DOOR ASSIST HANDLE PER B757 AMM.
- [SDR FDEA201304100763](https://openairdocs.org/sdr/FDEA201304100763.md): Skin · chafed · Apr 10, 2013 · N938FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN BELOW STRINGER 9L AFT OF BULKHEAD BS 1787, EXT SURFACE CHAFED BY STAB FAIRING. COMPLIED WITH EA F-5330-T0300225, CAT "A" MAJOR REPAIR.
- [SDR FDEA201304050732](https://openairdocs.org/sdr/FDEA201304050732.md): Skin · dented · Apr 5, 2013 · N938FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED BS 443 AT S15R. A SKIN REPAIR WAS ACCOMPLISHED IAW EA 757 -5331-16-F4106, REV. MAJOR REPAIR
- [SDR FDEA201304020711](https://openairdocs.org/sdr/FDEA201304020711.md): Skin · misrepaired · Apr 2, 2013 · N938FD · Boeing 75723A · Leading Edge Devices
  > LT WING, NR 2 SLAT COVE PANEL INBD OF OTBD DRIVE TRACK MISREPAIRED. R & R, NR 2 SLAT, INBD OF OTBD DRIVE TRACK, COVE SKIN IAW DWG 114N4026 AND INSTALLED IAW SRM 51-40-02, CAT "A" MAJOR REPAIR.
- [SDR FDEA201303300692](https://openairdocs.org/sdr/FDEA201303300692.md): Structure · damaged · Mar 30, 2013 · N938FD · Boeing 75723A · Trailing Edge Flaps
  > OTBD FLAP LT WING BETWEEN STA 565 -600 HAS ELONGATED HOLE. A REPAIR WAS ACCOMPLISHED IAW EA 757-5753 -16 -F4116, REV-. MAJOR REPAIR.
- [SDR FDEA201303290687](https://openairdocs.org/sdr/FDEA201303290687.md): Skin · failed · Mar 29, 2013 · N938FD · Boeing 75723A · Vertical Stabilizer, Plate/Skin
  > TWO MISDRILLED HOLES AT VERTICAL STAB LT PANEL 322DL ATTACHMENT. COMPLIED WITH EA F-5530-TO300208. MAJOR REPAIR.
- [SDR FDEA201303280684](https://openairdocs.org/sdr/FDEA201303280684.md): Skin · cracked · Mar 28, 2013 · N938FD · Boeing 75723A · Service Doors
  > R2 DOOR FWD FRAME FACE HINGE CUTOUT CRACKED A REPAIR WAS ACCOMPLISHED ON R2 DOOR FWD FRAME UPPER HINGE CUTOUT IAW EA 757-5211-16-F4100 REV, MAJOR REPAIR.
- [SDR FDEA201303200633](https://openairdocs.org/sdr/FDEA201303200633.md): Skin · dented · Mar 20, 2013 · N938FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > INCOMING EXTERNAL FUSELAGE SKIN DENTED BS 1618, BETWEEN S17-18L, REPAIRED IAW EA 757-5361-16-F4111, REV. MAJOR REPAIR.
- [SDR FDEA201303150583](https://openairdocs.org/sdr/FDEA201303150583.md): Intercostal · corroded · Mar 15, 2013 · N938FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FRAME BS 1380-1400 INTERCOSTAL CORRODED. REPAIRED IAW EA 757-5360-16-F4146. MAJOR REPAIR
- [SDR FDEA201303150577](https://openairdocs.org/sdr/FDEA201303150577.md): Stiffener · gouged · Mar 15, 2013 · N938FD · Boeing 75723A · Fuselage Main, Bulkhead
  > BS 1180 BULKHEAD STIFFENER, LBL 45.57 WL 182, GOUGED. BLENDED GOUGE ON STA 1180 BULKHEAD IAW SRM 51-10-02. L= 1.25 W=.75 D=.046 ORIGINAL MATERIAL.107 OUT OF LIMITS IAW SRM 53-40-0 FIG 101, DETAIL III. R & R STIFFENER IAW SRM 51-40-02 AND DWG 144N2509.
- [SDR FDEA201303150582](https://openairdocs.org/sdr/FDEA201303150582.md): Skin · dented · Mar 15, 2013 · N938FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN BS 1701-1720 BETWEEN S28-29R DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REPAIRED IAW SRM 53-00-01 FIG 201.
- [SDR FDEA201303130564](https://openairdocs.org/sdr/FDEA201303130564.md): Skin · corroded · Mar 13, 2013 · N938FD · Boeing 75723A · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON INSIDE AREA, INBD SKIN IS CORRODED TWO PLACES. ACCOMPLISHED EA F- 5450- TO300125.
- [SDR FDEA201303130563](https://openairdocs.org/sdr/FDEA201303130563.md): Skin · dented · Mar 13, 2013 · N938FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED BS 550 BETWEEN S-18R TO S-19R. A SKIN DENT REPAIR BS 540-560, STRINGER S18-20R WAS ACCOMPLISHED IAW EA 757-5331-16-F 4088, REV.
- [SDR FDEA201303080528](https://openairdocs.org/sdr/FDEA201303080528.md): Skin · dented · Mar 8, 2013 · N938FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED BS 395 BETWEEN S-16R TO S-17R FOUND TO BE OUT OF LIMITS IAW SRM 53-00-010, FIG 101, DETAIL III. REPAIRED IAW SRM 53-00-01, REPAIR 16. MAJOR REPAIR,
- [SDR FDEA201303070513](https://openairdocs.org/sdr/FDEA201303070513.md): Skin · corroded · Mar 7, 2013 · N938FD · Boeing 75723A · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON INTERNAL SKIN SURFACES LT SIDE FROM PPS 138 - 174, HAS SIGN OF CORROSION. REPAIRED IAW EA F-5450-T0300141. MAJOR REPAIR
- [SDR FDEA201303060504](https://openairdocs.org/sdr/FDEA201303060504.md): Skin · corroded · Mar 6, 2013 · N938FD · Boeing 75723A · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON LEFT SKIN PANEL 443GL CUTOUT, EDGE CORRODED. REPAIRED IAW EA F-5450-T0300094. MAJOR REPAIR

Next page: https://openairdocs.org/aircraft/N938FD/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 = 'N938FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N938FD/reports

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