# Service difficulty reports: N840FD

A list on [N840FD](https://openairdocs.org/aircraft/N840FD.md).

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

- [SDR FDEA202608281245](https://openairdocs.org/sdr/FDEA202608281245.md): Skin · dented · Aug 28, 2026 · N840FD · Boeing 777F · Trailing Edge Flaps
  > FOUND LT WING, T/E, OTBD FLAP LOWER SURFACE, HAD ONE DENT AT CROSS OTEF, 315 INCHES AND T/E 5 INCHES. REPAIRED LH WING T/E O/B FLAP LOWER SURFACE 01 EA DENT AT CROSS OTEF 315 INCHES AND T/E 5 INCHES AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70
- [SDR FDEA202608261229](https://openairdocs.org/sdr/FDEA202608261229.md): Skin · cracked · Aug 26, 2026 · N840FD · Boeing 777F · Wing, Plate/Skin
  > DURING PERFORM W/O: E G-5710-E0376285 H P14 STEP 5.A.(2) THEN FOUND TWO CRACKS AT NR 5 HOLE OF RT UPPER WING SKIN AT WBL 262. RHW UPPER SKIN OF NO.5 HOLE CRACKS REPAIRED AS PER B777 SRM 51-50-02-0G FIG 1, SRM 51- 40-02-0G FIG 12, SRM 51-10-01-0G FIG 1, SR
- [SDR FDEA202509011585](https://openairdocs.org/sdr/FDEA202509011585.md): Bulb · failed · Sep 1, 2025 · N840FD · Boeing 777F · Emergency Lighting
  > DOOR 1 L/H EXTERIOR EMERGENCY LIGHT INOP. FILAMENT REPLACED AND OPS CHECKED IAW AMM 33-51-04-02-0.
- [SDR FDEA202408301198](https://openairdocs.org/sdr/FDEA202408301198.md): Window · cracked · Aug 30, 2024 · N840FD · Boeing 777F · Escape Slide
  > POST-FLT INSP, L1 DOOR ESCAPE SLIDE BUSTLE PRESSURE GAUGE VIEWPORT WINDOW CRACKED. THE PART FINALLY SHOWED UP. REMOVED AND REPLACED L1 DOOR EMERGENCY ESCAPE SLIDE BUSTLE PRESSURE VIEWPORT LENS ASSY, REF AMM: 25-66-06-4.
- [SDR FDEA202408031080](https://openairdocs.org/sdr/FDEA202408031080.md): Window · overheated · Aug 3, 2024 · N840FD · Boeing 777F · Flight Compartment Windows
  > RIGHT SIDE AFT WINDOW IS VERY HOT TO THE TOUCH AND APPEARS TO HAVE SOME CHARRING AND DELAMINATION IN THE MIDDLE OF THE WINDOW ALONG THE BOTTOM EDGE. COMPLIED WITH PART 3 OF E.A. #: G-5610-T0380167 REMOVED AND REPLACED R3 WINDOW, OPS CHECKS GOOD.
- [SDR FDEA202403270381](https://openairdocs.org/sdr/FDEA202403270381.md): Module · inoperative · Mar 27, 2024 · N840FD · Boeing 777F · Air Data Computer
  > RECEIVED MULTIPLE EICAS ALERTS CLIMBING TO FL330. NO AUTOLAND, WNDSHEAR SYS, EEC MODE L, EEC MODE R. RAN ECL CHECKLISTS FOR EEC MODE LT & RT. ACFT CONTINUED TO CLIMB THRU MCP SELECTED ALT ON ATTEMPING LEVEL OFF. ATC SHOWED 200 FT LOW WHEN MCP SELECTED ALTITU
- [SDR FDEA202403260372](https://openairdocs.org/sdr/FDEA202403260372.md): Pitot Head · failed · Mar 26, 2024 · N840FD · Boeing 777F · Pitot/Static System
  > AUTO PILOT DISCONNECTED AFTER LEVELING FL340. ALTIMETERS LEFT AND RIGHT INDICATED 400' HIGH. MULTIPLE EICAS: "AIRSPEED UNRELIABLE" " ENG EEC MODE R" "ENG EEC MODE L" " GND PROX WARN". ATC READOUT SHOWED 300' LOW WHEN WE RETURNED TO FL 340'. EICAS BUTTON DE
- [SDR FDEA202402210205](https://openairdocs.org/sdr/FDEA202402210205.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 57, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 57, SHEET 2 OF 5 SECTION CUT B-B ARROW ORIENTATION IS CLARI
- [SDR FDEA202402210204](https://openairdocs.org/sdr/FDEA202402210204.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 53, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE GAP 0.60 MIN IS TOO WIDE TO LOCATE THE REPAIR ANGLE. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE
- [SDR FDEA202402210203](https://openairdocs.org/sdr/FDEA202402210203.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 51, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 - 0.30 TYPICAL GAP" SHOWN SEEMS TOO BIG. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 51, S
- [SDR FDEA202402210202](https://openairdocs.org/sdr/FDEA202402210202.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 49, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 49, SHEET 2 OF 3 SECTION CUT B-B ARROW ORIENTATION IS CLARI
- [SDR FDEA202402210201](https://openairdocs.org/sdr/FDEA202402210201.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 47, SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 47, SHEET 2 OF 4 SECTION CUT D-D ARROW ORIENTATION IS CLARI
- [SDR FDEA202402210200](https://openairdocs.org/sdr/FDEA202402210200.md): Longeron · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing, Longeron/Stringer
  > WHILE ACCOMPLISHING EO E G-5710-E0366409 D PART7,(LEFT HAND LONGERON MODIFICATION) FOUND FIGURE 44, SHEET 2 OF 2, VIEW A, CIRCLE STEP 2, THE PRINTED QUANTITY 48 LOCATIONS IS NOT IN ACCORDANCE WITH THE FIGURE AND AIRCRAFT QUANTITY. DISCREPANCY IN EO E G-5
- [SDR FDEA202402210199](https://openairdocs.org/sdr/FDEA202402210199.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 120, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 120, SHEET 2 OF 5, SECTION CUT B-B ARROW ORIENTATION IS CL
- [SDR FDEA202402210198](https://openairdocs.org/sdr/FDEA202402210198.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 116, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE 0.60 MIN GAP TOO WIDE TO LOCATE THE REPAIR ANGLE. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 1
- [SDR FDEA202402210197](https://openairdocs.org/sdr/FDEA202402210197.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 114, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 - 0.30 TYPICAL GAP" SEEMS TOO BIG. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 114, SHEET
- [SDR FDEA202402210196](https://openairdocs.org/sdr/FDEA202402210196.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 112, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 112, SHEET 2 OF 3, SECTION CUT B-B ARROW ORIENTATION IS CL
- [SDR FDEA202402210195](https://openairdocs.org/sdr/FDEA202402210195.md): Unknown · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 110 SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 110 SHEET 2 OF 4, SECTION CUT D-D ARROW ORIENTATION IS CLA
- [SDR FDEA202402210194](https://openairdocs.org/sdr/FDEA202402210194.md): Longeron · misoverhauled · Feb 21, 2024 · N840FD · Boeing 777F · Fuselage Main, Longeron/Stringer
  > WHILE ACCOMPLISHING EO E G-5710-E0366409D PART8 (RIGHT LONGERON MODIFICATION), FOUND FIGURE 107, SHEET 2 OF 2, VIEW A, CIRCLE STEP 2, THE PRINTED QTY 48 LOCATIONS IS NOT IAW FIGURE AND AIRCRAFTQUANTITY. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 107
- [SDR FDEA202402180184](https://openairdocs.org/sdr/FDEA202402180184.md): Structure · unknown · Feb 18, 2024 · N840FD · Boeing 777F · Wing Main, Frame Structure
  > WHILE ACCOMPLISHING EO # EG-5710-E0366409D-PART8, FOUND RIGHT HAND RING CHORD MODIFICATION KIT PART NUMBER 005W0129-4 SHORTAGE REPAIR ANGLE PART NUMBER 691W0017-2. EO # EG-5710-E0366409D PART8 WORK ACCOMPLISHED WITH THE RIGHT HAND RING CHORD REPAIR ANGLE
- [SDR FDEA202307261305](https://openairdocs.org/sdr/FDEA202307261305.md): Light · inoperative · Jul 26, 2023 · N840FD · Boeing 777F · Emergency Lighting
  > POST-FLT INSP, SUPRNMRY DIRECT CTR OVRHD EMERGENCY LT INOP. REPLACED LIGHT ASSEMBLY PER AMM 33-51-03-2 OPS CHECKES OK FOR SVC
- [SDR FDEA202212303044](https://openairdocs.org/sdr/FDEA202212303044.md): Cooling Fan · failed · Dec 30, 2022 · N840FD · Boeing 777F · Air Distribution Fan
  > AIRCRAFT SMELLS OF ELECTRICAL SMOKE. DURING TROUBLESHOOTING IT WAS NOTICED THAT WHEN THE L EQUIPMENT COOLING FAN WAS ISOLATED THERE WAS AN IMPROVEMENT OF THE ODOR. FOR PRECAUTION THE L EQUIPMENT COOLING FAN IS RELEASED MEL AND DEACTIVATED. REMOVED A
- [SDR FDEA202203290751](https://openairdocs.org/sdr/FDEA202203290751.md): None · none · Mar 29, 2022 · N840FD · Boeing 777 · Emergency Lighting
  > PDIS 840 33-50 1107 03FEB22 CDG EMER LIGHT ARM SWITCH WIRE GUARD DOES NOT PROTECT THE SWITCH R/R THE EMERGENCY LIGHT SWITCH GUARD PER SMP.
- [SDR FDEA202202060236](https://openairdocs.org/sdr/FDEA202202060236.md): None · leaking · Feb 6, 2022 · N840FD · Boeing 737 · Hydraulic Power Accumulator, Main
  > PDIS 840 29-11 1118 06FEB22 MEM FACT U GOT THE HYD PRESS PRI L CHECKLIST AND THE HYD QTY LOW L EICAS APPROXIMATELY 3 HOURS INTO FLIGHT FROM EGSS TO KMEM. FL340/ M84/ 480 KTS TAS. COMPLIED WITH ECL. NO FURTHER PROBLEMS. FACT 06FEB22 18:57 M
- [SDR FDEA202111082794](https://openairdocs.org/sdr/FDEA202111082794.md): None · none · Nov 8, 2021 · N840FD · Boeing 777 · Service Doors
  > REPEAT WRITE UP HIGH PITCH CONTINUOUS TONE, FROM CAPTAIN SIDE BELOW LEFT FOOT. CAB ALT 5800 FT DP 8.5. WENT TO MANUAL ON OUTFLOW VALVES, REDUCED CAB ALT TO 5000 FT TONE DP 8.3, THE TONE WAS NOTICEABLY QUIETER. AFTER APPROXIMATELY 10 MINUTES WE RESELECT
- [SDR FDEA202104261044](https://openairdocs.org/sdr/FDEA202104261044.md): Skin · damaged · Apr 26, 2021 · N840FD · Boeing 777F · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING LEFT HAND E.O.#G-5310-E0332629 K P5 FOUND NEW FUSELAGE SKIN DOUBLER (PART NUMBER: 143W2314Y405) EXISTING HOLE AT STATION 998 STRINGER S-35 LEFT NEAR MILLED EDGE. COMPLIED WITH E.A.#:G-5310-T0361452 P1. TITLE:FUSELAGE-MAINFRAME-LH AND
- [SDR FDEA202104261043](https://openairdocs.org/sdr/FDEA202104261043.md): Skin · damaged · Apr 26, 2021 · N840FD · Boeing 777F · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING RIGHT HAND E.O.#G-5310-E0332629 K P6 FOUND NEW FUSELAGE SKIN DOUBLER (PART NUMBER: 143W2314Y406) EXISTING HOLE AT STATION 998 STRINGER S-35 RIGHT NEAR MILLED EDGE. COMPLIED WITH E.A.#:G-5310-T0361452 P2. TITLE:FUSELAGE-MAINFRAME-LH AND
- [SDR FDEA202104230985](https://openairdocs.org/sdr/FDEA202104230985.md): Skin · cracked · Apr 23, 2021 · N840FD · Boeing 777 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1033 STRINGER 37 RIGHT, APPROXIMATELY 1 INCH IN LENGTH. COMPLIED WITH E.O.#:G
- [SDR FDEA202104230984](https://openairdocs.org/sdr/FDEA202104230984.md): Skin · cracked · Apr 23, 2021 · N840FD · Boeing 777 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1028 STRINGER 37 RIGHT, APPROXIMATELY 1 INCH IN LENGTH. COMPLIED WITH E.O.#:G
- [SDR FDEA202104230983](https://openairdocs.org/sdr/FDEA202104230983.md): Skin · cracked · Apr 23, 2021 · N840FD · Boeing 777 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1028 STRINGER 37 LEFT, APPROXIMATELY 1 INCH IN LENGTH. COMPLIED WITH E.O.#:G-531
- [SDR FDEA202104230982](https://openairdocs.org/sdr/FDEA202104230982.md): Skin · cracked · Apr 23, 2021 · N840FD · Boeing 777 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1033 STRINGER 37 LEFT, APPROXIMATELY 1.5 INCHES IN LENGTH. COMPLIED WITH E.O.#:

## 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 = 'N840FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N840FD/reports

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