# Service difficulty reports: Boeing 777FHT

A list on [Boeing 777FHT](https://openairdocs.org/model/boeing-777fht.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 119 reports

- [SDR FDEA202610081491](https://openairdocs.org/sdr/FDEA202610081491.md): Lamp · failed · Oct 8, 2026 · N842FD · Boeing 777FHT · Emergency Lighting
  > PRE-FLT MX INSP, (1EA) DIRECT GALLEY OVERHEAD EMERGENCY LIGHT INOP. REPLACED THE LAMPS, IAW AMM 33-51-04-2. LIGHTS TESTED SATIS, ITEM OK FOR SVC.
- [SDR FDEA202609171359](https://openairdocs.org/sdr/FDEA202609171359.md): Hose · loose · Sep 17, 2026 · N843FD · Boeing 777FHT · Hydraulic System, Main
  > HYD QTY LOW C EICAS AT 3:45 AFTER TAKEOFF. EICAS WAS REVIEWED AND EVENT RECORD AT 1246Z. THEN RESERVE BRAKES/STRG EICAS OCCURRED. EICAS WAS REVIEWED AND DECISION TO DIVERT TO LFPG. FOUND A RUNNING LEAK COMING FROM THE NUT CONNECTING THE #12 BRAKE HOSE
- [SDR FDEA202608261230](https://openairdocs.org/sdr/FDEA202608261230.md): Lamp · inoperative · Aug 26, 2026 · N842FD · Boeing 777FHT · Emergency Lighting
  > POST-FLT INSP, (1EA) OVRHD SUPRNMRY AREA EMERGENCY LIGHT INOP. RE-LAMPED, IAW AMM: 33-51-04-2. LIGHT TESTS SATIS, OK FOR SVC.
- [SDR FDEA202607140922](https://openairdocs.org/sdr/FDEA202607140922.md): Skin · damaged · Jul 14, 2026 · N883FD · Boeing 777FHT · Nacelle/Pylon, Main Frame
  > WHEN PERFORM EA G-5730-T0384072 P2 STEP 2, REPORT THE CURRENT AIRCRAFT CONFIGURATION TO FEDEX SERVICE ENGINEERING TO REQUEST AIRPLANE JACKING REQUIREMENTS FROM BOEING TO PERFORM THE PERMANENT DOUBLER/TRIPLER REPAIR AS SHOWN IN FIGURE 1. NOTED: NO.1 E
- [SDR FDEA202606040672](https://openairdocs.org/sdr/FDEA202606040672.md): Lamp · no test · Jun 4, 2026 · N842FD · Boeing 777FHT · Emergency Lighting
  > EMERGENCY LIGHT OVER THE GALLEY TESTS BAD. AMM 33-50-00-2 RELAMPED EMER LIGHT OVER THE GALLEY. OPS TEST OK. AIRCRAFT GOOD TO GO.
- [SDR FDEA202605280682](https://openairdocs.org/sdr/FDEA202605280682.md): Fan · failed · May 28, 2026 · N844FD · Boeing 777FHT · Air Distribution Fan
  > PRIOR TO PUSH, HEARD A LOUD POP ON THE FLIGHT DECK. STATUS MESSAGE: EQUIP VENT FAN. REPLACED EQUIPMENT COOLING VENT FAN PER MM 21-27-20-4, FOUND REMOVED FAN WITH ALL BLADES DESTROYED. PERFORMED OPS TEST PER SAME MM. TEST FAILED WITH MAINTENANCE MESSAGE 2
- [SDR FDEA202602260284](https://openairdocs.org/sdr/FDEA202602260284.md): Safety Wire · wrong part · Feb 26, 2026 · N883FD · Boeing 777FHT · Emergency Equipment
  > REMOVED RH DOOR SLIDE MPN 62771-128 MSN M10748 REF FEA G-2560-F0386294 REV NO. A PS P1 AND AMM 25-66-01-4 AND WRI 25-60/513. INSTALLED COPPER SAFETY WIRE (MS20995CY16). REPACKED/ LACED RH SLIDE AND INSTALLED ON AIRCRAFT PER CMM 25-61-31, FEA G-2560-
- [SDR FDEA202602260283](https://openairdocs.org/sdr/FDEA202602260283.md): Safety Wire · wrong part · Feb 26, 2026 · N883FD · Boeing 777FHT · Emergency Equipment
  > REMOVED LH SLIDE MPN 62771-127 MSN M10268 REF FEA G-2560-F0386282 REV NO. A PS P1 AND AMM 25-66-01-4 AND WRI 25-60/5712 PLACED SLIDE IN LINESHACK 380 INSTALLED COPPER SAFETY WIRE (MS20995CY16). REPACKED/ LACED LH SLIDE AND INSTALLED ON AIRCRAFT PER
- [SDR FDEA202602110221](https://openairdocs.org/sdr/FDEA202602110221.md): Safety Wire · incorrect · Feb 11, 2026 · N843FD · Boeing 777FHT · Escape Slide
  > REF FEA G2560-F0386294 REV C P1 FOUND INCORRECT SAFETY WIRE ON RIGHT DOOR SLIDE. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-66-01-4-0.
- [SDR FDEA202512250013](https://openairdocs.org/sdr/FDEA202512250013.md): Modulating Valve · inoperative · Dec 25, 2025 · N883FD · Boeing 777FHT · Cabin Cooling System
  > AT FL390 WITH OAT -58C, BEGAN TO RECEIVE INTERMITTENT PACK L EICAS MESSAGE WITH CORRESPONDING CABIN TEMPERATURE DROP. COCKPIT TEMPERATURE WAS SET TO 26C AS COCKPIT TEMPERATURE DROPPED TO 10C. DECENDED TO FL350 AND RAN CABIN TEMP COLD QRH CHECKLIST THAT
- [SDR FDEA202511172187](https://openairdocs.org/sdr/FDEA202511172187.md): Lamp · failed · Nov 17, 2025 · N842FD · Boeing 777FHT · Emergency Lighting
  > FOUND RT DOOR FWD EXIT SIGN - LAMP INOPERATIVE. AMM: 33-51-01-2 IAW AMM 33-51-01-2, REPLACED EXIT SIGN LAMPS, OPS TEST GOOD. OK TO CONTINUE. IAW AMM 33-51-01-2, REPLACED EXIT SIGN LAMPS, OPS TEST GOOD. OK TO CONTINUE.
- [SDR FDEA202510202055](https://openairdocs.org/sdr/FDEA202510202055.md): Switch · out of position · Oct 20, 2025 · N844FD · Boeing 777FHT · Central Warning
  > AT FL350 AFTER APPROXIMATELY 2 HOUR STARRED RECEIVING INTERMITTENT OVERSPEED WARNING AND THE UPPER ZIPPER KEPT MOVING UP AND DOWN. THEN AFTER 10 MIN OVERSPEED WARNING STAYED ON AND ZIPPER WENT TO 240 IT S AND STAYED ON. THEN THE OVERSPEED GEAR VMO/MMO ADVISOR
- [SDR FDEA202507171232](https://openairdocs.org/sdr/FDEA202507171232.md): Oil System · leaking · Jul 17, 2025 · N842FD · Boeing 777FHT · Turbine Engine Oil System
  > OIL QTY ON RIGHT ENGINE WENT TO 4 QTS ABOUT 3.5 HOURS INTO FLIGHT. EVENTUALLY DECREASED TO ZERO OIL QTY ABOUT 1.5 HOURS LATER. OIL PRESSURE DECREASED TO 35 IN DESCENT, NEVER ANY LOWER. NEVER GOT ANY EICAS MESSAGES OR SECONDARY INDICATIONS. REMOVED AND RE
- [SDR FDEA202507111178](https://openairdocs.org/sdr/FDEA202507111178.md): Skin · cracked · Jul 11, 2025 · N883FD · Boeing 777FHT · Wing, Plate/Skin
  > UT AND HFEC OPEN HOLE INSPECTION FOUND TWO CRACKS IN LH WING #5 HOLE. THE LH WING UPPER SKIN #5 HOLE TWO CRACKS REPAIRED AS PER B777 SRM51-20-07-0G REV:47.6 AND EA G-5730-T0384072 P1, TITLE:WING-PLATES AND SKINS-LH WING UPPER SKIN CRACK REPAIR IN RIB BAY
- [SDR FDEA202411011627](https://openairdocs.org/sdr/FDEA202411011627.md): Lamp · failed · Nov 1, 2024 · N843FD · Boeing 777FHT · Emergency Lighting
  > POST-FLT INSP, R1 DOOR EXTERIOR EMERGENGY LT INOP. AMM: 33-51-04-2 RE-LAMPED, REF AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202409281383](https://openairdocs.org/sdr/FDEA202409281383.md): Pan · eroded · Sep 28, 2024 · N844FD · Boeing 777FHT · Trailing Edge Flaps
  > LH I/B MAIN FLAP OB SIDE SEAL PAN FOUND EROSION. REPAIRED LH I/B MAIN FLAP OB SIDE SEAL PAN EROSION AS PER B777 SRM 57-53-01-2R-1 AND SRM 51-70-04-2R-10 REV 47.0 AND EA G-5750-T0380710 P1, TITLE: WING-FLIGHT SURFACES-LH INBD MAIN FLAP OUTBOARD CLOSURE SEAL
- [SDR FDEA202408091095](https://openairdocs.org/sdr/FDEA202408091095.md): Skin · delaminated · Aug 9, 2024 · N842FD · Boeing 777FHT · Trailing Edge Flaps
  > RH WING OB FLAP LWR SURFACE FOUND DENT WITH DISBOND AT 275 IN AWAY FROM OB, 10 IN AWAY TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 251 AS PER B777 SRM 57-53-01-2R REPAIR 2, SRM 51-70-04-2R REPAIR 1 REV 46.3 AND EA: G-5750-T0380234 P1,
- [SDR FDEA202408081093](https://openairdocs.org/sdr/FDEA202408081093.md): Skin · dented · Aug 8, 2024 · N842FD · Boeing 777FHT · Fuselage Main, Plate/Skin
  > DURING PERFORM E.A:G-5330-T0368078 - FUSELAGE - PLATES&SKINS - AFT FUSELAGE SKIN PANEL STA 1902.5 - 1907.5, STR 46R - 47R, THE DENT DAMAGE FOR CAT C INTERIM REPAIR WILL BE REPLACED BY CAT A OR B PERMANENT REPAIR. AFT FUSELAGE SKIN AT STA 1902.5-1907.5, ST
- [SDR FDEA202408021078](https://openairdocs.org/sdr/FDEA202408021078.md): Bulb · failed · Aug 2, 2024 · N842FD · Boeing 777FHT · Emergency Lighting
  > SVC CK, (1EA) SUPRNMRY AREA OVERHEAD EMERGENCY LIGHT INOP. RE-LAMPED, REF B777 AMM: 33-50-00-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202407231045](https://openairdocs.org/sdr/FDEA202407231045.md): Skin · delaminated · Jul 23, 2024 · N843FD · Boeing 777FHT · Trailing Edge Flaps
  > LH WING OB FLAP LWR SURFACE FROM IB TO OB 163 INCH CROSS TE TO LE 11 INCH FOUND DELAMINATION. REPAIRED LH WING OB FLAP LWR SURFACE AT OTEF STA188 DELAMINATION AS PER B777 SRM 57-53-01-2R REPAIR 2, SRM 51-70-04-2R REPAIR 1 REV.46.3 AND EA:G-5750-T0380006 P1
- [SDR FDEA202403110276](https://openairdocs.org/sdr/FDEA202403110276.md): Wire Harness · damaged · Mar 11, 2024 · N842FD · Boeing 777FHT · Landing Gear Steering System
  > DURING TAXI OUT MAIN GEAR STEERING ALERT ON EICAS - FLASHED UP & DISAPPEARED DURING ONE OF FOUR TURNS TO RUNWAY. AFTER LINE UP & TOGA PRESSED - MAIN GEAR STEERING WARNING ANNUNCIATED. REJECTED TAKEOFF & RTB AT 40KTS. EICAS MAIN GEAR STEERING ANNUNCIATED A
- [SDR FDEA202311081841](https://openairdocs.org/sdr/FDEA202311081841.md): Light · inoperative · Nov 8, 2023 · N842FD · Boeing 777FHT · Emergency Lighting
  > POST-FLT INSP, R-1 DOOR OVRHD EMERGENCY LT INOP. RE-LAMPED, REF B777 AMM: 33-51-04-2. LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202310041697](https://openairdocs.org/sdr/FDEA202310041697.md): Slat · dented · Oct 4, 2023 · N883FD · Boeing 777FHT · Leading Edge Devices
  > NO.7 SLAT EXTERNAL UPR SURFACE FROM IB TO OB 74 INCH CROSS TE TO LE 2 INCH FOUND ONE DENT. EVALUATED NO.7 SLAT EXTERNAL UPR SURFACE FROM IB TO OB 74INCH CROSS TE TO LE 2INCH ONE DENT DAMAGE SIZE LXWXY=8.2"X7.0"X0.098"OUT OF ALLOWABLE LIMIT AS PER B777 SRM
- [SDR FDEA202310021685](https://openairdocs.org/sdr/FDEA202310021685.md): Flap · dented · Oct 2, 2023 · N883FD · Boeing 777FHT · Trailing Edge Flaps
  > LH WING OB FLAP LOWER SURFACE FROM OB TO IB 210 INCH CROSS TE TO LE 13 INCH FOUND ONE DENT. EVALUATED LH WING OB FLAP LOWER SURFACE FROM OB TO IB 210 INCH CROSS TE TO LE 13 INCH ONE DENT DAMAGE SIZE LXW=1.5"X1.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57-5
- [SDR FDEA202310021684](https://openairdocs.org/sdr/FDEA202310021684.md): Floor Panel · cracked · Oct 2, 2023 · N883FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED,AT STA1710 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 CRACKED AT STA1710 RBL1, DAMAGE SIZE L=2.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 REV 45.0. RE
- [SDR FDEA202310021683](https://openairdocs.org/sdr/FDEA202310021683.md): Floor Panel · cracked · Oct 2, 2023 · N883FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 FOUND CRACKED,AT STA1660 RBL1. EVALUATED AND MEASURE MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 CRACKED AT STA1660 RBL1, DAMAGE SIZE L=2.3" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00- 50-1A ALLOWABLE DA
- [SDR FDEA202203250683](https://openairdocs.org/sdr/FDEA202203250683.md): Floor Panel · delaminated · Mar 25, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND DELEMINATION AT BL0 STA 1600,1640,1660. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 AT BL0 STA 1600,1640,1660 REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1 REV40.0 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202203180568](https://openairdocs.org/sdr/FDEA202203180568.md): None · none · Mar 18, 2022 · N842FD · Boeing 777FHT · Emergency Lighting
  > POST-FLT INSP, R-1 EXTERIOR EMERGENCY LT INOP. RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202203040411](https://openairdocs.org/sdr/FDEA202203040411.md): Doubler · misaligned · Mar 4, 2022 · N844FD · Boeing 777FHT · Fuselage Structure (General)
  > DURING PERFORMING EA T G-5710-T0366182 A P2 STEP 11.C.(5), FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT ED
- [SDR FDEA202203040410](https://openairdocs.org/sdr/FDEA202203040410.md): Doubler · unknown · Mar 4, 2022 · N844FD · Boeing 777FHT · Fuselage Structure (General)
  > DURING PERFORMING EA T G-5710-T0366182 A P1 STEP 11.C.(5), FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT ED
- [SDR FDEA202202250371](https://openairdocs.org/sdr/FDEA202202250371.md): Floor Panel · cracked · Feb 25, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL PN: 152W8151-1 AT STA 403-424 LBL 74 FOUND CRACKED. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230361](https://openairdocs.org/sdr/FDEA202202230361.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8351-29 FOUND CRACKED AT STA 1015 LBL86. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230360](https://openairdocs.org/sdr/FDEA202202230360.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-21 FOUND CRACKED AT STA 1331 LBL43. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230359](https://openairdocs.org/sdr/FDEA202202230359.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8351-30 FOUND CRACKED AT STA 1014 RBL84. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230358](https://openairdocs.org/sdr/FDEA202202230358.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8351-28 FOUND CRACKED AT STA 1014 RBL71. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230357](https://openairdocs.org/sdr/FDEA202202230357.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-17 FOUND CRACKED AT STA 1248 LBL76. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230356](https://openairdocs.org/sdr/FDEA202202230356.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8351-27 FOUND CRACKED AT STA 1013 LBL69. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230355](https://openairdocs.org/sdr/FDEA202202230355.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-19 FOUND CRACKED AT STA 1398 LBL38. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230354](https://openairdocs.org/sdr/FDEA202202230354.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-22 FOUND CRACKED AT STA 1365 RBL46. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230353](https://openairdocs.org/sdr/FDEA202202230353.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8651-4 FOUND CRACKED AT STA 1434 RBL81. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230352](https://openairdocs.org/sdr/FDEA202202230352.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8651-6 FOUND CRACKED AT STA 1435 RBL11. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230351](https://openairdocs.org/sdr/FDEA202202230351.md): Floor Panel · cracked · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-18 FOUND CRACKED AT STA 1287 RBL82. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202202230350](https://openairdocs.org/sdr/FDEA202202230350.md): Frame · dented · Feb 23, 2022 · N844FD · Boeing 777FHT · Fuselage Main, Structure
  > MAIN DECK CARGO MAIN FRAME FOUND DEFORM AT STA 1727 S-19R. DEFORMED FRAME REPAIRED AS PER B777 SRM 53-00-07- 2R REPAIR 1 REV 40.0 AND EA G-5310-T0367399 P1, TITLE: FUSELAGE - MAINFRAME - REPAIR OF DENT ON STA1727 FRAME INNER FLANGE AT S-18R. REFER TO WRI:5
- [SDR FDEA202202140291](https://openairdocs.org/sdr/FDEA202202140291.md): Angle · unknown · Feb 14, 2022 · N842FD · Boeing 777FHT · Wing Main, Frame Structure
  > WHILE ACCOMPLISHING EA G-5710-T0366056A P2 RIGHT HAND LOWER CHORD INSTALLATION ON STEP (10.E), MENTIONED IN EA, FASTENER WET INSTALL WITH BMS 5-95 SEALANT (GENERAL PURPOSE SEALANT) COMPLIED WITH E.A # G-5710-T0366458.P2. TITLE: WING-BASIC WING STRUCTURE -
- [SDR FDEA202202140290](https://openairdocs.org/sdr/FDEA202202140290.md): Angle · unknown · Feb 14, 2022 · N842FD · Boeing 777FHT · Wing Main, Frame Structure
  > WHILE ACOMPLISHING EA G-5710-T0366056A P1 LEFT HAND LOWER CHORD INSTALLATION ON STEP (10.E), MENTIONED IN EA, FASTENER WET INSTALL WITH BMS 5-95 SEALANT (GENERAL PURPOSE SEALANT). COMPLIED WITH E.A.# G-5710-T0366458.P1 TITLE: WING - BASIC WING STRUCTURE
- [SDR FDEA202201200104](https://openairdocs.org/sdr/FDEA202201200104.md): Pan · corroded · Jan 20, 2022 · N843FD · Boeing 777FHT · Fuselage Miscellaneous Structure
  > FOUND WASTE DRAIN VALVE ASSEMBLY INSTALLATION HOLE SURROUND CORROSION. WASTE DRAIN VALVE ASSEMBLY INSTALLATION CORROSION WASTE WATER SERVICE PANEL REMOVED AND REPLACED AS PER B777 SRM 51-40-02 REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202201180077](https://openairdocs.org/sdr/FDEA202201180077.md): Doubler · failed · Jan 18, 2022 · N843FD · Boeing 777FHT · Fuselage Structure (General)
  > DURING PERFORMING EA T G-5710-T0366180 A P2 STEP 11.C.(5), 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS FOUND TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDG
- [SDR FDEA202201180076](https://openairdocs.org/sdr/FDEA202201180076.md): Doubler · failed · Jan 18, 2022 · N843FD · Boeing 777FHT · Fuselage Structure (General)
  > DURING PERFORMING EA T G-5710-T0366180 A P1 STEP 11.C.(5), 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS FOUND TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDG
- [SDR FDEA202201160074](https://openairdocs.org/sdr/FDEA202201160074.md): Doubler · unknown · Jan 16, 2022 · N842FD · Boeing 777FHT · Fuselage Main, Structure
  > WHILE ACCOMPLISHING RIGHT HAND E.A.#G-5710-T0366056A P2 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.#G-5710-T0366458 P2 TITLE: WING - BASIC WING STRUCTURE - CENTER WING RING CHORD, FRONT
- [SDR FDEA202201160073](https://openairdocs.org/sdr/FDEA202201160073.md): Doubler · unknown · Jan 16, 2022 · N842FD · Boeing 777FHT · Fuselage Main, Structure
  > WHILE ACCOMPLISHING LEFT HAND E.A.#G-5710-T0366056A P1 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35L NEAR MILLED EDGE COMPLIED WITH E.A.#G-5710-T0366458 P1 TITLE: WING - BASIC WING STRUCTURE - CENTER WING RING CHORD, FRONT SP

Next page: https://openairdocs.org/model/boeing-777fht/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 aircraft_model_key = '777FHT'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-777fht/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.