# Boeing 777-FS2 - Type: Aircraft model (FAA registry) - Registry code: 138527H - Manufacturer (registry): BOEING CO - Model: 777-FS2 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 13 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 24 - Page: https://openairdocs.org/model/boeing-777-fs2 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (24) - [N850FD](https://openairdocs.org/aircraft/N850FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2009, S/N 37721 - [N851FD](https://openairdocs.org/aircraft/N851FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2009, S/N 37722 - [N852FD](https://openairdocs.org/aircraft/N852FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2010, S/N 37723 - [N853FD](https://openairdocs.org/aircraft/N853FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2009, S/N 37724 - [N854FD](https://openairdocs.org/aircraft/N854FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2010, S/N 37725 - [N855FD](https://openairdocs.org/aircraft/N855FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2010, S/N 37726 - [N856FD](https://openairdocs.org/aircraft/N856FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2010, S/N 37727 - [N857FD](https://openairdocs.org/aircraft/N857FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2010, S/N 37728 - [N858FD](https://openairdocs.org/aircraft/N858FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2011, S/N 37729 - [N859FD](https://openairdocs.org/aircraft/N859FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2013, S/N 37730 - [N861FD](https://openairdocs.org/aircraft/N861FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2011, S/N 37732 - [N862FD](https://openairdocs.org/aircraft/N862FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2011, S/N 37733 - [N863FD](https://openairdocs.org/aircraft/N863FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2012, S/N 37734 - [N864FD](https://openairdocs.org/aircraft/N864FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2012, S/N 37735 - [N868FD](https://openairdocs.org/aircraft/N868FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2015, S/N 40674 - [N869FD](https://openairdocs.org/aircraft/N869FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2015, S/N 40675 - [N884FD](https://openairdocs.org/aircraft/N884FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2011, S/N 37137 - [N885FD](https://openairdocs.org/aircraft/N885FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2011, S/N 41064 - [N886FD](https://openairdocs.org/aircraft/N886FD): [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2012, S/N 41065 - [N887FD](https://openairdocs.org/aircraft/N887FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2012, S/N 41066 - [N889FD](https://openairdocs.org/aircraft/N889FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2012, S/N 41067 - [N890FD](https://openairdocs.org/aircraft/N890FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2012, S/N 41439 - [N892FD](https://openairdocs.org/aircraft/N892FD): [Federal Express Cor](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20COR), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2011, S/N 38707 - [N895FD](https://openairdocs.org/aircraft/N895FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2013, S/N 41749 ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB OPS26LA027](https://openairdocs.org/ntsb/OPS26LA027), Mar 18, 2026: Boeing 777-FS2 (N853FD), Newark, NJ, incident, no damage, investigation ongoing ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (690, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FDEA202608221219](https://openairdocs.org/sdr/FDEA202608221219), Aug 22, 2026: TIRE TREAD. SEPARATED. CHECK FOUND NR 11 TIRE TREAD SEPARATION. - [SDR FDEA202608221218](https://openairdocs.org/sdr/FDEA202608221218), Aug 22, 2026: POWER SUPPLY. INOPERATIVE. DURING SERVICE CHECK, FOUND EXTERIOR RT EMERGENCY LIGHT NOT WORKING. RT EMERGENCY LIGHT POWER SUPPLY REPLACED IAW AMM 33-51-06-2. TESTED OK. - [SDR FDEA202607150925](https://openairdocs.org/sdr/FDEA202607150925), Jul 15, 2026: SKIN. BULGED. RIGHT WING NR 9 SLAT UPPER SURFACE 32IN FROM OTBD EDGE FOUND BULGE. NR 9 SLAT UPPER SURFACE 32 INCH FROM OB EDGE BULGE AREA REPAIRED IAW SRM 51-40-02-0G, SRM 57 - [SDR FDEA202607120916](https://openairdocs.org/sdr/FDEA202607120916), Jul 12, 2026: LIGHT SYS. MALFUNCTIONED. CHECK FOUND WHEN THE OVERHEAD PANEL EMER LIGHTS SWITCH IN "ON" POSITION, THE EMERGENCY LIGHTS NOT ILLUMINATED. AMM: 33-51-00-5 RESET THE CB'S AND PERFORMED EMER - [SDR FDEA202606090690](https://openairdocs.org/sdr/FDEA202606090690), Jun 9, 2026: RETAINER. DAMAGED. FOUND RH WING SLAT NR 8 IB EDGE SEAL RETAINER UPPER SURFACE AFT SECOND FASTENER HOLE WORN. RH WING NO.8 SLAT IB EDGE OUTER SKIN FASTENER HOLE WORN AREA REPAIRED - [SDR FDEA202606090689](https://openairdocs.org/sdr/FDEA202606090689), Jun 9, 2026: SKIN. DAMAGED. NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE FOUND WORN. NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE WORN AREA REPAIR - [SDR FDEA202606060678](https://openairdocs.org/sdr/FDEA202606060678), Jun 6, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD: E G-5710-E0376285 G P11 STEP 5.A.(2) THEN FOUND 01 EA CRACKED ON LT UPPER WING SKIN FASTENER NR 5. REPAIRED AS PER B777 SRM 51-40-05- - [SDR FDEA202606060677](https://openairdocs.org/sdr/FDEA202606060677), Jun 6, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:E G-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 01 EA CRACK ON RH UPPER WING SKIN FASTENER #5. REPAIRED AS PER B777 SRM 51-40-05- 0G FI - [SDR FDEA202606050674](https://openairdocs.org/sdr/FDEA202606050674), Jun 5, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 02EA CRACKS ON RH UPPER WING SKIN COMMON TO FASTENER #5 AS MARKED. - [SDR FDEA202606050673](https://openairdocs.org/sdr/FDEA202606050673), Jun 5, 2026: SKIN. DAMAGED. REQUEST A PERMANENT REPAIR ON AFT FUSELAGE SKIN STA 2319 TO STA 2344.5, S-48R TO S-49R. - [SDR FDEA202606040671](https://openairdocs.org/sdr/FDEA202606040671), Jun 4, 2026: LAMP. INOPERATIVE. POST-FLT INSP, L1 OVERHEAD EMERGENCY LT INOP. AMM: 33-51-04-2 RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC. - [SDR FDEA202606010665](https://openairdocs.org/sdr/FDEA202606010665), Jun 1, 2026: FIRE BOTTLE. FAILED. AT 2335Z (APPROX 1:15 INTO THE FLIGHT), FL340, TAT -11, .838MACH, GOT BOTTLE DISCHARGE APU CAUTION WITH LIGHT APU BTL DSCG ON OVERHEAD AND BOTTLE APU ON STATUS - [SDR FDEA202605310656](https://openairdocs.org/sdr/FDEA202605310656), May 31, 2026: SKIN. DAMAGED. REQUEST A PERMANENT REPAIR ON LT AFT FUSELAGE AT APPROXIMATELY STA 1895 TO 1958 AND S-40L TO S-43L. LT AFT FUSELAGE AT APPROXIMATELY BS 1895 TO 1958 AND S-40L T - [SDR FDEA202605300655](https://openairdocs.org/sdr/FDEA202605300655), May 30, 2026: WIRE. DETACHED. ARMING WIRE ON EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL IS STRETCHED OUT AND NOT ARMING EMERGENCY LIGHTS NORMALLY WHEN THE WIRE FALLS OFF SWITCH. AMM: 33-51-00 - [SDR FDEA202605140595](https://openairdocs.org/sdr/FDEA202605140595), May 14, 2026: SKIN. DEBONDED. LEFT OTBD FLAP LWR SURFACE FROM OTBD TO INBD 268 INCHES CROSS TE TO LE 10 INCHES FOUND DEBONDED. REPAIRED LH OB FLAP LWR SURFACE DISBOND AT OTEF STA 260 AS PER - [SDR FDEA202605110586](https://openairdocs.org/sdr/FDEA202605110586), May 11, 2026: SWITCH. OUT OF ADJUST. EMERGENCY LIGHTS ADVISORY MESSAGE STILL APPEARS. AMM: 33-51-00-5 ADJUSTED SWITCH GAURD, OPS CHECK GOOD. - [SDR FDEA202605110585](https://openairdocs.org/sdr/FDEA202605110585), May 11, 2026: WARNING MESSAGE. FALSE ACTIVATION. EMERGENCY LIGHTS ADVISORY APPEARED ON PREFLIGHT. AMM: 33-51-00-5 EMERGENCY LIGHTS OPS CHECKS OK PER ABOVE REF, OK FOR SERVICE - [SDR FDEA202605110581](https://openairdocs.org/sdr/FDEA202605110581), May 11, 2026: SKIN. BULGED. FOUND RT WING LE NR 11 SLAT EXTERNAL SURFACE A BULGE AT STA 873. BULGE REPAIRED AS PER B777 SRM57- 43-01-2R REPAIR 9 FIGURE 202 REV:51.0 AND EA G-5750-T0387321 - [SDR FDEA202605110580](https://openairdocs.org/sdr/FDEA202605110580), May 11, 2026: SKIN. BULGED. FOUND RT WING LE NR 9 SLAT EXTERNAL SURFACE A BULGE AT STA 564. BULGE REPAIRED AS PER B777 SRM57-43- 01-2R REPAIR 16 FIGURE 202 REV:53.0. AND EA G-5750-T0387322 - [SDR FDEA202605100579](https://openairdocs.org/sdr/FDEA202605100579), May 10, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP3.B & STEP5.A.(2) THEN FOUND 01EA CRACK ON THE RH UPPER WING SKIN FASTENER #5. RH UPPER WING SKIN RIB BAY 10 - [SDR FDEA202605100578](https://openairdocs.org/sdr/FDEA202605100578), May 10, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP3.B & STEP5.A.(2) FOUND TWO CRACKS ON THE LT UPPER WING SKIN FASTENER #5. H WING UPPER SKIN IN RIB BAY 10 TR - [SDR FDEA202605030534](https://openairdocs.org/sdr/FDEA202605030534), May 3, 2026: SKIN. DENTED. FOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 127 INCHES AND T/E 10 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT - [SDR FDEA202605030533](https://openairdocs.org/sdr/FDEA202605030533), May 3, 2026: SKIN. DENTED. FOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 231 INCHES AND T/E 8 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT - [SDR FDEA202604300524](https://openairdocs.org/sdr/FDEA202604300524), Apr 30, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT RH WING UPPER WING SKIN COMMON TO FASTENER 5. RT WING UPPER - [SDR FDEA202604300523](https://openairdocs.org/sdr/FDEA202604300523), Apr 30, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT LT WING UPPER WING SKIN COMMON TO FASTENER 5. LT WING UPPER - [SDR FDEA202604240496](https://openairdocs.org/sdr/FDEA202604240496), Apr 24, 2026: BULB. INOPERATIVE. R1 DOOR AFT EMERGENCY EXIT SIGN LIGHT INOP (1EA BULB). REPLACED THE BULB EMERGENCY EXIT LIGHT AT R1 DOOR IAW AMM 33-51-01-2. - [SDR FDEA202603200359](https://openairdocs.org/sdr/FDEA202603200359), Mar 20, 2026: SKIN. DENTED. RIGHT WING OTBD FLAP LOWER SURFACE FROM OB TO IB 272 INCHES CROSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED RH WING OB FLAP LOWER SURFACE DENT AT OTEF STA 250 - [SDR FDEA202603170356](https://openairdocs.org/sdr/FDEA202603170356), Mar 17, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK ON UPPER WING SKIN FASTENER NR 5. RH WING UPPER SKIN #5 HOLE CR - [SDR FDEA202603160354](https://openairdocs.org/sdr/FDEA202603160354), Mar 16, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285G P11 STEP 3.B.(1)& STEP 5.A.(2) THEN FOUND 01EA CRACK ON UPPER WING SKIN FASTENER #5. LT WING UPPER SKIN #5 HOLE CRACK - [SDR FDEA202603050315](https://openairdocs.org/sdr/FDEA202603050315), Mar 5, 2026: LAMP. INOPERATIVE. DURING POSTFLIGHT, FOUND R1 DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED THE LAMPS, R1 DOOR SLIDE EMERGENCY EXTERIOR LIGHT 777 AMM. OPS CHECKED GOOD. ACFT OK FOR S - [SDR FDEA202603020314](https://openairdocs.org/sdr/FDEA202603020314), Mar 2, 2026: SLIDE. FAULTED. UPON CLOSING THE AIRCRAFT ENTRY DOOR AND ARMING THE EVACUATION SLIDES, F/O NOTICED AN FSS FAULT ON POSITIONS 13L AND 13R. F/O OPENED THE DOOR TO SEE IF THE FAUL - [SDR FDEA202603020304](https://openairdocs.org/sdr/FDEA202603020304), Mar 2, 2026: SLIDE. UNWANTED DEPLOY. UPON CLOSING THE ACFT ENTRY DOOR AND ARMING THE EVACUATION SLIDES, F/O NOTICED AN FSS FAULT ON POSITIONS 13L & 13R. F/O OPENED THE DOOR TO SEE IF THE FAULTS WOU - [SDR FDEA202602280291](https://openairdocs.org/sdr/FDEA202602280291), Feb 28, 2026: SAFETY WIRE. WRONG PART. LEFT SLIDE PACKBOARD RELEASE CABLE MECHANISM REQUIRES CAD COPPER SAFETY WIRE. REF FEA G-2560-F0386282 C P1. SAFETIED LT SLIDE PACKBOARD RELEASE CABLE MECHANISH - [SDR FDEA202602230259](https://openairdocs.org/sdr/FDEA202602230259), Feb 23, 2026: SAFETY WIRE. WRONG PART. FOUND INCORRECT SAFETY WIRE ON L1 DOOR SLIDE. AMM: 25-66-01-4 REPLACED SAFETY WIRE WITH CAD COPPER. - [SDR FDEA202602200247](https://openairdocs.org/sdr/FDEA202602200247), Feb 20, 2026: SKIN. DENTED. LH WING OB FLAP LOWER SURFACE FROM OB TO IB 97 INCHES CROSS TE TO LE 8 INCHES FOUND ONE DENT. REPAIRED LT WING OB FLAP LOWER SURFACE DENT AT OTEF STA 431 AS PER - [SDR FDEA202602180233](https://openairdocs.org/sdr/FDEA202602180233), Feb 18, 2026: SLIDE. DAMAGED. R1 DOOR SLIDE REQUIRES CORRECT BREAKAWAY WIRE TO BE INSTALLED ON PACKBOARD RELEASE CABLE. REF F.E.A. G2560-F0386294 C P1. INSTALLED CAD-PLATED COPPER BREAKAWAY - [SDR FDEA202602160217](https://openairdocs.org/sdr/FDEA202602160217), Feb 16, 2026: SAFETY WIRE. WRONG PART. LEFT SLIDE ASSY. SN 3359, FOUND BREAK AWAY WIRE SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. RELEASED FOR SERVICE PER MEL : 52-11-01-02 CATE - [SDR FDEA202602160216](https://openairdocs.org/sdr/FDEA202602160216), Feb 16, 2026: SAFETY WIRE. WRONG PART. FOUND L1 DOOR SLIDE SAFETY WIRE NON-COMPATIBLE, NEEDS REPLACING. REPLACED SAFETY WIRE WITH PART NO. MS20995CY16 CAD PLATED COPPER. REF. AMM 25-66-01-4. AC OK FO - [SDR FDEA202602160215](https://openairdocs.org/sdr/FDEA202602160215), Feb 16, 2026: SAFETY WIRE. WRONG PART. RH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER - [SDR FDEA202602160214](https://openairdocs.org/sdr/FDEA202602160214), Feb 16, 2026: SAFETY WIRE. WRONG PART. LH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOAR RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER - [SDR FDEA202602150211](https://openairdocs.org/sdr/FDEA202602150211), Feb 15, 2026: SAFETY WIRE. WRONG PART. WRI TO REPLACE THE R1 DOOR SLIDE WIRE WITH MS20995CY16 WIRE. AMM: 25-66-01-4 REPLACED R1 DOOR SLIDE SHEAR WIRE WITH MS20995CY16 WIRE PER REF ABOVE - [SDR FDEA202602150204](https://openairdocs.org/sdr/FDEA202602150204), Feb 15, 2026: RELEASE CABLE. WRONG PART. RIGHT SLIDE PACKBOARD RELAEASE CABLE MECHANISM REQUIRES CAD PLATED COPPER BREAKAWAY WIRE. REF WRI 25-60/4116 FEA 2560-F0386282 C P1. SAFETIED RT SLIDE PACKBOARD - [SDR FDEA202602150203](https://openairdocs.org/sdr/FDEA202602150203), Feb 15, 2026: SLIDE. FOM. L1 DOOR SLIDE REMOVED FOR F.O.M. OF F.E.A. MOD TYPE F MOD NR G-2560-F0386282 REV NR C PS P1. INSTALLED L1 DOOR SLIDE OPS CHECKS GOOD IAW AMM 25-66-01-4, & AMM 2 - [SDR FDEA202602140194](https://openairdocs.org/sdr/FDEA202602140194), Feb 14, 2026: SAFETY WIRE. WRONG PART. SAFETY WIRE FOUND ON SLIDE WAS NOT THE CORRECT TYPE ACCORDING TO F.E.A.#:G-2560-F0386282 C PART: 1 (P1) REPLACED BREAKAWAY WIRE WITH CORRECT WIRE SPEC (MS20995C - [SDR FDEA202602140193](https://openairdocs.org/sdr/FDEA202602140193), Feb 14, 2026: SAFETY WIRE. WRONG PART. RIGHT SLIDE, REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE P - [SDR FDEA202602130192](https://openairdocs.org/sdr/FDEA202602130192), Feb 13, 2026: SLIDE. MISWIRED. R1 DOOR SLIDE HAS INCORRECT SAFETY WIRE ON PACKBOARD RELEASE CABLE. INSTALLED PROPER SAFETY WIRE ON R1 SLIDE PACKBOARD RELEASE CABLE IAW B777MM 25-66-01-4. A/C - [SDR FDEA202602120183](https://openairdocs.org/sdr/FDEA202602120183), Feb 12, 2026: WIRE. WRONG PART. FOUND BREAKAWAY WIRE THAT SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. REMOVED LT DOOR SLIDE IAW MM 25-66-01-4. REMOVED STAINLESS SAFETY WIR - [SDR FDEA202602090152](https://openairdocs.org/sdr/FDEA202602090152), Feb 9, 2026: SKIN. CRACKED. DURING WORK CARD: EG-5710-E0376285F P12 STEP3.B(1) & 5.A.(2), FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RIGHT WING UPPER SKIN NR 5 FASTENER HOLE REP - [SDR FDEA202602090151](https://openairdocs.org/sdr/FDEA202602090151), Feb 9, 2026: SKIN. CRACKED. DURING WORK CARD: EG-5710-E0376285F P12 STEP4.B(2).(B), THEN FOUND ONE CRACK ON RT UPPER WING SKIN FASTENER #6 AS MARKED. RIGHT WING UPPER SKIN NR 6 FASTENER HO - [SDR FDEA202602090150](https://openairdocs.org/sdr/FDEA202602090150), Feb 9, 2026: SKIN. CRACKED. DURING WORK CARD: EG-5710-E0376285F P11 STEP4.B(2).(B), THEN FOUND ONE CRACK ON LT UPPER WING SKIN FASTENER NR 6. THE LEFT WING UPPER SKIN #6 FASTENER HOLE CRAC All 690: https://openairdocs.org/model/boeing-777-fs2/reports.md --- 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.