# Boeing 777F28

- Type: Aircraft model (FAA registry)
- Registry code: 138527E
- Manufacturer (registry): BOEING
- Model: 777F28
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 2
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 2
- Page: https://openairdocs.org/model/boeing-777f28

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 (2)

- [N880FD](https://openairdocs.org/aircraft/N880FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2009, S/N 32967
- [N882FD](https://openairdocs.org/aircraft/N882FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2009, S/N 32969

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (72, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR FDEA202610051477](https://openairdocs.org/sdr/FDEA202610051477), Oct 5, 2026: HOSE. DISCONNECTED. ON POSTFLIGHT WALKAROUND FOUND NR 10 BRAKE HOSE DISCONNECTED AND HANGING. AMM: 32-45-07-4 RECONNECTED NR 10 BRAKE HOSE. REF AMM 32-45-07-4. OP'S CHECK GOOD, LEA
- [SDR FDEA202602170225](https://openairdocs.org/sdr/FDEA202602170225), Feb 17, 2026: SAFETY WIRE. WRONG PART. RIGHT SIDE DOOR SLIDE INSPECTION REVEALED THAT THE WRONG SAFETY WIRE WAS USED. THE WO REQUIRES REPLACING THE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. RH DO
- [SDR FDEA202602150202](https://openairdocs.org/sdr/FDEA202602150202), Feb 15, 2026: SLIDE. NOT REPORTED. LH SLIDE ELECTRONIC CLOSURE FROM TRANSACTION MCFCTMOD, CLOSED DUE TO REMOVAL OF AFFECTED PART.
- [SDR FDEA202510222070](https://openairdocs.org/sdr/FDEA202510222070), Oct 22, 2025: SKIN. DENTED. REWORK: RH WING IB AFT FLAP LWR SURFACE FOUND DENT AT 58 INCHES TO OB EDGE AND 3 INCHES TO FWD EDGE. REPAIRED RH WING IB AFT FLAP LWR SURFACE DENT AT ITEF BS 27
- [SDR FDEA202510162033](https://openairdocs.org/sdr/FDEA202510162033), Oct 16, 2025: SKIN. DENTED. RH WING OB FLAP LWR SURFACE FOUND DENT AT 99.5 INCHES TO IB EDGE AND 11.5 INCHES TO AFT EDGE. REPAIRED RT WING OTBD FLAP LWR SURFACE DENT AT OTEF STA 99.5 IAW S
- [SDR FDEA202510152010](https://openairdocs.org/sdr/FDEA202510152010), Oct 15, 2025: SKIN. CRACKED. DURING PERFORMANCE OF WORK CARD: E G-5710-E0376285E, P12, STEP 3.B.(1), STEP 5.A.(2), & FOUND TWO CRACKS AT HOLE NR 5 OF RT UPPER WING SKIN COMMON TO FASTENERS 
- [SDR FDEA202510152009](https://openairdocs.org/sdr/FDEA202510152009), Oct 15, 2025: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285E P11 STEP 3.B.(1)&STEP 5.A.(2) AND FOUND TWO CRACKS AT HOLE #5 OF LH UPPER WING SKIN COMMON TO FASTENERS 0-5. LH WING 
- [SDR FDEA202508021365](https://openairdocs.org/sdr/FDEA202508021365), Aug 2, 2025: LIGHT. MALFUNCTIONED. EMERGENCY LIGHTS ILLUMINATED DURING BEFORE START CHECKLIST. AMM 33-51-00-5 FOUND EMERGENCY LIGHT SWITCH AT THE OVERHEAD PANEL IN THE OFF POSITION. SWITCH PUT BA
- [SDR FDEA202503140410](https://openairdocs.org/sdr/FDEA202503140410), Mar 14, 2025: SKIN. CRACKED. RH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 51 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 51 INCH TO I/B EDGE CRACK AREA REPAIRED AS PER B777 SRM51-10-02-
- [SDR FDEA202503050333](https://openairdocs.org/sdr/FDEA202503050333), Mar 5, 2025: SKIN. CRACKED. RH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 39 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 39 IN TO IB EDGE CRACK REPAIRED AS PER B777 SRM51-10- 02-0G,51-2
- [SDR FDEA202503050332](https://openairdocs.org/sdr/FDEA202503050332), Mar 5, 2025: SKIN. CRACKED. OPEN HOLE HFEC INSPECTION ON THE RH WING WBL 262 THEN FOUND HOLE #6 CRACK IN UPPER WING SKIN AS MARKED. RH WING WBL 262 UPPER SKIN #6 HOLE CRACK REPAIRED AS PER
- [SDR FDEA202501150071](https://openairdocs.org/sdr/FDEA202501150071), Jan 15, 2025: CONTROLLER. FAILED. ANTI ICE ENG L EICAS DISPLAYED IN FLIGHT. EMERGENCY DECLARED, T/S ACTIVE MX MSG 30-10291, FOUND SOLENOID ON LH ENG ANTI ICE CONTROLLER BAD, REMOVED AND REPLACED
- [SDR FDEA202410031414](https://openairdocs.org/sdr/FDEA202410031414), Oct 3, 2024: OUTFLOW VALVE. FAULTED. ON DEPARTURE, ACFT WOULD NOT PRESSURIZE. THE FWD OUTFLOW VALVE ON MEL. THE REMAINING AFT OUTFLOW VALVE INDICATED CLOSED ON DEPART BUT WOULD NOT ALLOW ACFT TO PR
- [SDR FDEA202405190689](https://openairdocs.org/sdr/FDEA202405190689), May 19, 2024: TIRE. LEAKING. ON CLIMB OUT GOT TIRE PRESS ALERT. RAN ECL AND TIRE PRESSURE SLOWLY DECREASED TO BELOW 50 PSI AND BEFORE DESCENT TO 7 PSI. LANDED UNEVENTFULLY 36C MEM. AIRPORT 
- [SDR FDEA202312231955](https://openairdocs.org/sdr/FDEA202312231955), Dec 23, 2023: SWITCH. FAILED. DURING POSTFLIGHT FOUND EMERGENCY LIGHT SWITCH IN THE FLIGHT DECK INTERMITTENT. AMM: 30-41-02-4 FIM: 33-51-00-2 PER ABOVE 777 FIM, REMOVED AND REPLACED WINDOW H
- [SDR FDEA202312231954](https://openairdocs.org/sdr/FDEA202312231954), Dec 23, 2023: MODULE. FAILED. DURING POSTFLIGHT FOUND EMERGENCY LIGHT SWITCH IN THE FLIGHT DECK INTERMITTENT. REMOVED AND REPLACED WINDOW HEAT/EMERGENCY LIGHTS MODULE PER ABOVE 777 AMM. OPS 
- [SDR FDEA202304240753](https://openairdocs.org/sdr/FDEA202304240753), Apr 24, 2023: UNKNOWN. UNKNOWN. PDIS 880 31-50 3973 24APR23 MEM VMO GEAR DOWN STATUS MESSAGE. RETURNED TO MEM DUE TO UNABLE HIGHER ALTITUDE/AIRSPEED. AMM: 27-32-01-4 FIM: 31-51-00-810-957 TROU
- [SDR FDEA202304240752](https://openairdocs.org/sdr/FDEA202304240752), Apr 24, 2023: UNKNOWN. UNKNOWN. PDIS 880 31-50 3973 24APR23 MEM FACT U VMO GEAR DOWN STATUS MESSAGE. RETURNED TO MEM DUE TO UNABLE HIGHER ALTITUDE/AIRSPEED. FACT 24APR23 08:02 MEM U AMM: 27-32
- [SDR FDEA202304210731](https://openairdocs.org/sdr/FDEA202304210731), Apr 21, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED AT STA1780 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 CRACK AT STA1780 RBL1. CRACK SI
- [SDR FDEA202304210730](https://openairdocs.org/sdr/FDEA202304210730), Apr 21, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8407-34 FOUND CRACKED AT STA1245 RBL55. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8407-34 CRACKED AT STA1245 RBL55.CRACK
- [SDR FDEA202304210729](https://openairdocs.org/sdr/FDEA202304210729), Apr 21, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-9 FOUND CRACKED AT STA1555 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-9 CRACKED AT STA1555 RBL1.CRACK SIZ
- [SDR FDEA202209222354](https://openairdocs.org/sdr/FDEA202209222354), Sep 22, 2022: LAMP. INOPERATIVE. MDIS 880 33-50 3430 21SEP22 ANC OPEN U DURING PREFLIGHT FOUND CENTER OVERHEAD EMERGENCY LIGHT OUT DURING EMERGENCY LIGHT TEST. ALL OTHER LIGHTS OPERATE NORMALLY
- [SDR FDEA202207291819](https://openairdocs.org/sdr/FDEA202207291819), Jul 29, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8701-11 FOUND CRACKED AT STA1970 LBL40. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8701-11 CRACKED AT STA 1970 LBL40 AS PE
- [SDR FDEA202207291818](https://openairdocs.org/sdr/FDEA202207291818), Jul 29, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED AT STA1748 BL0. MAIN DECK CARGO FLOOR PANEL P/N: 152W8601-31 CRACKED AT STA1748 BL0 AS PER B777 SRM 53
- [SDR FDEA202207291817](https://openairdocs.org/sdr/FDEA202207291817), Jul 29, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-17 FOUND CRACKED AT STA1660 BL0. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 CRACKED AT STA1660 BL0 AS PER B77
- [SDR FDEA202206261566](https://openairdocs.org/sdr/FDEA202206261566), Jun 26, 2022: TIRE. DELAMINATED. PDIS 880 32-41 3226 26JUN22 MEM FACT U SUSPECTED TIRE FAILURE ON TAKEOFF IN OSAKA. LANDED WITHOUT INCIDENT. TIRE DID INCUR FURTHER DAMAGE. NEED CHANGE RH NOSE W
- [SDR FDEA202201270753](https://openairdocs.org/sdr/FDEA202201270753), Jan 27, 2022: LAMP. FAILED. PDIS 882 33-50 2851 27JAN22 DXB STARBOARD CEILING EMERGENCY LIGHT IN SUPERNUMERARY INOP. RELAMPED STARBOARD SIDE AREA LIGHT & OPS CHK SATISFACTORY IAW AMM REF 3
- [SDR FDEA202106021435](https://openairdocs.org/sdr/FDEA202106021435), Jun 2, 2021: BRAKE ASSY. FIRE. AFTER BLOCK IN, #8 BRAKE CAUGHT FIRE. FIRE EXTINGUISHED BY RAMP CREW, THEN BY FIRE DEPARTMENT. REMOVED #8 BRAKE & WHEEL & PERFORMED HIGH ENERGY STOP/ HEAT DAMAG
- [SDR FDEA202009302365](https://openairdocs.org/sdr/FDEA202009302365), Sep 30, 2020: BATTERY. CORRODED. MDIS 880 52-20 1013 30SEP20 MEM. L1 EPAS BATTERY UNIT TERMINALS ARE CORRODED. FACT 30SEP20 21:38 MEM 0000086819 STEVENSON, BRIAN A-30-SEP-2020 14:10. REPLACED L
- [SDR FDEA202008071783](https://openairdocs.org/sdr/FDEA202008071783), Aug 7, 2020: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT BS 1937, RBL 49.8 ON REMOVAL OF FLOOR SUPPORT FOUND EDGE CRACKED. STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM 
- [SDR FDEA2020081821747](https://openairdocs.org/sdr/FDEA2020081821747), Aug 2, 2020: SKIN. CRACKED. 02 EACH CRACK FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACK DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE FUSELAGE SKIN BETWEEN STATION 103
- [SDR FDEA2020081402747](https://openairdocs.org/sdr/FDEA2020081402747), Aug 2, 2020: SKIN. CRACKED. 02 EACH CRACK FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACK DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE FUSELAGE SKIN BETWEEN STATION 103
- [SDR FDEA2020081421746](https://openairdocs.org/sdr/FDEA2020081421746), Aug 2, 2020: SKIN. CRACKED. CRACK FOUND APPROXIMATE 0.7" IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE FUSELAGE SKIN AT APPROXIMATELY STATION 1030, STRINGER STR
- [SDR FDEA2020080321747](https://openairdocs.org/sdr/FDEA2020080321747), Aug 2, 2020: SKIN. CRACKED. TWO CRACKS FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACKS FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION FUSELAGE SKIN BETWEEN BS 1030 AND 1035, STRINGER
- [SDR FDEA2020080321746](https://openairdocs.org/sdr/FDEA2020080321746), Aug 2, 2020: SKIN. CRACKED. CRACK FOUND APPROXIMATE 0.7" IN LENGTH, DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE FUSELAGE SKIN AT BS 1030, STRINGER 37L.
- [SDR FDEA2020080321745](https://openairdocs.org/sdr/FDEA2020080321745), Aug 2, 2020: SKIN. DAMAGED. WHILE ACCOMPLISHING EO G-5310-E0332629 G P6, FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT BS 998, STRINGER 35R NEAR MILLED EDGE.
- [SDR FDEA2020080321744](https://openairdocs.org/sdr/FDEA2020080321744), Aug 2, 2020: SKIN. DAMAGED. WHILE ACCOMPLISHING EO G-5310-E0332629 G P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT BS 998, STRINGER 35L NEAR MILLED EDGE.
- [SDR FDEA202007301725](https://openairdocs.org/sdr/FDEA202007301725), Jul 30, 2020: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT BS 1916, RBL 49.8 FLOOR SUPPORT FOUND CRACKED. REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM EXISTING SPLICE STATIO
- [SDR FDEA2020081421648](https://openairdocs.org/sdr/FDEA2020081421648), Jul 25, 2020: LONGERON. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 02 EA FASTENER HOLES WITH CRACK INDICAT
- [SDR FDEA2020081451647](https://openairdocs.org/sdr/FDEA2020081451647), Jul 25, 2020: LONGERON. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 01EA FASTENER HOLES WITH CRACK INDICAT
- [SDR FDEA2020072751648](https://openairdocs.org/sdr/FDEA2020072751648), Jul 25, 2020: STRINGER. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 04EA FASTENER HOLES WITH CRACK INDICATI
- [SDR FDEA2020072751647](https://openairdocs.org/sdr/FDEA2020072751647), Jul 25, 2020: STRINGER. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 03EA FASTENER HOLES WITH CRACK INDICAT
- [SDR FDEA202005291078](https://openairdocs.org/sdr/FDEA202005291078), May 29, 2020: BATTERY. DISCHARGED. POST FLIGHT INSPECTION. L-1 DOOR EPAS BATTERY PACK STATUS LIGHT NOT FLASHING. REMOVED AND REPLACED THE 2 9V BATTERIES FOR THE L-1 EPAS BATTERY PACK IAW AMM 52-1
- [SDR FDEA202002200358](https://openairdocs.org/sdr/FDEA202002200358), Feb 20, 2020: SKIN. DAMAGED. WHILE ACCOMPLISHING E.O. #G-5310-EO332629 D P5 FOUND EXISTING UNDERWING LONGERON FASTENER HOLE AT LEFT HAND STATION 1014 AND STRINGER 36 LEFT OVERSIZED TO 0.403
- [SDR FDEA202002200357](https://openairdocs.org/sdr/FDEA202002200357), Feb 20, 2020: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND 02 CRACK INDICATION AROUND F
- [SDR FDEA202002140333](https://openairdocs.org/sdr/FDEA202002140333), Feb 13, 2020: SKIN. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UNDERWING LONGERON A
- [SDR FDEA202002140332](https://openairdocs.org/sdr/FDEA202002140332), Feb 13, 2020: SPAR. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON RIGHT HAND SIDE UNDERWING LONGERON LOWER WING FRONT SPAR CHORD AND FOUND 01 EACH HOLE WIT
- [SDR FDEA2020020650268](https://openairdocs.org/sdr/FDEA2020020650268), Feb 5, 2020: LONGERON. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT SIDE UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATIONS ON 02 EACH FASTENER AT VERTICAL FLANGE AN
- [SDR FDEA202002060267](https://openairdocs.org/sdr/FDEA202002060267), Feb 5, 2020: LONGERON. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT SIDE UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATIONS ON 02 EACH FASTENER AT VERTICAL FLANGE A
- [SDR FDEA2019101082496](https://openairdocs.org/sdr/FDEA2019101082496), Oct 8, 2019: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT TEST FAIL. FOUND LH SIDE EMERGENCY LIGHT BATTERY PACK UNSERVICEABLE. REPLACED BATTERY PACK ACC. AMM. 33-51-06. OPS CHECK FOUND SATISFACTORY.

All 72: https://openairdocs.org/model/boeing-777f28/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.