# N77865: 2002 Boeing 757-33N

- Status: Valid registration
- Airframe: [Boeing 757-33N](https://openairdocs.org/model/boeing-757-33n) (registry code 1384931, 275 seats)
- Engine: [Rolls-Royce RB-211-22 series](https://openairdocs.org/engine/rolls-royce-rb-211-22-series) (registry code 54554)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 32589
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 27, 2002
- Certificate issued: November 9, 2023
- Expires: November 30, 2030
- Mode S code: AA8A07
- Registered owner: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=77865
- Page: https://openairdocs.org/aircraft/N77865

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce RB-211-22 model are included.

## ADs that may apply (OpenAirDocs): 24 in force

### Matched by airframe (Boeing 757-33N)

None in force.

### Matched by engine (Rolls-Royce RB-211-22 series)

- [AD 2016-08-07](https://openairdocs.org/ad/2016-08-07): LPT support roller bearing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective May 16, 2016
- [AD 2010-17-10](https://openairdocs.org/ad/2010-17-10): Rear cooling air holes · Rolls-Royce RB211-22B-02, RB211-524B4-D-02, RB211-524D4-19 and 5 more. Effective Sep 27, 2010
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-14-21](https://openairdocs.org/ad/2003-14-21): Engine turbine cooling air overheat monitoring panel · Lockheed Martin L-1011-385-1, L-1011-385-1-14, L-1011-385-1-15 and 7 more. Effective Aug 25, 2003
- [AD 2003-13-12](https://openairdocs.org/ad/2003-13-12): Intermediate pressure (IP) compressor · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Aug 1, 2003
- [AD 2000-11-10](https://openairdocs.org/ad/2000-11-10): Rotor Shafts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524-02 and 23 more. Effective Aug 7, 2000
- [AD 87-23-04 R1](https://openairdocs.org/ad/87-23-04-R1): Low PressureTurbine Disk · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524-02 and 7 more. Effective May 31, 1989
- [AD 86-15-01 R2](https://openairdocs.org/ad/86-15-01-R2): Stage 1 And 2 HPC Disk Assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 23 more. Effective Jul 1, 1987
- [AD 86-24-05](https://openairdocs.org/ad/86-24-05): Rotors And Disks Oversped · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Dec 20, 1986
- [AD 86-20-09](https://openairdocs.org/ad/86-20-09): Intermediate Pressure Compressor (IPC) Stage 6 to 7 Rotor Assemblies · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Nov 4, 1986
- [AD 85-10-05 R1](https://openairdocs.org/ad/85-10-05-R1): Low Pressure Rotor Location Bearing Area Modifications · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 14 more. Effective Mar 28, 1986
- [AD 80-13-05 R1](https://openairdocs.org/ad/80-13-05-R1): (HPC) Rotor Stage 1 And 2 Disk Assembly · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Nov 28, 1983
- [AD 83-01-03](https://openairdocs.org/ad/83-01-03): Disk Assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Feb 17, 1983
- [AD 82-12-05](https://openairdocs.org/ad/82-12-05): Fan Assembly · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Jun 7, 1982
- [AD 78-19-01](https://openairdocs.org/ad/78-19-01): High Pressure Turbine Discs · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Sep 25, 1978
- [AD 76-26-01](https://openairdocs.org/ad/76-26-01): H.P. Turbine Disc · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Jan 3, 1977
- [AD 76-15-09](https://openairdocs.org/ad/76-15-09): Engine Shutdown · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700 and RB211-22C-02. Effective Jul 22, 1976
- [AD 75-16-09](https://openairdocs.org/ad/75-16-09): HS External Gearbox Oil Tank Filler Cap And Housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Aug 27, 1975
- [AD 75-16-08](https://openairdocs.org/ad/75-16-08): Intermediate and High Pressure Compressors · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Aug 22, 1975
- [AD 73-10-01](https://openairdocs.org/ad/73-10-01): VIGV Scheduling · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700 and RB211-22C-02. Effective May 8, 1973

### Historical (superseded or no longer in force)

- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2001-23-02](https://openairdocs.org/ad/2001-23-02) (historical): High Pressure Turbine Disks · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 2 more. Effective Dec 24, 2001
- [AD 94-18-03](https://openairdocs.org/ad/94-18-03) (historical): Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524-02 and 23 more. Effective Sep 26, 1994

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N77865.

## FAA accident and incident reports

None matched to N77865.

## Service difficulty reports (114, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA2026083118994](https://openairdocs.org/sdr/CALA2026083118994), Aug 27, 2026: LAMP. FAULTY. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE, DOOR 2L EXTERIOR SLIDE LIGHT INOP. REPLACED THE LAMPS IAW AMM 33-51-06-962-001-002. OPS TEST
- [SDR CALA2026080918372](https://openairdocs.org/sdr/CALA2026080918372), Aug 5, 2026: SURVIVAL KIT. WRONG PART. VERIFY THE AIRCRAFT HAS THE CORRECT NUMBER OF SURVIVAL KIT PACK ASSY AND VERIFY SERIAL NUMBERS. INSPECTED AND FOUND 6 SURVIVAL KITS LOCATED ONBOARD IN 3 DROPDOW
- [SDR CALA2026031014475](https://openairdocs.org/sdr/CALA2026031014475), Mar 9, 2026: CHARGER. INOPERATIVE. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - 1R EXIT IDENTIFIER SIGN INOP. R & R M731 EMERGENCY BATTERY CHARGER, IAW AMM 33-51-07-862-02
- [SDR CALA2026011913049](https://openairdocs.org/sdr/CALA2026011913049), Jan 14, 2026: SKIN. CORRODED. FUSELAGE SKIN INTERNAL BETWEEN BS 879 - 900 BLIGE CENTER LINE HAS CORROSION (EXFOLIATED). REPAIR ACCOMPLISHED IAW ECRA 5330-07683. MAJOR REPAIR. PERFORMED A REP
- [SDR CALA2026012813411](https://openairdocs.org/sdr/CALA2026012813411), Jan 11, 2026: FRAME. DENTED. DURING C-CHECK, MX REPORTED ONE DENT ON INBD FLANGE OF BS 500 FRAME, S-15L & 16L. ACCOMP A REPAIR IAW ECRA 5330-07671, PART 1, STEP 1 WITH NO DEVIATIONS.
- [SDR CALA2026012713358](https://openairdocs.org/sdr/CALA2026012713358), Jan 11, 2026: SKIN. CORRODED. DURING C-CHECK, THREE CORROSION DAMAGES ON BS 1420 FRAME BOTTOM BETWEEN S29L & S30, S29R & S30 AND S28R & S29R. PERFORMED A REPAIR IAW 757-5360-13-A4238,
- [SDR CALA2026012813413](https://openairdocs.org/sdr/CALA2026012813413), Jan 9, 2026: FRAME. CORRODED. DURING C-CHECK, THREE CORROSION DAMAGES ON BS 1420 FRAME BTWN S29-30L, S29-30R & S28-29R. MAJOR REPAIR ACCOMPLISHED AND ALL RII STEPS C/W.
- [SDR CALA2026012813412](https://openairdocs.org/sdr/CALA2026012813412), Jan 9, 2026: FRAME. CORRODED. CORROSION DAMAGE ON BS 1460 FRAME BOTTOM BETWEEN S29 -30R. PERFORMED AN INSPECTION IAW PART 2 OF THE LATEST REVISION OF ECRA 5360-02086. ACCOMPLISHED MAJOR REPA
- [SDR CALA2026010712745](https://openairdocs.org/sdr/CALA2026010712745), Jan 4, 2026: FRAME. DENTED. BULK CARGO, BS 1480, LOWER SIDEWALL, S26 - 27L, FRAME HAD A DENT. ACCOMPLSHED REPAIR IAW EA 757-5360-13-A4239, FIGURE 1 - 7, WITH NO DEVIATIONS IAW EC/RA 5360-0
- [SDR CALA2026012813414](https://openairdocs.org/sdr/CALA2026012813414), Jan 2, 2026: FRAME. DENTED. DURING C-CHECK, MAINTENANCE REPORTED ONE DENT, BS 1480 FRAME BOTTOM BTWN S26-27L. THE DENT MEASURED 0.860 INCH LONG, 0.390 INCH WIDE, AND 0.011 INCH DEEP. ACCOM
- [SDR CALA2026012713356](https://openairdocs.org/sdr/CALA2026012713356), Jan 2, 2026: FRAME. DENTED. DURING C-CHECK, MAINTENANCE REPORTED ONE DENT ON BS 1480 FRAME BOTTOM BETWEEN S26L AND S27L. THE DENT MEASURED 0.860 INCH LONG, 0.390 INCH WIDE, AND 0.011 INCH 
- [SDR CALA2026012713355](https://openairdocs.org/sdr/CALA2026012713355), Jan 2, 2026: FRAME. DENTED. DURING THE C-CHECK MAINTENANCE REPORTED ONE DENT ON INBD FLANGE OF THE BS 500 LT FRAME BTWN S15L AND S16L. MAJOR REPAIR
- [SDR CALA2026011212865](https://openairdocs.org/sdr/CALA2026011212865), Dec 24, 2025: FRAME. CORRODED. AFT CARGO, FLOOR AREA, BS 1460, BTWN STG 29R TO STG 30, FRAME HAS CORROSION. PART FABRICATED IN HOUSE PER DWG146N2063 AND DWG 140N2063. PERFORMED A REPAIR IAW 7
- [SDR CALA2026011212864](https://openairdocs.org/sdr/CALA2026011212864), Dec 24, 2025: FRAME. CORRODED. AFT CARGO, FLOOR AREA, BS 1420, BTWN S29L - 28R, FRAME HAS CORROSION. PART FABRICATED IAW DWG 146N5426, REV A. PERFORMED A REPAIR IAW 757-5360-13-A4238 F IGURES
- [SDR CALA2025123012522](https://openairdocs.org/sdr/CALA2025123012522), Dec 24, 2025: FLOOR SUPPORT. CORRODED. AFT CARGO, FLOOR SUPPORT, BS 1400 - 1420, S29 - 30L., CORRODED. REMOVED IAW SRM 53-60-04-1A-0, FIG 101, SHEET 2, DETA IL II. FABRICATED A NEW FLOOR SUPPORT AND 
- [SDR CALA2025123012521](https://openairdocs.org/sdr/CALA2025123012521), Dec 24, 2025: FLOOR SUPPORT. CORRODED. AFT CARGO, FLOOR SUPPORT, BS 1400 - 1420, S29 - 30R, CORRODED. BLENDED REPAIR WITHIN LIMITS.
- [SDR CALA2025122312377](https://openairdocs.org/sdr/CALA2025122312377), Dec 20, 2025: WINDOW FRAME. DENTED. MAIN CABIN, LT BS 500 BELOW PASSENGER WINDOW FRAME HAD A DENT. REPAIRED THE WINDOW FRAME BS 500 BTW S15L AND S16L IAW EC/RA 53 30-07671 AND EA 757-5330-13-A4230
- [SDR CALA2025122312361](https://openairdocs.org/sdr/CALA2025122312361), Dec 20, 2025: BRACKET. CORRODED. BULK CARGO, BS 1520 ABOVE STRINGER 30R, ANGLE BRACKET WAS CORRODED. R & R THE BRACKET BS 1520, S20 - 30R IAW SRM 51-40-02-OG-0.
- [SDR CALA2026010212591](https://openairdocs.org/sdr/CALA2026010212591), Dec 19, 2025: FLOOR SUPPORT. CORRODED. BULK CARGO, BETWEEN BS 1500 - 1520, FLOOR SUPPORTS HAVE CORROSION AT NUTPLATES AREA (4 PLACES). PART FABRICATED REMOVED AND REPLACED FLOOR SUPPORT AT AFT CARGO 
- [SDR CALA2025122312346](https://openairdocs.org/sdr/CALA2025122312346), Dec 19, 2025: FLOOR SUPPORT. CORRODED. BULK CARGO, FLOOR AREA, CLOSE TO BS 1500, BETWEEN S29 - 30, FLOOR SUPPORT SPLICE HAS CORROSION. REMOVED AND REPLACED TWO FLOOR SUPPORT SPLICES IN THE AFT CARGO 
- [SDR CALA2025122312344](https://openairdocs.org/sdr/CALA2025122312344), Dec 19, 2025: DRAG FITTING. CRACKED. NDT ROTO INSPECTION ON NR 1 ENG PYLON DRAG FITTING. NOTED A CRACK IN HOLE NR 8 AT TOP OF SKIN AT THE 3 O'CLOCK. ACCOMPLISHED A REPAIR IAW EA 757-5720-13-A4226, 
- [SDR CALA2025121912257](https://openairdocs.org/sdr/CALA2025121912257), Dec 17, 2025: LONGERON. CORRODED. APU COMPARTMENT LT BS 1885-1890 ABOVE APU DOOR LONGERON, METALIC HONEYCOMB SKIN INNER SURFACE CORRODED. REPAIRED AREA OF APU COMPT. LT BS 1885-1890 IAW SRM 51 -
- [SDR CALA2025121912255](https://openairdocs.org/sdr/CALA2025121912255), Dec 17, 2025: SKIN. CRACKED. EA 5210-03219 REV C: L4 ENTRY DOOR INTERNAL STRUCTURE CRACKED WITH LOCAL PERFORATION THROUGH SKIN, LOCATED BTWN THE UPPER HINGE FITTING AREA. PERFORMED REPAIR I
- [SDR CALA2025122212292](https://openairdocs.org/sdr/CALA2025122212292), Dec 13, 2025: FITTING. CRACKED. L2 DOOR CUTOUT, FWD FRAME, MECHANISM, SUPPORT STRUCTURE IS CRACKED. REMOVED AND REPLACED FITTING ON L2 DOOR FWD CUTOUT FRAME BS 684 -692.38. IAW SRM 51-40-02-0G
- [SDR CALA2025122412387](https://openairdocs.org/sdr/CALA2025122412387), Dec 12, 2025: ANGLE. CORRODED. FUSELAGE APU INLET DOOR CUTOUT BS 1825, STRINGERS 3-6R, INNER STRAP HAS EXFOLIATION. AFT STRAP WAS REPAIRED IAW SRM 53-80-15-2R-1, REPAIR 1, FIGURE 202, DETAIL 
- [SDR CALA2025121512096](https://openairdocs.org/sdr/CALA2025121512096), Dec 12, 2025: PLUG. DAMAGED. (SDR)(19-0671-1-0004) CUSTOMER REQUEST - DO A HIDDEN DAMAGE INSP ECTION AT NUMBER 2 ENG DUE TO A BORESCOPE PLUG MISSING AT THE LP COMPRESSOR I/B UPR FAIRING ARE
- [SDR CALA2025121512094](https://openairdocs.org/sdr/CALA2025121512094), Dec 12, 2025: PLATE. CORRODED. UPON REMOVAL OF TRANSITION PANEL AFT CARGO COMPARTMENT FR1380/S26R-S27R, FOUND PLATE WITH CORROSION. REF N RC 137865. REMOVED AND REPLACED SPLICE AT AFT CARGO C
- [SDR CALA2026011913084](https://openairdocs.org/sdr/CALA2026011913084), Dec 8, 2025: TRANSITION PANEL. CORRODED. BULK CARGO, FLOOR AREA, BS 1520 , RT TRANSITION PANEL LOWER SURFACE HAS CORROSION. PERFORMED REPAIR AT TRANSITION PANEL BS 1520 TO 1640 IAW SRM 53-00-53-2R-2.
- [SDR CALA2025121011990](https://openairdocs.org/sdr/CALA2025121011990), Dec 8, 2025: STRINGER CLIP. CORRODED. STRINGER CLIP CORRODED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-OG-0.
- [SDR CALA2025121011988](https://openairdocs.org/sdr/CALA2025121011988), Dec 8, 2025: SKIN. CORRODED. AFT CABIN METALIC PRESSURE DECK BETWEEN BS 1680 - 1720, UPPER SURFACE CORRODED BETWEEN LT CREASE BEAM TO RT CREASE BEAM. REF NRC 137952. REMOVED CORROSION AT AF
- [SDR CALA2025120811873](https://openairdocs.org/sdr/CALA2025120811873), Dec 5, 2025: ANGLE. CORRODED. UPON REMOVAL OF TRANSITION PANEL AT AFT CARGO BAY BS 1360 - 1380, S26R - S27R, FOUND WEB ASSY WITH CORROSION. REMOVED AND EVALUATED DAMAGE AT WEB ASSY AND FOUND
- [SDR CALA2025120811867](https://openairdocs.org/sdr/CALA2025120811867), Dec 5, 2025: TEE ANGLE. CORRODED. CORROSION FOUND AT TEE CHORD LOWER SURFACE AT BS 900 BOTTOM SECTION. PERFORMED TEE CHORD REPAIR ON BS 900 BOTTOM, FABRICATED PARTS ON TRAVELER'S T25/1841651, T2
- [SDR CALA2025120511807](https://openairdocs.org/sdr/CALA2025120511807), Dec 4, 2025: BRACKET. CRACKED. ONE BRACKET CRACKED AT THE LOWER LEFT WING OT BODY FAIRING STRUCTURE AT BS 1040, LOCATED AT THE FWD END OF THE BEAM. REMOVED AND REPLACED THE BRACKET ON LT WTB 
- [SDR CALA2025120811847](https://openairdocs.org/sdr/CALA2025120811847), Dec 3, 2025: BRACKET. CORRODED. RIGHT UPPER WTB, UNDER FAIRINGS, BTWN BS 1080 - 1100, PANEL BRACKET SUPPORT HAS CORROSION. REMOVED AND REPLACED TEE BRACKET ON RT WING UPPER WTB STRUCTURE AT BS
- [SDR CALA2025120411773](https://openairdocs.org/sdr/CALA2025120411773), Dec 3, 2025: CHANNEL. CORRODED. L1 DOOR LOWER CUTOUT ATTACHED INTERCOSTAL CORRODED. REMOVED AND REPLACED TWO EA CHANNELS AT L1 DOOR LOWER CUTOUT IAW SRM 51-40-02-0G-0.
- [SDR CALA2025120211640](https://openairdocs.org/sdr/CALA2025120211640), Nov 28, 2025: CREASE BEAM. CORRODED. (SDR) MAIN DECK RH SIDE CREASE BEAM BETWEEN STA 1290 AND STA 140 0 HAS CORROSION EXFOLIATED. ESFR ENTRY CREASE BEAM WAS EXFOLIATED REMOVE DAMAGE CREASE BEAM IAW
- [SDR CALA2025112711524](https://openairdocs.org/sdr/CALA2025112711524), Nov 26, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK FLOOR AREA RBL 1 AT FR 352 FLOOR SUPPORT HAS SURFACE CORROSION. PERFORMED REPAIR AT MAIN DECK FLOOR SUPPORT BETWEEN RBL 1 FR 352 IAW SRM 51-70-11-0G-0
- [SDR CALA2025112111396](https://openairdocs.org/sdr/CALA2025112111396), Nov 20, 2025: SEAT TRACK. CORRODED. CORROSION ON CABIN SEAT TRACK CENTER OF CROWN, LBL 46, BS 1080 - 1180. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02-0G-0.
- [SDR CALA2025112111394](https://openairdocs.org/sdr/CALA2025112111394), Nov 20, 2025: SEAT TRACK. CORRODED. CORROSION ON CABIN SEAT TRACK CENTER OF CROWN RBL 46, BS 1060 - 1180. REMOVED CORROSION IAW AMM 51-00-53-102-054; EVALUATED AS FOLLOW 0. THICKNESS 0.185", MATER
- [SDR CALA2025111911336](https://openairdocs.org/sdr/CALA2025111911336), Nov 17, 2025: FLOOR SUPPORT. CORRODED. CORROSION UNDER THE NUTPLATE AT CABIN FLOOR STRUCTURE BS 353 RBL 24. REMOVED CORROSION AT CABIN FLOOR STRUCTURE STA 353 RBL 24 IAW B7 57-300 SRM 51-10-02-0G, CH
- [SDR CALA2025111911334](https://openairdocs.org/sdr/CALA2025111911334), Nov 17, 2025: FRAME. CORRODED. AFT CARGO, FLOOR AREA, BS 1440, BTWN S29 - 30L, FRAME HAS CORROSION. REMOVED AND REPLACED DOUBLER IAW SRM 53-60-07-1A-0, SRM 51-40- 02, & DWG 146N1013, REV B. R
- [SDR CALA2025091108792](https://openairdocs.org/sdr/CALA2025091108792), Sep 7, 2025: VALVE. MALFUNCTIONED. LEFT ENG HIGH STAGE EICAS C, THE LEFT ENGINE HPSOV IS CLOSED BECAUSE THE HIGH STAGE BLEED PRESSURETOO HIGH. CREW ABORTED TAKEOFF AT APPROX 20KTS. REF MEL 3611P 
- [SDR CALA2025081807861](https://openairdocs.org/sdr/CALA2025081807861), Aug 15, 2025: OIL SYSTEM. OVERSERVICED. FAULT LIGHT ON DURING APU START. SECOND ATTEMPT MADE AFTER CLEARING FAULT. PERFORMED APU ECB BITE IAW FIM 49-11 TASK 875 & NOTED LOW OIL PRESSURE FLAG ON LAST 3
- [SDR CALA2025081107567](https://openairdocs.org/sdr/CALA2025081107567), Aug 9, 2025: SKIN. GOUGED. IMPACT DAMAGE TO SKIN WITH MULTIPLE DEEP SCRATCHES & GOUGES, JUST BELOW & AFT OF AFT CARGO DOOR, BETWEEN S27R & 28R RUNNING FROM APPROX 6" FWD OF FRAME 1460 TO 
- [SDR CALA2025080707410](https://openairdocs.org/sdr/CALA2025080707410), Aug 4, 2025: BOTTLE. NO DISCREPANCY. R2 DOOR SLIDE AND BOTTLE, PLEASE VERIFY R2 DOOR-MOUNTED ESCAPE SLIDE BOTTLES EXPIRATION DATE AND THE SLIDE EXPIRATION DATE AND CONTACT TOMC WITH THE DATES ON BO
- [SDR CALA2025072206840](https://openairdocs.org/sdr/CALA2025072206840), Jul 18, 2025: ACCESS DOOR. MISSING. PDA 1 ENG #2 OIL SERVICING DOOR MISSING ON ARRIVAL. PRESUME PANEL DEPARTED FROM AC LOGPAGES 5605104, 5605196 ASSOCIATED WITH THIS LOGPAGE... INSTALLED NEW OIL S
- [SDR CALA2025063006044](https://openairdocs.org/sdr/CALA2025063006044), Jun 26, 2025: HANDLE. FALSE INDICATION. DOOR 2L SLIDE LIGHT NOT ILLUMINATING WITH HANDLE ARMED. CYCLED DOOR HANDLE AND CHEKED OK. NO MX ACTION. OPS CHECKS GOOD MULTIPLE TIMES.
- [SDR CALA2025062605931](https://openairdocs.org/sdr/CALA2025062605931), Jun 22, 2025: IDG. FAULTY. GENERATOR DRIVE SYSTEM EICAS MESSAGE (01=L,02=R) GEN DRIVE DISPL AYED. GEN DRIVE LIGHT ON. GEN DRIVE DISCONNECTED 02 ON CLIMB OUT COMPLETED CHECKLIST"R IDG OIL 
- [SDR CALA2025040103390](https://openairdocs.org/sdr/CALA2025040103390), Mar 28, 2025: BATTERY PACK. INOPERATIVE. (SUPPORT TASK) EMERGENCY PACK AT LOCATION M11486 THAT FAILED OPS CHECK AND WAS REEMOVED AND REPLACED ON LOG PAGE 9286036, BATTERY PACK WAS REMOVED AND REPLACED 
- [SDR CALA2025040103389](https://openairdocs.org/sdr/CALA2025040103389), Mar 28, 2025: BATTERY PACK. INOPERATIVE. (SUPPORT TASK) EMERGENCY BATTERY PACK AT LOCATION M736 THAT FAILED OPS CHECK AND WAS REMOVED AND REPLACED ON LOG PAGE 9286036. BATTERY PACK WAS REMOVED AND REPL

All 114: https://openairdocs.org/aircraft/N77865/reports.md

## STCs that may be installed (OpenAirDocs) (2)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Rolls-Royce RB-211-22 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-22B-02
- [STC SE1516CE](https://openairdocs.org/stc/SE1516CE): Modification of lower fuel control box assembly to incorporate vibration isolators. Trans World Airlines Inc. Lists RB211-22B-02

## Earlier aircraft with N77865

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N77865 before.

- [Cancelled 1955-10-12](https://openairdocs.org/deregistered/N77865-1955-10-12): Luscombe 8A, S/N 3592, built 1946. Owner: [Wiggins E H](https://openairdocs.org/faa-owner/WIGGINS%20E%20H), [Edenton, NC](https://openairdocs.org/faa-place/NC/Edenton)

## Related

- Other Boeing 757-33N aircraft: https://openairdocs.org/model/boeing-757-33n/aircraft.md
- The Rolls-Royce RB-211-22 series engine: https://openairdocs.org/engine/rolls-royce-rb-211-22-series.md

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