# N78866: 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: 32591
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 26, 2002
- Certificate issued: September 15, 2023
- Expires: September 30, 2030
- Mode S code: AAB187
- 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=78866
- Page: https://openairdocs.org/aircraft/N78866

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 N78866.

## NTSB investigations on N78866 not matched to an aircraft (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 FTW66D0123](https://openairdocs.org/ntsb/FTW66D0123), Jul 2, 1965: Mooney M21 (N78866), Gould, AR, substantial damage

## FAA accident and incident reports

None matched to N78866.

## Service difficulty reports (63, 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 CALA2026091419408](https://openairdocs.org/sdr/CALA2026091419408), Sep 11, 2026: SIGN. BROKEN. DOOR 2 OVERHEAD EMERGENCY EXIT SIGN LIGHT HOUSING LOOSE, FOUND DAMAGED MOUNTS, REPLACED THE EXIT SIGN AND PERFORMED EMERGENCY LIGHT OP CHECKED IAW AMM 33-51-00 
- [SDR CALA2026030314259](https://openairdocs.org/sdr/CALA2026030314259), Mar 1, 2026: DOOR SILL. CORRODED. R3 DOOR LOWER SILL HAD CORROSION. REPAIRED R3 DOOR LOWER SILL BTWN BS 1310 - 1370 IAW EC/RA 5310-08814.
- [SDR CALA2026021913914](https://openairdocs.org/sdr/CALA2026021913914), Feb 18, 2026: STRAP. GOUGED. L1 DOOR CUTOUT UPPER SILL INBOARD STRAP GOUGED BY DOOR SURROUND LINER HARDWARE. REPLACED L1 DOOR UPPER SILL INBOARD STRAP REF SRM 51-40-02 AND BOEING DWG 141N83
- [SDR CALA2026021913913](https://openairdocs.org/sdr/CALA2026021913913), Feb 18, 2026: STRUCTURE. CORRODED. SIGNS OF CORROSION FOUND AT INNER CHORD UPPER SURFACE APROX. BS 1459, S17R. SEE N/R 003197679 FOR ALL WORK PERFORMED.
- [SDR CALA2026021213723](https://openairdocs.org/sdr/CALA2026021213723), Feb 11, 2026: FLOORBEAM. CORRODED. FOUND CORROSION ON THE FLOORBEAM AT BS 333.40, BL 0, SEE BAM N/R 003182031 FOR WORK PERFORMED.
- [SDR CALA2025091508914](https://openairdocs.org/sdr/CALA2025091508914), Sep 12, 2025: SLIDE. NO DISCREPANCY. DOOR 4R SLIDE WILL NOT ARM, OPENED AND CLOSED DOOR 4R. ARMED SLIDE NORMALLY. OPS CHECK GOOD
- [SDR CALA2025073007082](https://openairdocs.org/sdr/CALA2025073007082), Jul 27, 2025: BOTTLE. FAULTED. OPERATIONAL TEST OF THE OFF-WING ESCAPE SLIDE PROCEDURE - REMOVED THE RIGHT INFLATION BOTTLE OF RIGHT OFF WING SLIDE SYSTEM DUE TO OPERATIONAL TEST REF AMM TASK
- [SDR CALA2025072106750](https://openairdocs.org/sdr/CALA2025072106750), Jul 17, 2025: SKIN. SCRATCHED. LEFT FUSELAGE SKIN APPOX. STA 418 TO STA. 428. HAS SCRATCH IN SKIN BETWEEN STR.17L AND 18L. FWD OF TAT SENSOR. REF LOG PAGE 5581101 BLENDED, REMOVED DAMAGE REF 
- [SDR CALA2025063006075](https://openairdocs.org/sdr/CALA2025063006075), Jun 25, 2025: CONTROL CABLE. OUT OF RIG. ON ROLL OUT FOR TAKE OFF CREW REPORTS AC PULLING TO THE RIGHT WITH FULL LH RUDDER PEDAL INOUT ON ROLL OUT FOR TAKE OFF CREW REPORTS AC PULLING TO THE RIGHT WITH
- [SDR CALA2025062605911](https://openairdocs.org/sdr/CALA2025062605911), Jun 24, 2025: BULB. BURNED OUT. MAIN CABIN R3 DOOR EMERGENCY EXIT SIGN HAS ONE BULB OUT. REPLACED THE LAMP L50 IAW AMM 33-51-01-962-001-002. OPS CHECK GOOD FOR L-50 AFTER CHARGING LIGHT IAW B7
- [SDR CALA2025062605910](https://openairdocs.org/sdr/CALA2025062605910), Jun 24, 2025: POWER SUPPLY. FAILED. EMERGENCY EXIT LIGHT BATTERY CHARGER M737 FAILS TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M737 AND OPS CHECK GOOD REF B757 AMM 33-51-07.
- [SDR CALA2025052004830](https://openairdocs.org/sdr/CALA2025052004830), May 16, 2025: LEVER. FAILED. DURING THE INSTALLATION OF DOOR 4 RIGHT EMERGENCY SLIDE, THE MANUAL ARM/DISARM LEVER FAILED THE OPERATIONAL CHECK DUE TO A BENT GIRT BAR, WHICH CAUSED THE BAR L
- [SDR CALA2025040703568](https://openairdocs.org/sdr/CALA2025040703568), Apr 4, 2025: LIGHT. DETACHED. 10C EMERGENCY FLOOR LGT HANGING R/R EPL ATTCHMENT HOUSING REF AMM 25-25-00. OPS CHECK GOO. PARTS USED: EMERGENCY LIGHTS - GENERAL VISUAL INSPECTION (ADDED BY EC
- [SDR CALA2025032803276](https://openairdocs.org/sdr/CALA2025032803276), Mar 27, 2025: LAMP. NO TEST. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - AISLE AREA LIGHT AT SEAT 32CBA INOP RELAMPED PER AMM 33-51-05-002-001 CK OK. PARTS USED: 99
- [SDR CALA2025022402460](https://openairdocs.org/sdr/CALA2025022402460), Feb 25, 2025: LAMP. NO TEST. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - #2 LEFT EXIT EMERGENCY LIGHT DOES NOT ILLUMINATE RELAMPED BULB OPERATIONAL CHECK GOOD.PARTS
- [SDR CALA2025010201752](https://openairdocs.org/sdr/CALA2025010201752), Dec 31, 2024: SENSOR. FAULTED. R ENG SPEED CARD AND R ENG BLEED OFF AND CTR R FUEL PUMP OFF AT SAME TIME AS RT ENG N3 FLUCTU PER CREW DEBRIEF CTR R FUEL PUMP, R PACK OFF & R ENG BLEED. N3 WAS
- [SDR CALA2024101800876](https://openairdocs.org/sdr/CALA2024101800876), Oct 17, 2024: STRINGER. CORRODED. POSIBLE CORROSION ON BELLY SKIN AT STA 1440 AND STR 30. CUTOUT DAMAGE SECTION, SKIN WAS NOT CORRODED. FABRICATED NEW SPLICE AND FILLER SEE TAG R06302 AND 44-000
- [SDR CALA2023050301315](https://openairdocs.org/sdr/CALA2023050301315), May 1, 2023: SKIN SPLICE. CORRODED. CORROSION FOUND IN LAP SPLICE STA 1660 RH SIDE S25R-S26R. NSPECTION THRESHOLD 37500 FLIGHT CYCLES AFTER AIRPLANE DELIVERY R COMES LATER, REF TABLE 206 ZONE A *[
- [SDR CALA2023041901155](https://openairdocs.org/sdr/CALA2023041901155), Apr 17, 2023: UNKNOWN. CORRODED. AFT LOWER CARGO DRAIN MAST DOUBLER AND SUPPORT BRACKETS HAS CORROSION. REMOVED DRAIN MAST DOUBLER AND BLENDED CORROSION FOUND 100% MATERIAL LOSS. FABRICATED AND
- [SDR CALA2022091402347](https://openairdocs.org/sdr/CALA2022091402347), Sep 14, 2022: NONE. NONE. REVERSER UNLOCK INDICATI ON DURING TAKEOFF. REJ ECTED AT AROUND 100KTS. BTS GOT TO 4 AT HIGHEST DEACTIVATED AND SECURED LEFT ENGINE THRUST REVERSER PER MEL DDP 
- [SDR CALA2022082402164](https://openairdocs.org/sdr/CALA2022082402164), Aug 24, 2022: WINDOW. OPEN. HIGH SPEED ABORT DUE TO FIRST OFFICERS WINDOW COMING OPEN ON TAK EOFF ROLL. HIGH ENERGY STOP INSPECTION COMPLETED ON L/P 9359946. PERFORMED OPERATIONAL CHECK OF
- [SDR CALA2022072001849](https://openairdocs.org/sdr/CALA2022072001849), Jul 20, 2022: BRAKE SYS. WARNING MESSAGE. RTO ON 17L AT 125KTS DUE TO HIGH EGT ON BOTH ENGS. BRAKE TEMPS 8 TOGW 229.4 CREW REPORTED A/C WAS ON 1HR BEFORE DEPARTURE, #1 ENG EGT SHOWED 117 BEFORE MOTORING
- [SDR CALA2022050901196](https://openairdocs.org/sdr/CALA2022050901196), May 9, 2022: NONE. INOPERATIVE. BOTH UTIL BUS OFF AT THRUST ADVANCEMENT FOR TO ADDING PICTURE REPLACED BPCU REF AMM24-41-03 OPS CHK GOOD NO LATCHED FAULTS IS FOUND ROTABLE PARTS CHANGE WAS IND
- [SDR CALA2022021400386](https://openairdocs.org/sdr/CALA2022021400386), Feb 14, 2022: COVER. MISSING. DOOR-MOUNTED ESCAPE SYSTEM DOOR 3L - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS FA REPORTS EMERGENCY TEST SWITCH
- [SDR CALA2021100601808](https://openairdocs.org/sdr/CALA2021100601808), Oct 6, 2021: NONE. NONE. STATUS MSG NOSE A/G DISAGREE REF FIM 32-09 FT 806, CLEANED & INSPECTED THE NLG NOT COMPRESSED SENSORS, NO DEFECTS NOTED. PER FIM 32-09 R&R PSEU. R&R
- [SDR CALA2020042400869](https://openairdocs.org/sdr/CALA2020042400869), Apr 23, 2020: FRAME. DENTED. B757-53-3-0523. AFT CARGO COMPARTMENT BS1400 S26L FRAME FOUND W ITH A DENT. MEASURED DENT AT AFT CARGO FRAME STA.1400 S26L FOUND TO BE WITH IN LIMITS IAW B757-3
- [SDR CALA2020042400867](https://openairdocs.org/sdr/CALA2020042400867), Apr 22, 2020: STRINGER. CRACKED. (B757-53-3-0559) STA 780+36 STR 16R CRACKED. REF ST-SAA NR 0091790. REMOVED DAMAGE STR AT STA780+36 STR-16R. ACCOMPLISHED PERMANENT REPAIR IAW B757-300 EC/RA 53
- [SDR CALA2020042400864](https://openairdocs.org/sdr/CALA2020042400864), Apr 21, 2020: FRAME. CRACKED. (CUSTOMER REQUEST - SUPPORT TASK) FRAME CRACKED AT FASTENER HOLE STATION 1580 BETWEEN STRINGERS 8R AND 9R. REF ST-SAA NR 0092124. CUTOUT CRACK L=1.250 W=1.050 A
- [SDR CALA2020042400862](https://openairdocs.org/sdr/CALA2020042400862), Apr 21, 2020: WEB. CRACKED. (B757-06-3-0374 R-4 DOOR UPPER INNER WEB AFT LIGHTNING HOLE IS C RACKED. REF ST-SAA NR0091847 CHECKED LIMITS TO CRACK AT R4 DOOR UPPER INNER SKIN; L=.25". OUT O
- [SDR CALA2020042400865](https://openairdocs.org/sdr/CALA2020042400865), Apr 21, 2020: FRAME. CRACKED. (CUSTOMER REQUEST - SUPPORT TASK) FRAME CRACKED AT FASTENER HOLE STATION 1580 BETWEEN STRINGERS 8L AND 9L. REF ST-SAA NR 0092123. CUTOUT CRACK 1.180 X 1.040 AND
- [SDR CALA2020042400859](https://openairdocs.org/sdr/CALA2020042400859), Apr 20, 2020: STRINGER. CRACKED. (B757-53-3-0559) STA 780+24 STR 16R CRACKED. REF ST-SAA NR 0091789. CHECKED LIMITS TO CRACKED STRINGER 16R AT STA 780+24; L=.40". OU T OF LIMITS IAW B757-300 SR
- [SDR CALA2020042400858](https://openairdocs.org/sdr/CALA2020042400858), Apr 19, 2020: STRINGER. CRACKED. (B757-53-3-0560) STA 780+24 STR 16L CRACKED. REF ST-SAA NR 00917 87. CHECKED LIMITS TO CRACKED STRINGER 16L AT STA 780+24 L+.70"; OUT OF LIMITS IAW B757-300 SRM
- [SDR CALA2020041700845](https://openairdocs.org/sdr/CALA2020041700845), Apr 15, 2020: BRACKET. CRACKED. (B757-06-3-0354) FWD CARGO DOOR UPPER FWD CORNER BRACKET CRACKED . REF ST-SAA NR 0091474. REMOVED AND REPLACED FWD CARGO DOOR UPPER FWD CORNER BRACKET IAW BOEIN
- [SDR CALA2020041300832](https://openairdocs.org/sdr/CALA2020041300832), Apr 12, 2020: SEAL DEPRESSOR. DENTED. (B757-06-3-0354) FWD CARGO AFT SEAL DEPRESSOR IS DENTED. REF ST- SAA NR 0091477. FOUND FWD CARGO DOOR AFT SEAL DEPRESSOR AT STA 615 S-20R TO S-25 R OUT OF LIMIT
- [SDR CALA2020041700838](https://openairdocs.org/sdr/CALA2020041700838), Apr 11, 2020: STRINGER. CRACKED. (B757-53-3-0560) STA 780 780+36 STR 16L CRACKED. REF ST-SAA NR 0 091788. FOUND STRINGER 16L AT STA 780+36 OUT OF LIMITS IAW B757-3 SRM 53 -30-03-R1 L=.750 CUTOU
- [SDR CALA2020041700837](https://openairdocs.org/sdr/CALA2020041700837), Apr 11, 2020: CREASE BEAM. CORRODED. (B757-53-3-0557) CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE,-LEADING UNDER DRAIN PAN AT L-2 LWR SILL, STA 730-740. R EF ST-SAA NR 0091960. FOUND LH 
- [SDR CALA2020041300829](https://openairdocs.org/sdr/CALA2020041300829), Apr 11, 2020: STRAP. CORRODED. (B757-49-3-8083) APU AIR INLET DOOR HOUSING FUSELAGE CUTOUT HAS CORROSION. REF ST-SAA NR 0091780. REMOVED CORROSION AND CHECKED LIMITS TO APU AIR INLET DOOR HOU
- [SDR CALA2020041300828](https://openairdocs.org/sdr/CALA2020041300828), Apr 11, 2020: PAN. ABNORMAL. (B757-53-3-0545) LH SIDE UPPER LOBE FUSELAGE L1 DOOR HANDLE PAN HAS TWO GOUGES. REF ST-SAA NR 0091391. CHECKED LIMITS TO 2EA GOUGES AT LH SIDE UPPER LOBE FUSELA
- [SDR CALA2019020100192](https://openairdocs.org/sdr/CALA2019020100192), Jan 29, 2019: SKIN. CORRODED. AFT AREA OF LAV SERVICE PANEL BETWEEN TRIM REINFORCING RING AND SKIN APPEARS TO HAVE CORROSION. LOG LOCKED FOR FERRY FLIGHT 2723-11JAN, HNL HOU, TO ACCOMPLISH R
- [SDR CALA2019020100191](https://openairdocs.org/sdr/CALA2019020100191), Jan 29, 2019: FRAME. CORRODED. REF L/P 9645024 FOUND CROSSION ON FRAME AT STATION 1560 S-27R AND S-28R REF FLEETCYCLE L/P 9645024 FOR ALL WORKED PERFORMED PLACED ON DI P IAW ECRA5360-01501 PA
- [SDR CALA2018020200442](https://openairdocs.org/sdr/CALA2018020200442), Feb 2, 2018: LIGHT. MISSING. DOOR 1L SLIDE LIGHT IS MISSING. INSTALLED MISSING LIGHT.
- [SDR CALA2017090102995](https://openairdocs.org/sdr/CALA2017090102995), Sep 1, 2017: LAMP. INOPERATIVE. L3 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-06.
- [SDR CALA2017050801291](https://openairdocs.org/sdr/CALA2017050801291), May 8, 2017: TRANSMITTER. FAULTY. AT CRUISE 34K FLIGHT LEVEL. EPR COMMAND TO 1.78 EPR ACTUAL NR1 EPR= 1.41 N1=78.7 EGT=545 N2=77 F/F=3.2, NR 2 EPR =1.74 N1=97 EGT=678 N2=89 F/F=5.7, A/T ON/OFF N
- [SDR CALA2015121300994](https://openairdocs.org/sdr/CALA2015121300994), Dec 13, 2015: ENGINE. MALFUNCTIONED. RIGHT ENG OIL PRESS 0, SHUT DOWN RT ENG. THE OIL PRESS LIGHT CAME ON DURING THE CLIMB. LEVELED OFF, SHUT DOWN & RETURNED. ENG SHUT DOWN FOR 20 MIN. R & R NR 2 E
- [SDR CALA2014080101062](https://openairdocs.org/sdr/CALA2014080101062), Aug 1, 2014: ENGINE. FAILED. LOW SPEED ABORT 80 KNOTS RT ENG OVER TEMP FOR TDR PURPOSES ONLY IAW LP 7750137 FOR ORIGINAL WRITE UP. R & R NR 2 ENG FOR STALLS & VIBRATIONS.
- [SDR CALA2014021100179](https://openairdocs.org/sdr/CALA2014021100179), Apr 23, 2014: FLOOR PANEL. CORRODED. AFT CARGO FLOOR & RAIL HAS HEAVY CORROSION BETWEEN STATION 1360 - 1380, CUT OUT DAMAGED AREA. FABRICATED REPAIRS & INSTALLED REPAIRS AT AFT CARGO FLOOR SIDE PAN
- [SDR CALA2014021000170](https://openairdocs.org/sdr/CALA2014021000170), Feb 7, 2014: LIGHT. INOPERATIVE. EXIT SIGN BULB OUT AFT OF 21DEF. RELAMPED EXIT SIGN AFT AT 21DEF & PERFORMED OPERATIONS CHECKED NORMAL IAW B757 AMM 33-51-10.
- [SDR CALA2014020700162](https://openairdocs.org/sdr/CALA2014020700162), Feb 4, 2014: WIRE. DAMAGED. L1 EMERGENCY LIGHT TEST SWITCH FAILED OPERATIONS CHECK. R & R WIRE W3752-0035-22 SPLICE IAW B757 AMM 33- 51-12 & BSWPM 20-30-12. PERFORMED EMERGENCY LIGHTS TEST
- [SDR CALA2014020700157](https://openairdocs.org/sdr/CALA2014020700157), Jan 31, 2014: ACCELEROMETER. FAULTY. ON CLIMB OUT, NR 1 ENG N3 INCREASED TO AMBER, RAN QRH, REDUCED THRUST FROM 89% N1 TO 75% N1 TO REMAIN OUT OF THE AMBER RANGE, DIVERTED TO HNL. R & R AVM ACCELER
- [SDR CALA2014012700114](https://openairdocs.org/sdr/CALA2014012700114), Jan 27, 2014: WEB. CORRODED. B757-53-3-0532 AFT GALLEY SUB FLOOR WEB HAS CORROSION STATION 1681 RBL 52. REMOVED CORROSION AT AFT GALLEY SUB FLOOR WEB, FOUND TO BE OUT LIMITS. FABRICATED REP

All 63: https://openairdocs.org/aircraft/N78866/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

## 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

---
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.