# N419UP: 1990 Boeing 757-24APF

- Status: Valid registration
- Airframe: [Boeing 757-24APF](https://openairdocs.org/model/boeing-757-24apf) (registry code 1384969, 178 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 23906
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 29, 2007
- Certificate issued: July 31, 1998
- Expires: November 30, 2027
- Mode S code: A4F75F
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=419UP
- Page: https://openairdocs.org/aircraft/N419UP

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 RB211-535E4 model are included.

## ADs that may apply (OpenAirDocs): 20 in force

### Matched by airframe (Boeing 757-24APF)

None in force.

### Matched by engine (Rolls-Royce RB211-535E4 series)

- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2012-02-11](https://openairdocs.org/ad/2012-02-11): LP turbine stage 1, 2, and 3 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Mar 6, 2012
- [AD 2009-20-14](https://openairdocs.org/ad/2009-20-14): Eddy current inspection (ECI) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Nov 17, 2009
- [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 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [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 2003-10-03 R1](https://openairdocs.org/ad/2003-10-03-R1): High pressure (HP) turbine discs · Rolls-Royce RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2001-19-05](https://openairdocs.org/ad/2001-19-05): High Speed Gearbox Drive · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Oct 11, 2001
- [AD 2000-09-14](https://openairdocs.org/ad/2000-09-14): Radial Drive Steady Bearings · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Jul 11, 2000
- [AD 97-02-12](https://openairdocs.org/ad/97-02-12): Fuel Flow Governor (FFG) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 4, 1997
- [AD 87-25-04](https://openairdocs.org/ad/87-25-04): Fuel Quantity Indication System · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Dec 8, 1987

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

- [AD 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008
- [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 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [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 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003
- [AD 2003-12-15](https://openairdocs.org/ad/2003-12-15) (historical): LPC fan blade roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jul 30, 2003
- [AD 2003-10-03](https://openairdocs.org/ad/2003-10-03) (historical): High Pressure (HP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2002-23-08](https://openairdocs.org/ad/2002-23-08) (historical): Low Pressure (LP) Turbine Stage 2 Discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 30, 2002
- [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 98-07-07](https://openairdocs.org/ad/98-07-07) (historical): Fuel System Tube Assembly · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 29, 1998
- [AD 86-07-01](https://openairdocs.org/ad/86-07-01) (historical): Outer Combustion Case Inspection · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective May 16, 1986

## Information bulletins (advisory) (1 in force)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N419UP.

## FAA accident and incident reports

None matched to N419UP.

## Service difficulty reports (204, 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 IPXA2026101627405](https://openairdocs.org/sdr/IPXA2026101627405), Aug 26, 2026: ANGLE. CORRODED. APU INLET SURROUND STRUCTURE FWD STRAP, UPPR AND LWR MID ANGLES, AND UPPR AND LWR FWD CORNER ANGLES HAVE EXFOLIATING CORROSION. VERIFIED STEP 32. REF. RII GMM 0
- [SDR IPXA2026101651749](https://openairdocs.org/sdr/IPXA2026101651749), Aug 18, 2026: NUT PLATE. CORRODED. EXFOLATION FOUND AT MAIN CARGO DECK FS 1680 LBL 39.5 REMOVED 5 EA NUT-PLATE SUPPORTS ASSY, FOR ACCESS AT MAIN CARGO DECK, FLOOR STRUCTURE ON STEP 7.
- [SDR IPXA2026101477713](https://openairdocs.org/sdr/IPXA2026101477713), Aug 13, 2026: DECK PLATE. CORRODED. MAJOR REPAIR, MAIN DECK CARGO, AFT DECK PLATE UPPER SURFACE HAD SEVERAL AREAS OF CORROSION, BS 1680 - 1700. REPAIRED IAW SRM 53-60-51-2R-5, REPAIR 5, FIGURE 201
- [SDR IPXA2026101456536](https://openairdocs.org/sdr/IPXA2026101456536), Aug 6, 2026: SKIN. DEBONDED. MAJOR REPAIR, LT ELEVATOR UPPER SKIN HAS ONE AREA OF DEBONDING 3 INCHES FROM T/E AND 4 INCHES OTBS OF ELEV STA 108.
- [SDR IPXA2026071686469](https://openairdocs.org/sdr/IPXA2026071686469), Jul 16, 2026: SEAT TRACK. CORRODED. AFTER REMOVAL OF MAIN CARGO DECK FLOOR BOARD, FOUND SEAT TRACK FLANGE UNDERLYING SURFACE NUT PLATE ATTACHMENT IS CORRODED BTWN STA. 1661 TO 1681.8 ALONG LBL 45.
- [SDR IPXA2026101472452](https://openairdocs.org/sdr/IPXA2026101472452), Jul 15, 2026: SKIN. DENTED. MAJOR REPAIR. CREW ENTRY DOOR BTWN BS 297 - 324, STR 9L - 14L HAD SEVERAL DENTS STEPS 19- 24, 28 AND 30 ARE RII IAW GMM 04-02.
- [SDR IPXA2026071692059](https://openairdocs.org/sdr/IPXA2026071692059), Jul 3, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SECTION 46 FLOOR STRUCTURE DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, RBL 36,
- [SDR IPXA2026071692063](https://openairdocs.org/sdr/IPXA2026071692063), Jul 3, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SECTION 46 FLOOR STRUCTURE DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, RBL 23,
- [SDR IPXA2026071692147](https://openairdocs.org/sdr/IPXA2026071692147), Jul 3, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SECTION 46 FLOOR STRUCTURE DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, RBL 12,
- [SDR IPXA2026071692206](https://openairdocs.org/sdr/IPXA2026071692206), Jul 3, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SECTION 46 FLOOR STRUCTURE DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, RBL 5,
- [SDR IPXA2026071692214](https://openairdocs.org/sdr/IPXA2026071692214), Jul 3, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SECTION 46 FLOOR STRUCTURE DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, LBL 12,
- [SDR IPXA2026071692277](https://openairdocs.org/sdr/IPXA2026071692277), Jul 3, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SECTION 46 FLOOR STRUCTURE DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, LBL 23, & 2.
- [SDR IPXA2026071692292](https://openairdocs.org/sdr/IPXA2026071692292), Jul 3, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SECTION 46 FLOOR STRUCTURE DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, LBL 36,
- [SDR IPXA2026071690616](https://openairdocs.org/sdr/IPXA2026071690616), Jun 27, 2026: FLOORBEAM. CORRODED. FWD CARGO RH OTBD SIDE STA 620 MAIN CABIN FLOORBEAM UPPER FLANGE LOWER SURFCE EXFOLIATED.
- [SDR IPXA2026073059903](https://openairdocs.org/sdr/IPXA2026073059903), Jun 25, 2026: ANGLE. CRACKED. NR 2 PYLON O/B AFT HAS A CRACKED SUPPORT BRACKET MARKED JK-24. INSTALLED NEW ANGLE BRACKET TO #2 PYLON O/B AFT SIDE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026071613931](https://openairdocs.org/sdr/IPXA2026071613931), Jun 23, 2026: FLOORBOARD. CORRODED. MAIN CARGO AFT FLOORBOARD 251XRF HAS SEVERAL CORRODED AND BROKEN FASTENER INSERTS.
- [SDR IPXA2026071614428](https://openairdocs.org/sdr/IPXA2026071614428), Jun 23, 2026: FLOORBOARD. CORRODED. MAIN CARGO AFT FLOORBOARD 252XUF HAS SEVERAL CORRODED AND BROKEN FASTENER INSERTS. VERIFIED STEP 1 HAS BEEN ACCOMPLISHED.
- [SDR IPXA2026050962784](https://openairdocs.org/sdr/IPXA2026050962784), Apr 30, 2026: ACCESS PANEL. DAMAGED. MAJOR REPAIR, LT VERTICAL STABILIZER ACCESS PANEL 322DL, AT FSS 295.915 TO 371.308, HAD HAIL DAMAGE.
- [SDR IPXA2025060293029](https://openairdocs.org/sdr/IPXA2025060293029), Jun 1, 2025: CONTROLLER. FAULTED. CABIN ALT R&R'D ACTUATOR REF AMM 21-31-04-404-009, PERFORMED OPERATINAL CHECK OF AUTO 1, AUTO 2, AND MAN, OPS CHECK GOOD. PERFORMED OPERATIONAL CHECK OF AUTO 1,
- [SDR IPXA2025040419949](https://openairdocs.org/sdr/IPXA2025040419949), Apr 3, 2025: GUARD. INOPERATIVE. EMER LIGHT ARM SWITCH COVER INOP REPLACED SWITCH GUARD PER AMM 33-51-04.
- [SDR IPXA2025011826131](https://openairdocs.org/sdr/IPXA2025011826131), Jan 16, 2025: NONE. NONE. REF HEAVY CHECK REPAIR T3F18E0056FMQ, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3769, REV- COMPLETED.
- [SDR IPXA2025011826183](https://openairdocs.org/sdr/IPXA2025011826183), Jan 16, 2025: NONE. NONE. REF HEAVY CHECK REPAIR T3F18E0056FHS, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3770, REV- COMPLETED.
- [SDR IPXA2024122713695](https://openairdocs.org/sdr/IPXA2024122713695), Dec 27, 2024: SWIVEL. DAMAGED. ON APPROACH TO KRFD CONFIGURED @FLAPS 25 + GEAR DOWN WE GO A GEAR DOOR LIGHT, FOLLOWED BY A DOOR DISAG, FOLLOWED BY A L HYD QTY AND L HYD PRESS. WE EXECUTED A M
- [SDR IPXA2024092267037](https://openairdocs.org/sdr/IPXA2024092267037), Sep 18, 2024: SUPPORT BRACKET. CRACKED. FWD PRESSURE BULKHEAD FWD MID AND AFT SUPPORT BRACKETS CRACKED. ALL WORK ACCOMPLISHED PER UPS EO-91446-REQ1 AND VT MAE EA 757-2555-27-A3689 REV-.
- [SDR IPXA2024092491833](https://openairdocs.org/sdr/IPXA2024092491833), Sep 14, 2024: GAUGE. DAMAGED. CREW ENTRY DOOR, LOWER LATCH HOOK W/GAUGE DAMAGE; DOT-005, JR-117. VERIFIED WORK ACCOMPLISHED PER SREO-14721-REQ001. REVIEWED
- [SDR IPXA2024092491775](https://openairdocs.org/sdr/IPXA2024092491775), Sep 14, 2024: HOOK. DAMAGED. CREW ENTRY DOOR, UPPER LATCH HOOK W/GAUGE DAMAGE; DOT-004, JR-117. VERIFIED WORK ACCOMPLISHED PER SREO-14721-REQ001. REVIEWED
- [SDR IPXA2024091691775](https://openairdocs.org/sdr/IPXA2024091691775), Sep 14, 2024: LATCH. DAMAGED. CREW ENTRY DOOR, UPPER LATCH HOOK W/GAUGE DAMAGE; DOT-004, JR-117. APPROVED.
- [SDR IPXA2024091691833](https://openairdocs.org/sdr/IPXA2024091691833), Sep 14, 2024: HOOK. DAMAGED. CREW ENTRY DOOR, LOWER LATCH HOOK W/GAUGE DAMAGE; DOT-005, JR-117.
- [SDR IPXA2024091982984](https://openairdocs.org/sdr/IPXA2024091982984), Sep 13, 2024: FRAME. DENTED. FAULT ZONE 100, STR: 02 EA DENTS ON FR STA 1480 AND BTW STRG 22R TO 23R, AFT CARGO COMPARTMENT. ACCOMPLISHED REPAIR IAW 757-200PF SRM REV 120 CHAPTER 53-00-07-2
- [SDR IPXA2024091983273](https://openairdocs.org/sdr/IPXA2024091983273), Sep 13, 2024: FRAME. DENTED. FAULT ZONE 100, STR: 01 EA DENTS ON FR STA 1300 AND BTW STRG 23R TO 24R, AFT CARGO COMPARTMENT. ACCOMPLISHED REPAIR IAW 757-200PF SRM REV 120 CHAPTER 53-00-07-2
- [SDR IPXA2024092472968](https://openairdocs.org/sdr/IPXA2024092472968), Sep 13, 2024: SKIN. DAMAGED. R/H LOWER FUSELAGE STA 1500-1520 MARKED WITH #7 BETWEEN STRINGERS 26-25 HAS A NICK. DOT 75-021 HA-75. AFTER REMEASUREMENTS AT SKIN BETWEEN STA 1500-1520, BTW ST
- [SDR IPXA2024091972968](https://openairdocs.org/sdr/IPXA2024091972968), Sep 13, 2024: SKIN. NICKED. R/H LOWER FUSELAGE STA 1500-1520 MARKED WITH #7 BETWEEN STRINGERS 26-25 HAS A NICK. DOT 75-021 HA-75 INSPECTED RESTORED SURFACE PROTECTION.<BR>JOB COMPLETED. OP
- [SDR IPXA2024100744451](https://openairdocs.org/sdr/IPXA2024100744451), Sep 11, 2024: FLOORBEAM. CORRODED. MC FLOOR BEAM, AT STA 1200 LBL 12 FOUND CORROSION. ACCOMPLISH PERMANENT REPAIR PER EO-91419-REQ1 AND VT-MAE 757-5360-27-A3686, REV- REVIEWED
- [SDR IPXA2024091944456](https://openairdocs.org/sdr/IPXA2024091944456), Sep 11, 2024: SEAT TRACK. CORRODED. SEAT TRACK AT STA 1195<BR> BL0 FOUND CORROSION. INSTALLED SEAT TRACK AT STA 1195, BL0. IAW B757-200 SRM 51-40-02, MATERIAL USED P/N: BACB30NX8K6, BATCH: 0004304
- [SDR IPXA2024091944451](https://openairdocs.org/sdr/IPXA2024091944451), Sep 11, 2024: FLOORBEAM. CORRODED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT: STR. ZONE 200 MC FLOOR BEAM, AT STA 1200 LBL 12 FOUND CORROSION. REVIEWED
- [SDR IPXA2023020690666](https://openairdocs.org/sdr/IPXA2023020690666), Feb 1, 2023: FUEL. INOPERATIVE. INSPECTION TYPE:NA*A/C WAS OOS* FUEL MIGRATES FROM THE LEFT FUEL TANK TO THE CNTR FUEL TANK . FUEL WAS LOADED CORRECTLY ON THE GROUND IN ELP . LEFT 9.5 , CENTER
- [SDR IPXA2023112756536](https://openairdocs.org/sdr/IPXA2023112756536), Dec 1, 2022: SKIN. PUNCTURED. *MAJOR REPAIR* RIGHT SIDE AFT FUSELAGE SKIN PUNCTURE AT STA 1520, S-21R-REPAIR REF EO-85346***SM2/LMX6/QC2*** COMPLIED WITH EO-85346-REQ003. REPAIR UPGRADED TO 
- [SDR IPXA2022120288631](https://openairdocs.org/sdr/IPXA2022120288631), Dec 1, 2022: SKIN. DAMAGED. DAMAGE TO AIRCRAFT SKIN BEHIND AFT CARGO DOOR, MAJOR REPAIR, ALL WORK ACCOMPLISHED ON NRC 684236 & NRC 684237
- [SDR IPXA2022083085766](https://openairdocs.org/sdr/IPXA2022083085766), Aug 30, 2022: NONE. NONE. INSPECTION TYPE:C18NEEDED AN ALTERNATIVE METHOD OF INSPECTION ON AN EXISTING REPAIR TO FS 1560 BETWEEN STR 25R AND STR 27R AS PER EO#B757-5310-73926-AFOLLOWED E
- [SDR IPXA2022090185816](https://openairdocs.org/sdr/IPXA2022090185816), Aug 22, 2022: NONE. DENTED. INSPECTION TYPE:C18AFT PIT FRAME STA 1320 RH SIDE HAS TWO DENTS ON UPPER FLANGEREPAIRED FRAME PER EA# 757-5360-27-A3010
- [SDR IPXA2022082585594](https://openairdocs.org/sdr/IPXA2022082585594), Aug 19, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C18FLOOR PANEL #241 XDF HAS BROKEN EDGES IN 2 PLACES DOT 70-15FABBED PANEL 241 XDF FROM 5024N400001SS-G, BATCH# 3855547 PER SREO B757-5320-9692-
- [SDR IPXA2022070183674](https://openairdocs.org/sdr/IPXA2022070183674), Jul 1, 2022: TAILPIPE. DAMAGED. INSPECTION TYPE:NARIGHT ENGINE TAILPIPE FIRE.ACCOMPLISHED FIM 71-06-00-815-804-POO VISUAL INSP OF INLET AND TAIL PIPE NO DAMAGE NOTED. CHECK FOR EPCS FAULTS NON
- [SDR IPXA2020052655806](https://openairdocs.org/sdr/IPXA2020052655806), May 22, 2020: WARNING MESSAGE. FALSE ACTIVATION. EMERGENCY DECLARED, FLIGHT LANDED UNEVENTFUL, TRAILING EDGE FLAP DISAGREE OCCURED WHEN FLAP POSITION 1 WAS SELECTED ON ARRIVAL IN OAK FOLLWED QRH PROCEEDURE.PER
- [SDR IPXA2018092864441](https://openairdocs.org/sdr/IPXA2018092864441), Sep 20, 2018: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL 242EF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032327734](https://openairdocs.org/sdr/IPXA2018032327734), Mar 22, 2018: BULB. INOPERATIVE. EMERGENCY LIGHT HAS SIX INOPERATIVE BULBS. R & R THE LAMPS IAW AMM 33-51-01-02.
- [SDR IPXA2018021626571](https://openairdocs.org/sdr/IPXA2018021626571), Feb 15, 2018: BULB. INOPERATIVE. EMERGENCY LIGHT HAS FOUR BULBS INOPERATIVE. REPLACED THE BULBS IAW AMM 33-51-01-2.
- [SDR IPXA2016083107697](https://openairdocs.org/sdr/IPXA2016083107697), Aug 25, 2016: FLOORBOARD. DELAMINATED. INSPECTION TYPE:C-15, MAIN CABIN FLOORBOARD 251 XCF DELAMINATED. FABRICATED NEW FLOORBOARD 251 XCF IAW EO B757-5320-9692-H.
- [SDR IPXA2016083107696](https://openairdocs.org/sdr/IPXA2016083107696), Aug 25, 2016: FLOORBOARD. DELAMINATED. INSPECTION TYPE:C-15, MAIN CABIN NEW FLOORBOARD 251XFF DELAMINATED. FABRICATED MAIN CABIN FLOORBOARD 251XFF IAW EO B757-5320-9692-H.
- [SDR IPXA2016091908440](https://openairdocs.org/sdr/IPXA2016091908440), Aug 23, 2016: DOOR SILL. UNKNOWN. INSPECTION TYPE:C-15, MAIN CARGO DOOR LOWER SILL WEB AND INNER CHORD PN 65-40510-3 REQUIRES REPLACEMENT, REF EO B757-5310-61883-A. REPLACED AS REQUIRED IAW B757
- [SDR IPXA2016091008067](https://openairdocs.org/sdr/IPXA2016091008067), Aug 23, 2016: SEAT TRACK. CORRODED. INSPECTION TYPE: C-15, CAPTAIN`S FWD INBD SEAT TRACK HAS CORROSION ON BOTTOM. REPLACED THE SEAT TRACK.

All 204: https://openairdocs.org/aircraft/N419UP/reports.md

## STCs that may be installed (OpenAirDocs) (1)

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 RB211-535E4 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-535E4-37

## Related

- Other Boeing 757-24APF aircraft: https://openairdocs.org/model/boeing-757-24apf/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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