# Boeing 757-23APF

- Type: Aircraft model (FAA registry)
- Registry code: 1384966
- Manufacturer (registry): BOEING
- Model: 757-23APF
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 178
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-757-23apf

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

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19990212012979I](https://openairdocs.org/incident/19990212012979I), Feb 12, 1999: Boeing 75723APF (N571CA), Quito, EU, Minor damage. Aircraft started its take off roll. At approx. 60 KTS. Left engine started to compressor stall. Aircraft started to yaw left of runway. Aborted t/o at 75KTS.…

## Service difficulty reports (96, newest 50)

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

- [SDR 22AA200900023](https://openairdocs.org/sdr/22AA200900023), Aug 25, 2009: ACTUATOR. INOPERATIVE. UNABLE TO RAISE LANDING GEAR. REMOVED AND REPLACED 2 EA BRACKETS AT LT M/G ALSO HYD LINE AND MAIN GEAR TRUCK POSITION ACTUATOR IAW MM 32-32-15. JACKING ACFT IAW
- [SDR 22AA200900007](https://openairdocs.org/sdr/22AA200900007), Aug 21, 2009: UNKNOWN. ODOR. ODOR OF ELECTRICAL FUMES FROM UNKNOWN SOURCE. UNABLE TO ISOLATE. VISUAL INSPECTED WIRE BUNDLES & TERMINALS, BLOCK IN FWD E/E. NO FUMES BURNED OR CHAFING NOTED. 
- [SDR 22AA200900008](https://openairdocs.org/sdr/22AA200900008), Jul 27, 2009: CONNECTOR. BURNED. DURING DESCENT, HAD MOMENTARILY ELEC ODOR LASTING NO LONGER THAN 30 SECONDS. NO SMOKE OBSERVED. REMOVED AND REPLACED TERMINAL CONNECTORS D3324 AND D3326 FROM WI
- [SDR 22AA200900006](https://openairdocs.org/sdr/22AA200900006), Jul 21, 2009: UNKNOWN. ODOR. FUMES FROM UNIDENTIFIABLE SOURCE ON FLIGHT. MADE EMERGENCY LANDING. INSPECTED AIR RECIRCULATION FAN IAW MM 21-05-01, FAULTS FOUND. INSPECTED E/E/ EQUIPMENT COOL
- [SDR DU4R2009319](https://openairdocs.org/sdr/DU4R2009319), Mar 12, 2009: ATTACH ANGLE. CORRODED. DURING SCHEDULED INSPECTION, FOUND MAJOR EXFOLIATED CORROSION ON ATTACH ANGLES ( 4 EA.) ATTACHED TO STRINGERS FOR APU INLET DOORS PLENUM ASSY MOUNTED ABOVE (THS
- [SDR DU4R2009310](https://openairdocs.org/sdr/DU4R2009310), Mar 5, 2009: ANGLE. CORRODED. S/O 381002 N/R 36347 DURING SCHEDULED INSPECTION, FOUND NR 10 SLAT I/B END HAS CORROSION ON L-ANGLE.
- [SDR DU4R2009308](https://openairdocs.org/sdr/DU4R2009308), Mar 2, 2009: WEB. CORRODED. S/O 318002 N/R 35473 DURING SCHEDULED INSPECTION, FOUND NR 2 PYLON LT AFT SIDE WEB HAS NUMEROUS AREAS OF CORROSION ON INNER AND OUTER SURFACES INCLUDING AROUND 
- [SDR DU4R2009299](https://openairdocs.org/sdr/DU4R2009299), Feb 13, 2009: SKIN PANEL. CORRODED. S/O 318002 N/R 34983 - DURING SCHEDULED INSPECTION, FOUND CORROSION ON NR 1 PYLON FWD O/B SKIN PSS 68 - 80.
- [SDR DU4R2009298](https://openairdocs.org/sdr/DU4R2009298), Feb 13, 2009: SKIN PANEL. CORRODED. S/O 318002 N/R 34848 - DURING SCHEDULED INSPECTION, FOUND CORROSION IN NR 2 ENGINE PYLON INBOARD SKIN PANEL BELOW FWD AND AFT OF MOST FWD ACCESS PANEL.
- [SDR DU4R2009297](https://openairdocs.org/sdr/DU4R2009297), Feb 11, 2009: SKIN PANEL. CORRODED. S/O 318002 N/R 34856 DURING SCHEDULED INSPECTION, FOUND CORROSION IN OUTBOARD PYLON SKIN PANEL FWD OF MOST FWD ACCESS PANEL NR 2 ENGINE.
- [SDR DU4R2009296](https://openairdocs.org/sdr/DU4R2009296), Feb 11, 2009: SKIN PANEL. CORRODED. S/O 318002 N/R 34856 DURING SCHEDULED INSPECTION, FOUND CORROSION IN OUTBOARD PYLON SKIN PANEL FWD OF MOST FWD ACCESS PANEL NR 2 ENGINE.
- [SDR DU4R2009309](https://openairdocs.org/sdr/DU4R2009309), Feb 10, 2009: SUPPORT BEAM. CORRODED. S/O 381002 N/R 36157 DURING SCHEDULED INSPECTION, FOUND LT WING REAR SPAR TO MLG SUPPORT BEAM HAS CORROSION AROUND AFT ATTACH BOLT HOLE.
- [SDR DU4R2009301](https://openairdocs.org/sdr/DU4R2009301), Feb 10, 2009: SKIN. CORRODED. DURING SCHEDULED INSP, FOUND CORROSION ON SKIN UPON REMOVAL OF TEMP REPAIR PLATE P/N 112N4303-2 AT RBBL 70.50, BS 958.39.
- [SDR DU4R2009326](https://openairdocs.org/sdr/DU4R2009326), Feb 4, 2009: SKIN. CORRODED. S/O NR 318002 NR 35425, DURING SCHEDULED INSP AT, FOUND NR 1 PYLON RT AFT SIDE WEB HAS NUMEROUS AREAS OF CORROSION ON INNER AND OUTER SURFACES INCLUDING FASTENE
- [SDR DU4R2009291](https://openairdocs.org/sdr/DU4R2009291), Jan 20, 2009: STIFFENER. CORRODED. DURING SCHEDULED INSPECTION FOUND VERTICAL STIFFENER ATTACHED TO THE REAR SPAR WEB HAS PITTING CORROSION AT ATTACH POINT OF A GROUNDING WIRE APPROX WS 184.
- [SDR DU4R2009290](https://openairdocs.org/sdr/DU4R2009290), Jan 13, 2009: BULKHEAD. CRACKED. DURING SCHEDULED INSPECTION, FOUND NR 2 PYLON MID BULKHEAD FWD I/B LOWER BOLT HOLE IS CRACKED.
- [SDR DU4R2009288](https://openairdocs.org/sdr/DU4R2009288), Jan 13, 2009: BULKHEAD. CRACKED. DURING SCHEDULED INSPECTION, FOUND NR 1 PYLON MID BULKHEAD FWD I/B LOWER BOLT HOLE IS CRACKED.
- [SDR DU4R2009327](https://openairdocs.org/sdr/DU4R2009327), Jan 9, 2009: KEELBEAM. CORRODED. S/O NR 318002 NR35531, DURING SCHEDULED INSP, FOUND CORROSION ON SPLICE PLATE ON FUSELAGE AT AFT END OF MLG DOORS BETWEEN BOTH DOORS ON BELLY.
- [SDR DU4R2009289](https://openairdocs.org/sdr/DU4R2009289), Jan 8, 2009: BULKHEAD. CRACKED. DURING SCHEDULED INSPECTION AT TIMCO, LAKE CITY, FL FOUND NR 1 PYLON MID BULKHEAD FWD O/B LOWER BOLT HOLE IS CRACKED.
- [SDR DU4R2009287](https://openairdocs.org/sdr/DU4R2009287), Jan 8, 2009: KEELBEAM. CORRODED. S/O 318002 N/R 35725 DURING SCHEDULED INSPECTION, FOUND CORROSION ON LOWER KEEL BEAM CHORD IN RT WW AT BS 1060.
- [SDR DU4R2009286](https://openairdocs.org/sdr/DU4R2009286), Jan 8, 2009: WEB. CORRODED. S/O 318002 N/R 35013 DURING SCHEDULED INSPECTION, FOUND CORROSION ON KEEL BEAM VERTICAL WEB AROUND HYD LINE FITTINGS AT FS 1100 S-19R RBL 5
- [SDR DU4R2008285](https://openairdocs.org/sdr/DU4R2008285), Dec 28, 2008: SKIN. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION IN SEVERAL AREAS OF UPPER SURFACE SKINS ON LT HORIZONTAL STABILIZER.
- [SDR DU4R2008284](https://openairdocs.org/sdr/DU4R2008284), Dec 17, 2008: SPAR. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON WEB, LT WING REAR SPAR, ABOVE LT AFT BOOST PUMP WS 188
- [SDR DU4R2008282](https://openairdocs.org/sdr/DU4R2008282), Dec 17, 2008: SUPPORT. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON WING TO BODY FAIRING SUPPORT ABOVE RT WING AT BS 1098.
- [SDR DU4R2008280](https://openairdocs.org/sdr/DU4R2008280), Dec 17, 2008: KEELBEAM. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON KEELBEAM LOWER SURFACE CROSS BRACE AT BS 996.
- [SDR DU4R2008279](https://openairdocs.org/sdr/DU4R2008279), Dec 17, 2008: SPAR. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON LT WING REAR SPAR BELOW LEFT AFT BOOST PUMP RSS 185.
- [SDR DU4R2008281](https://openairdocs.org/sdr/DU4R2008281), Dec 16, 2008: SKIN. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON EXT SKIN AROUND APU OIL FUEL DRAIN MAST RT APD ACCESS DOOR.
- [SDR DU4R2008278](https://openairdocs.org/sdr/DU4R2008278), Dec 16, 2008: SKIN. DAMAGED. DURING SCHEDULED INSPECTION, FOUND NUMEROUS CREASES IN EXT. FUSELAGE SKIN BS 1364 - 1410, S-26L TO S-26R
- [SDR DU4R2008277](https://openairdocs.org/sdr/DU4R2008277), Dec 16, 2008: SKIN. DENTED. DURING SCHEDULED INSPECTION, FOUND DENT IN EXT. FUSELAGE SKIN BS 1125, S-10L LAP SEAM.
- [SDR DU4R2008276](https://openairdocs.org/sdr/DU4R2008276), Dec 16, 2008: SKIN. DENTED. DURING SCHEDULED INSPECTION, FOUND 3 EA. DENTS IN LOWER FWD FUSELAGE BELOW MLG DOOR SCUFF PLATE BS 600-612.
- [SDR DU4R2008275](https://openairdocs.org/sdr/DU4R2008275), Dec 16, 2008: SKIN. CORRODED. DURING SCHEDULED INSPECTION, FOUND LT WING HAD CORROSION IN UPPER SKIN AT ALL VORTEX GENERATORS
- [SDR DU4R2008274](https://openairdocs.org/sdr/DU4R2008274), Dec 13, 2008: KEELBEAM. CORRODED. DURING SCHEDULED INSPECTION, FOUND KEELBEAM LOWER SURFACE CROSS BRACE HAS CORROSION AT BS 1040. 
- [SDR DU4R2008273](https://openairdocs.org/sdr/DU4R2008273), Dec 13, 2008: KEELBEAM. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND KEEL BEAM LOWER SURFACE CORSS BRACE HAS CORROSION AT BS 956 S/O 318002 N/R #35360
- [SDR DU4R2008272](https://openairdocs.org/sdr/DU4R2008272), Dec 12, 2008: SKIN. DENTED. DURING SCHEDULED INSPECTION, FOUND DENT IN FWD LOWER FUSELAGE BELOW MAIN CARGO DOOR THRESHOLD SCUFF PLATE AT BS 522. 
- [SDR DU4R2008283](https://openairdocs.org/sdr/DU4R2008283), Dec 10, 2008: STRAP. CORRODED. DURING SCHEDULED INSPECTION, FOUND HEAVY CORROSION ON 2 EA. SUPPORT STRAPS REMOVED FROM BS 1825, B/O 0, RT SIDE TO HORIZ STAB.
- [SDR DU4R2008271](https://openairdocs.org/sdr/DU4R2008271), Dec 7, 2008: KEELBEAM. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND KEEL BEAM AREA PANEL SUPPORT FRAME HAS CORROSION ON BOTH SIDES TOP AND BOTTOM SURFACES.
- [SDR DU4R2008270](https://openairdocs.org/sdr/DU4R2008270), Dec 7, 2008: SUPPORT. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND LT WHEEL WELL (MLG) WTB FAIRING SUPPORT ARE CORRODED THROUGHOUT AT BS 1040 - 1060 LBL 40 - 651.
- [SDR DU4R2008269](https://openairdocs.org/sdr/DU4R2008269), Dec 7, 2008: SKIN. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION ON LT WING AFT SPAR UPPER CHANNEL, SKIN FROM FUSELAGE TO WING TIP.
- [SDR DU4R2008268](https://openairdocs.org/sdr/DU4R2008268), Dec 7, 2008: PRESSURE PANEL. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION IN RT WHEEL WELL ON LOWER SURFACE OF CEILING AREA AT BS 1120 S-17R ALONG FASTENERS RBL 6
- [SDR DU4R2008267](https://openairdocs.org/sdr/DU4R2008267), Dec 7, 2008: FITTING. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORRODED ANGLE FITTING ON RT ELEVATOR STRAKELET.
- [SDR DU4R2008266](https://openairdocs.org/sdr/DU4R2008266), Dec 7, 2008: SKIN. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION ON LT WING AT NUMEROUS FASTENERS IN UPPER SKIN IN PREVIOUSLY WORKED SKIN AND UNWORKED SK
- [SDR DU42008F00000](https://openairdocs.org/sdr/DU42008F00000), Nov 18, 2008: SKIN. CRACKED. DURING SCHEDULED INSPECTION, FOUND 1/8" LONG CRACK RUNNING FWD AND AFT FROM FASTENER HOLE ON REPAIR FILLER AT BS 1739-5 S-29R. EXISTING EO REPAIR FAT EO 757-53-
- [SDR UPS06546376](https://openairdocs.org/sdr/UPS06546376), Mar 3, 2006: WARNING LIGHT. ILLUMINATED. ON T/O FROM MIA, NOSE GEAR "GREEN" DOWN AND LOCK LIGHT REMAINED ILLUMINATED W/GEAR UP AND LOCKED. RECYCLED LANDING GEAR, NO HELP. RIGHT HALF OF NOSE GEAR GREEN 
- [SDR 2000ZZZX215](https://openairdocs.org/sdr/2000ZZZX215), Oct 1, 1999: LINE. RUPTURED. KMIA/KSAL - FLT 067 AT 21:30 Z - LEFT HYDRAULIC QUANTITY INDICATOR DECREASED TO 0.03 GALLON. ENGINE DRIVEN PUMP DEPRESSURIZED AND ELECTRIC PUMP OFF, QUANTITY IN
- [SDR 99ZZZM701](https://openairdocs.org/sdr/99ZZZM701), Sep 4, 1999: ACTUATOR. FAILED. KMIA - LEFT MLG DID NOT RETRACT AFTER NORMAL TAKEOFF. GEAR DISAGREE/GEAR DOOR LIGH TON, STATUS AIR/GROUND DISAGREE ON LANDING GEAR MONITOR. FOUND LEFT MAIN LAND
- [SDR 99ZZZM702](https://openairdocs.org/sdr/99ZZZM702), Aug 31, 1999: ACTUATOR. FAILED. KMIA - LEFT MLG WOULD NOT RETRACT, GEAR DISAGREE/GEAR DOOR LIGHT ON WHEN GEAR HANDLE PLACED DOWN. FOUND LEFT MLG TILT ACTUATOR WITH INTERNAL LEAKAGE. REPLACED L
- [SDR 99ZZZM703](https://openairdocs.org/sdr/99ZZZM703), Aug 27, 1999: RETRACT MECH. LACK OF LUBE. KMIA - LEFT MLG WOULD NOT RETRACT, GEAR DISAGREE/GEAR DOOR LIGHT ON WHEN GEAR HANDLE PLACED DOWN. JACKED AND SWUNG GEAR SEVERAL TIMES WITH NO DISCREPANCY NOTED.
- [SDR 99ZZZM700](https://openairdocs.org/sdr/99ZZZM700), Aug 25, 1999: HOSE. LOOSE. FLT KMIA-SJO - REJECTED TAKEOFF DUE TO AIRSPEED DIFFERENCE, CAPTAIN 80 KNOTS, F/O 120 KNOTS, ABORTED AT 120 KNOTS. FOUND CAPTAIN PITOT SYSTEM LEAKING AT ELBOW F
- [SDR CLCA9903](https://openairdocs.org/sdr/CLCA9903), Mar 19, 1999: CIRCUIT BREAKER. TRIPPED. FLT 33 - MIA-SAP - AIR TURN BACK, CLIMBOUT OF FL240 THE FOLLOWING OCCURED. THE LEFT IRS DISPLAYED ON DC AND EICAS MESSAGE. THE CTR AUTOPILOT DISENGAGED AND AUTO
- [SDR CLCA9901](https://openairdocs.org/sdr/CLCA9901), Jan 11, 1999: FILLER. FAILED. FLT 96 - SEQU TO CLO - ON T/OF ROLL AT 0010Z. ON ROUTINE NORMAL T/O AT APPROX 75 KNOTS A/C BEGAN TO MAKE VIOLENT BANGING NOISE AND ABNORM EXTREME SHUDDERING FOL

All 96: https://openairdocs.org/model/boeing-757-23apf/reports.md

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