# Boeing 727-24C - Type: Aircraft model (FAA registry) - Registry code: 1384005 - Manufacturer (registry): BOEING - Model: 727-24C - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 3 ยท Turbo-jet - Seats: 134 - Weight class: 20,000 lb and over - Cruise speed: 435 mph - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-727-24c 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 (4) 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 19881105063609I](https://openairdocs.org/incident/19881105063609I), Nov 5, 1988: Boeing 72724C (N2475), Johnston Island, HI. Pilot not informed to overfly jon afb. Runway lights off on arrival. Made few low approaches before lights turned on - [Incident 19870420042759I](https://openairdocs.org/incident/19870420042759I), Apr 20, 1987: Boeing 72724C (N2475), Majuro, Northern Mariana Islands. Engine shutdown after a loud bang, high EGT reading. Returned. Tar ingested into engine. Runway under repair. - [Incident 19801221087879I](https://openairdocs.org/incident/19801221087879I), Dec 21, 1980: Boeing 72724C (N2475), Agana, Guam. Engine shutdown due to low oil pressure. Replaced pressure transmitter. - [Incident 19780202005539I](https://openairdocs.org/incident/19780202005539I), Feb 2, 1978: Boeing 727 (N2475), Agana, Guam. Pilot shut an engine down due to high oil temperature. Completed the trip. Found a broken wire to temp bulb. ## Service difficulty reports (17) As reported by operators and repair stations, by the model named in the report. - [SDR 02FDEA00944](https://openairdocs.org/sdr/02FDEA00944), Dec 13, 2002: DOWNLOCK SWITCH. INOPERATIVE. DURING LANDING GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. NO DOWN, GREEN LIGHT. NOTE: MANUAL GEAR EXTENSION PROCEDURE COMPLETED EMERGENCY, DECLARED WIT - [SDR 01FDEA00125](https://openairdocs.org/sdr/01FDEA00125), Feb 15, 2001: RELIEF VALVE. FAILED. WHILE IN FLT NR 2 ENG OIL PRESSURE ABOVE RED LINE (60 PSI) COMPLIED WITH RED TABS TO SHUT DOWN ENG. NOTE: ABOVE RED LINE FOR LESS THAN 5 MIN WHILE ADDRESSING PR - [SDR 00FDEA00012](https://openairdocs.org/sdr/00FDEA00012), Jan 13, 2000: GEARBOX. LEAKING. 00-12 - 15 MIN IN CR FLT NR 2 ENG RAPIDLY LOST OIL QUANTITY WITH ENSUING OIL PRESS LOSS. RED TABS COMPLIED WITH AND NR 2 ENG SHUTDOWN, EMERGENCY DECLARED WITH A - [SDR 98FDEA00209](https://openairdocs.org/sdr/98FDEA00209), Mar 20, 1998: DUCT. FAILED. DURING CLIMBOUT, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUM. BOTH NR 3 BLEED AND RIGHT PACK WERE ON AT THE TIME. AFTER RED TABS CALLED FOR CLOSING/OFF ON BOTH N - [SDR 98FDEA00208](https://openairdocs.org/sdr/98FDEA00208), Mar 19, 1998: GASKET. LEAKING. 98-0074, DURING CLIMB-OUT, THE NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. ENG NR 3 BLEED AIR SWITCH WAS CLOSED AT THE TIME THE LIGHT ILLUM. APPROPRIATE RED TABS WERE - [SDR 97FDEA00886](https://openairdocs.org/sdr/97FDEA00886), Dec 12, 1997: ACTUATOR. MALFUNCTIONED. UPON GEAR EXTENSION RIGHT GEAR DOOR AND RED DOORS LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND ALL WAS NORMAL. OPERATIONAL CKS OK PER ADJUSTMENT TEST PER MAINT - [SDR 97FDEA00869](https://openairdocs.org/sdr/97FDEA00869), Nov 26, 1997: SWITCH. FAILED. DURING GEAR RETRACTION, EXPERIENCED A RIGHT MAIN GEAR DOOR ANNUNCIATOR LIGHT. COMPLETED THE GEAR UNSAFE AND OR DOORS LIGHT GEAR HANDLE UP CHECKLIST. AFTER CYCLI - [SDR 97FDEA00809](https://openairdocs.org/sdr/97FDEA00809), Nov 7, 1997: SWITCHES. MOISTURE CONTAM. RIGHT MAIN GEAR DOOR LIGHT ON SECOND OFFICER'S ANNUNCIATOR PANEL AND RED GEAR DOOR LIGHT ON GEAR POSITION PANEL REMAINED ILLUMINATED AFTER EXTENSION. GEAR INDIC - [SDR 97FDEA00529](https://openairdocs.org/sdr/97FDEA00529), Aug 12, 1997: FRAME. CORRODED. NR 0380 - WHILE WORKING CARD NR 0142, FOUND CORROSION ON STA 1130 FRAME, LBL 25, WL 150 AT FASTENER HOLES. ACCOMPLISHED REPAIR TO BS 1130 FRAME AT LBL 25 PER FE - [SDR 97FDEA00528](https://openairdocs.org/sdr/97FDEA00528), Aug 12, 1997: KEEL BEAM. CRACKED. NR 0054 IN THE AFT CARGO BAY, FOUND CRACK IN STR 29L KEEL BEAM AT BS 1082 AND CORROSION AT BS 1055. REMOVED AND REPLACED STRINGER 29L KEEL BEAM IAW FED-EX SRM 5 - [SDR 97FDEA00525](https://openairdocs.org/sdr/97FDEA00525), Aug 11, 1997: FLAP. CORRODED. LT WING I/B MIDFLAP T/E WEDGE UPPER IS CORRODED APPROX 18 INCHES AND 64 INCHES FROM O/B END. *S/D* REMOVED AND REPLACED WITH SERVICEABLE LT WING I/B MIDFLAP IAW - [SDR 97FDEA00541](https://openairdocs.org/sdr/97FDEA00541), Aug 7, 1997: FLOORBEAM. CORRODED. NR 0107 001 STA-PAE - CORROSION ON BS 328 FLOORBEAM UPPER FLANGE LBL 47, WL 208. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 53-10-1, 5 - [SDR 97FDEA00507](https://openairdocs.org/sdr/97FDEA00507), Aug 7, 1997: FLOORBEAM. CORRODED. NR 0107 001 STA-PAE - CORROSION ON BS 328 FLOORBEAM UPPER FLANGE, LBL 47, WL 208. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 53-10-1, - [SDR 97FDEA00477](https://openairdocs.org/sdr/97FDEA00477), Jul 29, 1997: INDICATION. MALFUNCTIONED. 97-0141 NOSE GEAR DID NOT INDICATE A GREEN DOWN SAFE LIGHT ON FIRST TRY. CYCLED GEAR AND GOT SAFE INDICATION. - [SDR 97FDEA00463](https://openairdocs.org/sdr/97FDEA00463), Jul 22, 1997: RETRACT MECH. LACK OF LUBE. NOSE GEAR DIDN'T COME DOWN UNTIL RECYCLED HANDLE. LUBRICATED NOSE LANDING GEAR DRAG BRACE KNUCKLE ASSEMBLY. ALSO, REPLACED AERODYNAMIC SEAL AT FORWARD EDGE OF N - [SDR 96FDEA01603](https://openairdocs.org/sdr/96FDEA01603), Oct 22, 1996: SUPPLY DUCT. BLOWN. FIRE LIGHT AND BELL NR 3 ENGINE AFTER TAKEOFF AT 600 FEET ABOVE GROUND LEVEL. AFTER THROTTLE BROUGHT TO IDLE FIRE LIGHT WENT OUT. BOTH FIRE LOOPS TEST GOOD. LAN - [SDR 95FDEA00165](https://openairdocs.org/sdr/95FDEA00165), Feb 18, 1995: SEAL. CRACKED. FWD ENTRY DIFFICULT TO CLOSE AND OPEN. UPON CLOSER INSP FOUND A CRACKED SEAL AROUND UPR ROLLER ASSY AT REAR. UNABLE TO CLOSE DOOR COMPLETELY. (UPR AND LWR AFT R --- 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.