# Boeing 727-2K5 - Type: Aircraft model (FAA registry) - Registry code: 138004P - Manufacturer (registry): BOEING - Model: 727-2K5 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 3 · Turbo-jet - Seats: 162 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/boeing-727-2k5 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 (1) - [N909PG](https://openairdocs.org/aircraft/N909PG): [Argenjet Air Lease Inc](https://openairdocs.org/faa-owner/ARGENJET%20AIR%20LEASE%20INC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1979, S/N 21852, Non-citizen corporation, flight hours not reported ## NTSB investigations (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 FTW97IA119](https://openairdocs.org/ntsb/FTW97IA119), Mar 10, 1997: Boeing 727-2K5 (N909PG), Dfw Airport, TX, incident, minor damage. Probable cause: failure of the outer bearing for undetermined reason(s). ## FAA accident and incident reports (2) 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 20060218001539I](https://openairdocs.org/incident/20060218001539I), Feb 18, 2006: Boeing 7272K5 (N909PG), Kansas City, MO. (-23) On February 18, 2006 custom air transport (cat) flight 16 was enroute from dayton, Ohio to Kansas City, Missouri. Approximately 260 miles from Kansas… - [Incident 19970310007319I](https://openairdocs.org/incident/19970310007319I), Mar 10, 1997: Boeing 7272L5 (N909PG), Dallas-Ft Worth, TX, Minor damage. Narrative: on departure from Dallas/fort Worth international airport, aeromexpress flight 9501 lost the #3 main landing gear tire & wheel assy at approx 50'… ## Service difficulty reports (53, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR PCS2008F00001](https://openairdocs.org/sdr/PCS2008F00001), Aug 19, 2008: WARNING LIGHT. FALSE ACTIVATION. AMERIJET FLIGHT 8116 ON 8/19/08 TTPP-KMIA DIVERTED TO TJSJ. CREW LOG ITEM "AT FL340 BOTH CAPT AND FIRST OFFICER CARGO DOOR LIGHTS ILLUMINATED ALONG WITH FE CARG - [SDR 1018200701](https://openairdocs.org/sdr/1018200701), Oct 18, 2007: CONTROL UNIT. MALFUNCTIONED. AMERIJET FLIGHT 843 DURING TAXI LOWER CARGO FIRE RED LIGHT ILLUMINATED AND REMAINS ILLUMINATED. THE AIRCRAFT RETURNED TO BLOCKS, THE CHANNEL A LOWER CARGO SMOKE - [SDR 715200701](https://openairdocs.org/sdr/715200701), Jul 15, 2007: SMOKE DETECTOR. FALSE ACTIVATION. SMOKE DETECTOR WARNING LIGHT CAME ON DURING TAXI. - [SDR PCSA10520071](https://openairdocs.org/sdr/PCSA10520071), Jan 5, 2007: PUMP. FAILED. DURING CLIMB FELT VIBRATION, NR 1 ENGINE EPR AND FUEL FLOW DROPPED TO ZERO. NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. SHUTDOWN WAS LESS THAN 30 MINU - [SDR C7WA200600011](https://openairdocs.org/sdr/C7WA200600011), Apr 27, 2006: ROD. BROKEN. AFTER DEPARTURE, NOSE LANDING GEAR DOOR UNSAFE LIGHT ILLUMINATED. CYCLED LANDING GEAR 3 TIMES, NO HELP. NOTIFIED ATC AND ELECTED TO CONTINUE FLT AT REDUCED AIRS - [SDR C7WA200600002](https://openairdocs.org/sdr/C7WA200600002), Feb 18, 2006: TURBINE BLADES. FAILED. AT FLIGHT LEVEL 260 NR 3 ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS, ENGINE RPM DECREASED AND EGT WENT HIGH. SHUTDOWN ENGINE. INSPECTION OF NR 3 ENGINE REVEAL - [SDR C7WA200500111](https://openairdocs.org/sdr/C7WA200500111), Jul 22, 2005: LANDING GEAR. MALFUNCTIONED. AIR RETURN, UNABLE TO RETRACT MAIN LANDING GEAR. PERFORMED GEAR SWING AND MANUAL EXTENSION OF LANDING GEAR IAW MM. MAIN LANDING GEAR OPERATES NORMAL, NO DEFECTS - [SDR 99ZZZX4171](https://openairdocs.org/sdr/99ZZZX4171), Oct 6, 1999: FRAME. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON A/C BAY STA 740 DOOR FRAME, LEFT. - [SDR 99ZZZX3150](https://openairdocs.org/sdr/99ZZZX3150), Jul 12, 1999: TRIPLER. CORRODED. DURING A B-CHECK INSPECTION, LEVEL 2 CORROSION FOUND ON INNER SIDE OF FUSELAGE SKIN TRIPLER LOCATED AT THE FORWARD BOTTOM CORNER OF THE AFT LAVATORY SERVICE PAN - [SDR 99ZZZX3151](https://openairdocs.org/sdr/99ZZZX3151), Jul 11, 1999: MECHANISM. OUT OF ADJUST. KMEM/KMIA - FAE FLT 114 - AFTER TAKEOFF, UNABLE TO PRESSURIZE CABIN. PURSER ADVISED EXTREMELY LOUD NOISE FROM FORWARD ENTRY DOOR. RETURNED TO KMEM, UNEVENTFUL L - [SDR 98ZZZM864](https://openairdocs.org/sdr/98ZZZM864), Oct 23, 1998: HINGE COVER. DAMAGED. FLT 907 - KMIA-KMLU - ON FAE FLT, SHORTLY AFTER TAKEOFF, A NOISE WAS EXPERIENCED ON OR AROUND THE FORWARD ENTRY DOOR, DUE TO THE PROXIMITY OF THE AIRPORT THE CA - [SDR 98ZZZM865](https://openairdocs.org/sdr/98ZZZM865), Oct 17, 1998: DUCT. CRACKED. FLT 807 - KLAS-KMDT, ON FAE FLIGHT, AIRCRAFT UNABLE TO MAINTAIN PRESET PRESSURIZATION, AT 20,000 FLT ALT CABIN WAS 10,000 FT. FUEL WAS DUMPED AND AIRCRAFT RETUR - [SDR 98ZZZM861](https://openairdocs.org/sdr/98ZZZM861), Oct 16, 1998: SEAL. TORN. KLAS-KMDT - ON FAE FLIGHT NR 807, AIRCRAFT UNABLE TO PRESSURIZE, AT 20,000 FLT ALT CABIN WAS 10,000 FT. FUEL WAS DUMPED AND AIRCRAFT RETURNED TO KLAS. ON GROUND - [SDR 98ZZZX3539](https://openairdocs.org/sdr/98ZZZX3539), Aug 1, 1998: FITTING. LOOSE. MDPC/KMIA - ON FAE - FLT 800 - ON APPROACH, RIGHT MLG FAILED TO EXTEND. CREW ACCOMPLISHED MANUAL EXTENSION. ON GROUND, MAINTENANCE FOUND RIGHT MLG DOOR OUT OF R - [SDR 98ZZZX2330](https://openairdocs.org/sdr/98ZZZX2330), May 14, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S29R BETWEEN STA 950F AND STA 970. - [SDR 98ZZZX2318](https://openairdocs.org/sdr/98ZZZX2318), May 14, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FRAME 480 BETWEEN S23L AND S26L. - [SDR 98ZZZX2311](https://openairdocs.org/sdr/98ZZZX2311), May 14, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S27L AT STA 687. - [SDR 98ZZZX2310](https://openairdocs.org/sdr/98ZZZX2310), May 14, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S28L AT STA 674. - [SDR 98ZZZX2309](https://openairdocs.org/sdr/98ZZZX2309), May 14, 1998: SEAT TRACK. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON CABIN SEAT TRACK, STA 344 AT RBL 45.5. - [SDR 98ZZZX2297](https://openairdocs.org/sdr/98ZZZX2297), May 14, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S29R BETWEEN STA 970 - STA 990. - [SDR 98ZZZX2329](https://openairdocs.org/sdr/98ZZZX2329), May 13, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, FOUND FS 1148.0 FRAME CORRODED BETWEEN S26L TO S26R. - [SDR 98ZZZX2328](https://openairdocs.org/sdr/98ZZZX2328), May 13, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, FOUND FS 950.0 FRAME CORRODED FROM S26L TO S26R. - [SDR 98ZZZX2327](https://openairdocs.org/sdr/98ZZZX2327), May 13, 1998: SKIN. CORRODED. DURING C-CHECK INSPECTION, FOUND BELLY SKIN CORRODED FROM FS 680.0 TO FS 712.0 AT AND UNDER LEVELING COMPOUND APPLICATION AREAS. - [SDR 98ZZZX2296](https://openairdocs.org/sdr/98ZZZX2296), May 13, 1998: SUPPORT. CORRODED. DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORTS AT FS 1030.0 THROUGH FS 1166.0 CORRODED AT RBL 8.0. - [SDR 98ZZZX2295](https://openairdocs.org/sdr/98ZZZX2295), May 13, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, FOUND FS 1050.0 FRAME CORRODED BETWEEN STR 29RT TO STR 27RT. - [SDR 98ZZZX2294](https://openairdocs.org/sdr/98ZZZX2294), May 13, 1998: SUPPORT. CORRODED. DURING C-CHECK INSPECTION, FOUND FS 1030.0 TO FS 1116.0 FLOOR SUPPORTS CORRODED AT LBL 6.0. - [SDR 98ZZZX2332](https://openairdocs.org/sdr/98ZZZX2332), May 12, 1998: CHORD. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON THE UPPER RIGHT SIDE OF CHORD AT STA 1176.9. - [SDR 98ZZZX2331](https://openairdocs.org/sdr/98ZZZX2331), May 12, 1998: ANGLE. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON ANGLE AT STA 950E, S28R. - [SDR 98ZZZX2326](https://openairdocs.org/sdr/98ZZZX2326), May 12, 1998: BRACKET. CORRODED. DURING C-CHECK INSPECTION, FOUND ADF ANTENNA MOUNT BRACKET CORRODED, STA 720E. - [SDR 98ZZZX2325](https://openairdocs.org/sdr/98ZZZX2325), May 12, 1998: INTERCOSTAL. CORRODED. DURING C-CHECK INSPECTION, FOUND INTERCOSTAL CORRODED STA 1050 - STA 1074, STR 29L - STR 30. - [SDR 98ZZZX2324](https://openairdocs.org/sdr/98ZZZX2324), May 12, 1998: INTERCOSTAL. CORRODED. DURING C-CHECK INSPECTION, FOUND INTERCOSTAL AND BRACKET CORRODED STA 1050 - STA 1070, STR 27 - STR 28L. - [SDR 98ZZZX2323](https://openairdocs.org/sdr/98ZZZX2323), May 12, 1998: SUPPORT. CORRODED. DURING C-CHECK INSPECTION, FOUND FOUND L-2 DOOR SILL SUPPORT CORRODED. - [SDR 98ZZZX2322](https://openairdocs.org/sdr/98ZZZX2322), May 12, 1998: SILL. CORRODED. DURING C-CHECK INSPECTION, FOUND L-2 DOOR SILL CORRODED. - [SDR 98ZZZX2321](https://openairdocs.org/sdr/98ZZZX2321), May 12, 1998: SEAT TRACK. CORRODED. DURING C-CHECK INSPECTION, FOUND SEAT TRACK CORRODED. - [SDR 98ZZZX2320](https://openairdocs.org/sdr/98ZZZX2320), May 12, 1998: SILL SUPPORT. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON THE R-2 DOOR SILL AT STA 1070, WL 232.5. - [SDR 98ZZZX2319](https://openairdocs.org/sdr/98ZZZX2319), May 12, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON STRINGER 28R AT STA 1130. - [SDR 98ZZZX2317](https://openairdocs.org/sdr/98ZZZX2317), May 12, 1998: SEAT TRACK. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON CABIN SEAT TRACK STA 1110 AT RBL 45.5. - [SDR 98ZZZX2316](https://openairdocs.org/sdr/98ZZZX2316), May 12, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FRAME 720 BETWEEN S28R AND S28L. - [SDR 98ZZZX2315](https://openairdocs.org/sdr/98ZZZX2315), May 12, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FRAME 700 BETWEEN S28L AND S28R. - [SDR 98ZZZX2314](https://openairdocs.org/sdr/98ZZZX2314), May 12, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S27R AT STA 685. - [SDR 98ZZZX2313](https://openairdocs.org/sdr/98ZZZX2313), May 12, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S28R AT STA 685. - [SDR 98ZZZX2312](https://openairdocs.org/sdr/98ZZZX2312), May 12, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S28L AT STA 686. - [SDR 98ZZZX2308](https://openairdocs.org/sdr/98ZZZX2308), May 12, 1998: SKIN. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON SKIN AT LOWER H.F. ANTENNA MOUNT, STA 470. - [SDR 98ZZZX2307](https://openairdocs.org/sdr/98ZZZX2307), May 12, 1998: SKIN. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON LT WING UPPER SURFACE AT NR 4 SPOILER ATTACH POINT. - [SDR 98ZZZX2306](https://openairdocs.org/sdr/98ZZZX2306), May 12, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FRAME 1090 BETWEEN S27L AND S27R. - [SDR 98ZZZX2305](https://openairdocs.org/sdr/98ZZZX2305), May 12, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FRAME 1130 BETWEEN S26L AND S26R. - [SDR 98ZZZX2304](https://openairdocs.org/sdr/98ZZZX2304), May 12, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FRAME 1050 BETWEEN S28L AND S27L. - [SDR 98ZZZX2303](https://openairdocs.org/sdr/98ZZZX2303), May 12, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FRAME 1030 BETWEEN S74R AND S28R - [SDR 98ZZZX2302](https://openairdocs.org/sdr/98ZZZX2302), May 12, 1998: FRAME. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS ONTED ON FRAME 1010 AT S27L. - [SDR 98ZZZX2301](https://openairdocs.org/sdr/98ZZZX2301), May 12, 1998: STRINGER. CORRODED. DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S29R AND SKIN BETWEEN STA 950E AND STA 950F. All 53: https://openairdocs.org/model/boeing-727-2k5/reports.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.