# Boeing 727-2Q6 - Type: Aircraft model (FAA registry) - Registry code: 138407V - Manufacturer (registry): BOEING - Model: 727-2Q6 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 3 · Turbo-jet - Seats: 134 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-727-2q6 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 (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 CHI01IA248](https://openairdocs.org/ntsb/CHI01IA248), Jul 27, 2001: Boeing 727-2Q6 (N782AT), Oshkosh, WI, incident, no damage. Probable cause: The unsafe condition caused when the pilot taxied onto the runway. Factors relating to this accident were the pilot not following the instructions given him by the ground marshaller, his wrong taxi… ## 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 20010727020211I](https://openairdocs.org/incident/20010727020211I), Jul 27, 2001: Boeing 7272Q6 (N782AT), Oshkosh, WI. (-23) On July 27, 2001, at 1453 central daylight time, a Boeing 727-2Q6, N782AT, operated by an airline transport pilot as American tans air (ata), amtran… ## Service difficulty reports (31) As reported by operators and repair stations, by the model named in the report. - [SDR CA081016008](https://openairdocs.org/sdr/CA081016008), Oct 3, 2008: SWITCH. INOPERATIVE. (CAN) ON CLIMB OUT, NR 3 ENGINE THRUST REVERSER OPERATING LIGHT ILLUMINATED THROUGH 5000 FT. THE ACFT RETURNED TO THE AIRPORT. THE NR3 ENG THRUST REVERSER WAS D - [SDR C7WA200700001](https://openairdocs.org/sdr/C7WA200700001), Apr 29, 2007: CONTROLLER. SMOKE. ON CLIMBOUT FROM SJU FLIGHT ENGINEER SMELLED SMOKE AND TRIED TO ID SOURCE. ACCOMPLISHED AOM PROCEDURE AND REMOVED POWER FROM CARGO DOOR CONTROL. SMOKE STOPPED A - [SDR C7WA200600017](https://openairdocs.org/sdr/C7WA200600017), Nov 30, 2006: WIRE. BROKEN. AIR RETURN: AT LIFT OFF, HEARD A LOUD BANG AND AIRCRAFT WOULD NOT PRESSURIZE. NO DOOR LIGHTS OBSERVED. RETURNED TO DEPARTURE. SECURED E&E BAY DOOR. PRESSURIZED - [SDR C7WA200600005](https://openairdocs.org/sdr/C7WA200600005), Feb 24, 2006: ACTUATOR. INOPERATIVE. NR 3 LEADING EDGE FLAP WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LEADING EDGE FLAP ACTUATOR IAW MM, OPERATIONAL CHECKS GOOD. (K) - [SDR C7WA200400071](https://openairdocs.org/sdr/C7WA200400071), Dec 10, 2004: ACTUATOR. LEAKING. AIR RETURN; AFTER TAKEOFF AND FLAP RETRACTION SYSTEM (A) HYDRAULIC QUANTITY WAS DROPPING RAPIDLY. ACCOMPLISHED ABNORMAL PROCEDURE FOR LOSS OF SYSTEM (A) QUANTIT - [SDR C7WA200400009](https://openairdocs.org/sdr/C7WA200400009), Apr 12, 2004: STRAP. CRACKED. FOUND FORWARD ENTRANCE DOOR AFT LOWER STRAP CRACKED. REPAIRED STRAP IAW B727 SRM 51-40-4. (M) - [SDR C7WA200400010](https://openairdocs.org/sdr/C7WA200400010), Apr 12, 2004: DOOR FRAME. CRACKED. FOUND MAIN CARGO DOOR FORWARD UPPER FRAME CRACKED. REPAIRED FRAME IAW AERONAUTICAL ENGINEERS INC EO NR 1434. (M) - [SDR C7WA200400011](https://openairdocs.org/sdr/C7WA200400011), Apr 12, 2004: DOOR FRAME. CRACKED. FOUND MAIN CARGO DOOR FORWARD UPPER FRAME CRACKED. REPAIRED FRAME IAW AERONAUTICAL ENGINEERS INC EO NR 1434. (M) - [SDR C7WA200400013](https://openairdocs.org/sdr/C7WA200400013), Apr 12, 2004: FRAME. CRACKED. FOUND FUSELAGE FRAME CRACKED FS 680 WL 208. REPAIRED FUSELAGE FRAME IAW B727 MM 51-40-3. (M) - [SDR C7WA200400012](https://openairdocs.org/sdr/C7WA200400012), Apr 12, 2004: HINGE. CRACKED. FOUND MAIN CARGO DOOR FORWARD HINGE HAS A CRACKED LOBE. REPLACED FORWARD HING HALF IAW AERONAUTICAL ENGINEERS INC SERVICE BULLETIN AE101-01. (M) - [SDR COOSDR020174](https://openairdocs.org/sdr/COOSDR020174), Jul 1, 2002: SUPPORT FITTING. CORRODED. LEFT AND RIGHT WING, INBOARD FLAP, INBOARD TRACK FORWARD SUPPORT FITTING WITH BORE CORRODED. - [SDR COOSDR020173](https://openairdocs.org/sdr/COOSDR020173), Jul 1, 2002: FLAP TRACK. CORRODED. RIGHT WING, FLAP TRACK NR 6, AFT PAD CORRODED. - [SDR COOSDR020172](https://openairdocs.org/sdr/COOSDR020172), Jun 1, 2002: SKIN. DELAMINATED. LEFT WING OUTBOARD AILERON TAB UPPER, LOWER SKIN DELAMINATED AND HONEYCOMB CORE SECTION CORRODED. - [SDR COOSDR020171](https://openairdocs.org/sdr/COOSDR020171), Jun 1, 2002: SKIN. DELAMINATED. LEFT WING SPOILER NR 3 UPPER SKIN DELAMINATED AND HONEYCOMB CORE SECTION CORRODED. - [SDR COOSDR020170](https://openairdocs.org/sdr/COOSDR020170), Jun 1, 2002: SKIN. DELAMINATED. RIGHT WING SPOILER NR 14 UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED. - [SDR COOSDR020169](https://openairdocs.org/sdr/COOSDR020169), Jun 1, 2002: AILERON. DELAMINATED. LEFT WING OUTBOARD AILERON TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED. - [SDR COOSDR020168](https://openairdocs.org/sdr/COOSDR020168), Jun 1, 2002: PANEL. DELAMINATED. RIGHT WING TRAILING EDGE LOWER FIX PANEL OUTER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED. - [SDR COOSDR020167](https://openairdocs.org/sdr/COOSDR020167), Jun 1, 2002: AILERON. DELAMINATED. RIGHT WING OUTBOARD AILERON TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED. - [SDR COOSDR020166](https://openairdocs.org/sdr/COOSDR020166), Jun 1, 2002: SPOILER. DELAMINATED. LEFT WING SPOILER NR 6 UPPER AND LOWER SKIN, DELAMINATED AND HONEYCOMB CORE CORRODED. - [SDR COOSDR020165](https://openairdocs.org/sdr/COOSDR020165), Jun 1, 2002: SHEAR TIE. CORRODED. AFT CARGO COMP. BS 950A SHEAR TIE CORRODED BETWEEN STR 28R AND STR 29R. - [SDR COOSDR020164](https://openairdocs.org/sdr/COOSDR020164), Jun 1, 2002: SKIN. CRACKED. SECTION 46-RIGHT FUSELAGE SKIN CRACKED AND CORRODED BETWEEN BS 1164.5 AND BS 1179 BETWEEN STR 26R AND STR 25R. - [SDR COOSDR020163](https://openairdocs.org/sdr/COOSDR020163), Jun 1, 2002: RIB. CORRODED. RIB UPPER CHORD CORRODED, BETWEEN BS 836.95 AND BS 848.95, AT LEFT WING, BUTTOCK LINE 70.5. - [SDR COOSDR020162](https://openairdocs.org/sdr/COOSDR020162), Jun 1, 2002: RIB. CORRODED. RIB UPPER CHORD CORRODED, BETWEEN BS 836.95 AND BS 848.95 AT LEFT WING, BUTTOCK LINE 70.5. - [SDR COOSDR020161](https://openairdocs.org/sdr/COOSDR020161), Jun 1, 2002: SKIN. WORN. FUSELAGE SKIN - RIGHT SIDE BODY STATION 720D+11 INCHES, STRINGER 19R - SKIN WITH WEAR. - [SDR C8GA200000006](https://openairdocs.org/sdr/C8GA200000006), Jul 7, 2000: CONNECTOR. DIRTY. FLIGHT 205 FROM IND TO DFW. IN TAKE OFF CONFIGURATION, WHEN THROTTLES ADVANCED, THE TAKE OFF WARNING HORN SOUNDED. THE AIRCRAFT TAXIED FROM RUNWAY AND RETURNED - [SDR 20000619AP001](https://openairdocs.org/sdr/20000619AP001), Feb 9, 2000: HYDRAULIC LINE. LEAKING. INBOUND TO MDW A/C WAS DIVERTED TO ORD DUE TO THE NR 2 B SYSTEM PUMP LOW PRESSURE LIGHT CAME ON AND THE B SYSTEM QTY DROPPED. THE NR 1 B SYSTEM PUMP LOW PRESSUR - [SDR 99ZZZM633](https://openairdocs.org/sdr/99ZZZM633), Jul 15, 1999: CONNECTOR. DAMAGED. NR 1 ENGINE FIRE WARNING ANNUNCIATOR CAME ON AT 230. ACCOMPLISHED ENGINE FIRE SHUTDOWN PROCEDURE, FIRE HANDLE PULLED AND FIRED BOTH BOTTLES AND LIGHT REMAINED O - [SDR 99ZZZM779](https://openairdocs.org/sdr/99ZZZM779), Jul 12, 1999: TUBE. INOPERATIVE. DURING LEVEL CRUISE AT 310, THE NR 1 ENGINE FIRE WARNING ANNUNCIATOR CAME ON. ACCOMPLISHED ENGINE FIRE SHUTDOWN PROCEDURE, FIRE HANDLE PULLED, LIGHT IMMEDIATELY - [SDR 99ZZZX2831](https://openairdocs.org/sdr/99ZZZX2831), Jun 26, 1999: ENGINE. FAILED. KDAY/KJAX - FLT 326 - IN CRUISE, THE NR 2 ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED ON FORWARD CONTROL PANEL. A CORRESPONDING DROP IN OIL PRESSURE WAS NOTED. OI - [SDR 98ZZZX4544](https://openairdocs.org/sdr/98ZZZX4544), Jul 2, 1998: BATTERY. DISCHARGED. IND - RIGHT SIDE AFT OVERWING EXPRESS (ABOVE FLAP) LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. - [SDR C8GA973204](https://openairdocs.org/sdr/C8GA973204), Sep 18, 1997: RETRACT MECH. MALFUNCTIONED. KTPA/KATL - FLT 103/18 - LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. PERFORMED LANDING GEAR EXTENSION AND RETRACTION CHECK PER MM 32-31-0 WITH AIRCRAFT ON JACKS. --- 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.