# N292AS: 1978 Boeing 727-212, registration cancelled 2009-01-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 20, 2009 - Exported to: Nigeria - Status when cancelled: Valid registration - Airframe: [Boeing 727-212](https://openairdocs.org/model/boeing-727-212) (registry code 138407G) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 21458 - Year built: 1978 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 17, 1998 - Certificate issued: June 25, 2008 - Last registry action: June 25, 2008 - Mode S code: A2FCF9 - Owner when cancelled: [Csds Aircraft Sales & Leasing Inc](https://openairdocs.org/faa-owner/CSDS%20AIRCRAFT%20SALES%20%26%20LEASING%20INC) - Location: [Torrance, CA](https://openairdocs.org/faa-place/CA/Torrance) - Owner type: Corporation - Owner's area on the map: 33.8673° N, 118.3316° W: Placed by OpenAirDocs at the center of ZIP code 90504, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N292AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=292AS - Page: https://openairdocs.org/deregistered/N292AS-2009-01-20 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 727-212: https://openairdocs.org/model/boeing-727-212.md ## Service difficulty reports (80, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR C1HA200892001](https://openairdocs.org/sdr/C1HA200892001), Jan 15, 2008: SKIN. CRACKED. FOUND CRACKED SKIN AND CORRODED STRINGER AT STA 1089 AT STR 28L. TRIMMED OUT DAMAGED TOP SKIN AND FABRICATED DOUBLER FROM 2024-T3 .060" AND INSTALLED PER SRM 53 - [SDR C1HA200792002](https://openairdocs.org/sdr/C1HA200792002), Aug 24, 2007: CONNECTOR. BROKEN. AFTER GEAR RETRACTION RED GEAR LIGHT FOR NOSE GEAR REMAINED ILLUMINATED REFORMED COM 2.32.22 LIGHT REMAINED ON. REPLACED BOTH NOSE GEAR DOWN LOCK AND GEAR POSIT - [SDR C1HA200792001](https://openairdocs.org/sdr/C1HA200792001), Apr 21, 2007: SWITCH. DEFECTIVE. AT FL 250 CABIN PRESS STARTED CLIMBING AT 100FT PER MIN PERFORMED COM 2.21.16 UNABLE TO STOP CLIMB. STARTED DESCENT, CABIN WOULD NOT HOLD PRESSURE UNTIL PASSING - [SDR C1HA200793001](https://openairdocs.org/sdr/C1HA200793001), Jan 29, 2007: SHEAR TIE. CORRODED. FOUND CORROSION AT SHEAR TIE AT BS 380 I/B OF STR 28L. REMOVED CORROSION FOUND OUT OF LIMITS FAB DOUBLER REPAIR AND INSTALLED IAW B727 SRM 53-10-4 FIG 13. - [SDR C1HA200692004](https://openairdocs.org/sdr/C1HA200692004), Aug 3, 2006: DUCT. LEAKING. AFTER ROTATION ENG 1 BLEED AIR TRIP OFF LIGHT ILLUMINATED. CREW PERFORMED COM 2.36.2 APPROX 1 OR 2 MINS AFTER COMPLETION OF COM PROCEDURE FOR ITEM 1, NR 1 ENG S - [SDR C1HA200692003](https://openairdocs.org/sdr/C1HA200692003), Mar 13, 2006: WARNING LIGHT. ILLUMINATED. DURING CLIMBOUT AT 12-13,000 FT THE NR 3 OIL FILTER BYPASS LIGHT ILLUMINATED. PERFORMED COM 2-72-19 ; 2-72-12 ; 2-28-4. RETURNED TO MMMZ. ALL ENGINE PARAMETERS - [SDR C1HA200692002](https://openairdocs.org/sdr/C1HA200692002), Mar 11, 2006: ACTUATOR. DIRTY. AFTER TAKEOFF TAIL SKID LIGHT REMIND ILLUMINATED FOLLOWED COM PROCEDURES DUMPED 26.2 FUEL RETURNED FOR LANDING IN ZIH. CLEANED ROLLER ACTUATOR ON BOTH SWITCHES. - [SDR C1HA200692001](https://openairdocs.org/sdr/C1HA200692001), Jan 19, 2006: ENGINE. FAILED. ON INITIAL CLIMB OUT, AFTER FLAPS UP AND SETTING CLIMB POWER NR 3 ENGINE (BANGED) AND ENGINE GAUGES FLUCTUATED AND AIRCRAFT YAWED. NO FIRE WARNING, NO BOOST PUM - [SDR C1HA200592004](https://openairdocs.org/sdr/C1HA200592004), Sep 19, 2005: TRUNNION. CORRODED. NOSE LANDING GEAR TRUNNION CAPS CORRODED, LEFT AND RIGHT. REMOVED CORROSION ON LT TRUNNION FITTING TO A FINAL BORE DIAMETER OF 2.602" AND RT 2.727" AND WITHIN L - [SDR C1HA200592003](https://openairdocs.org/sdr/C1HA200592003), Aug 8, 2005: PUMP. FAILED. NR 2 B PUMP FAILED INFLIGHT, REPLACED NR 2 B HYD PUMP, CASE DRAIN AND PRESSURE FILTER, OP'S CHECK GOOD. LEAK CK GOOD REF MM 29-12-3. - [SDR C1HA200592002](https://openairdocs.org/sdr/C1HA200592002), Jun 24, 2005: ACTUATOR. FAILED. ON DEPARTURE THE NR 6 L/E FAILED TO RETRACT, COMPLIED WITH COM PROCEDURE 2.27.12 SLAT WAS STILL EXTENDED. CONFERRED WITH DISPATCH/MDC, DECLARED AN EMERGENCY. CO - [SDR C1HA200492015](https://openairdocs.org/sdr/C1HA200492015), Jul 15, 2004: LIGHT. MALFUNCTIONED. UPON POWER TRANSFER FROM APU TO GENERATORS EMERGENCY LIGHTS ILLUMINATED WHILE IN THE ARMED POSITION. GATE RETURN INITIATED. SWITCHED TO GROUND POWER, RESET EMER - [SDR C1HA200492014](https://openairdocs.org/sdr/C1HA200492014), May 22, 2004: BEAM. CRACKED. FS 1183 LBL 36 CRACK IN VERTICAL BEAM. - [SDR C1HA200492013](https://openairdocs.org/sdr/C1HA200492013), May 20, 2004: FLOORBEAM. DAMAGED. STA 1110 BL 0 FLOORBEAM UPPER TEE. REPAIR STRAPS INSTALLED. - [SDR C1HA200492010](https://openairdocs.org/sdr/C1HA200492010), May 19, 2004: SKIN. CORRODED. STA 1055 STR 28L SKIN CORROSION. INSTALLED DOUBLER. - [SDR C1HA200492008](https://openairdocs.org/sdr/C1HA200492008), May 19, 2004: SHEAR TIE. CORRODED. STA 1148 STR 27L SHEAR TIE CORROSION. - [SDR C1HA200492009](https://openairdocs.org/sdr/C1HA200492009), May 19, 2004: SKIN. CORRODED. WINDOW 17 RIGHT CORROSION ON SKIN BEYOND LIMITS. INSTALLED DOUBLER. - [SDR C1HA200492007](https://openairdocs.org/sdr/C1HA200492007), May 19, 2004: SKIN. CORRODED. STA 680 STR 27R CORROSION ON SKIN. - [SDR C1HA200492011](https://openairdocs.org/sdr/C1HA200492011), May 19, 2004: SKIN. CORRODED. STA 970 STR 28L SKIN CORROSION. INSTALLED DOUBLER. - [SDR C1HA200492012](https://openairdocs.org/sdr/C1HA200492012), May 19, 2004: STRINGER. CORRODED. STA 684 STR 27R STRINGER CORRODED. INSTALLED REPAIR DOUBLER. - [SDR C1HA200492001](https://openairdocs.org/sdr/C1HA200492001), May 18, 2004: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT UPPER FLANGE. - [SDR C1HA200492002](https://openairdocs.org/sdr/C1HA200492002), May 18, 2004: SEAT TRACK. CORRODED. SEAT TRACK CORROSION. - [SDR C1HA200492004](https://openairdocs.org/sdr/C1HA200492004), May 18, 2004: STRAP. CORRODED. REPAIR STRAP CORRODED. - [SDR C1HA200492003](https://openairdocs.org/sdr/C1HA200492003), May 18, 2004: SEAT TRACK. CORRODED. SEAT TRACK CORROSION. - [SDR C1HA200392007](https://openairdocs.org/sdr/C1HA200392007), Nov 29, 2003: BATTERY PACK. INOPERATIVE. OVERHEAD EMERGENCY LIGHT BETWEEN L2 AND R2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW 727 MM 33-50-22 ALL OPS NORMAL. - [SDR C1HA200392008](https://openairdocs.org/sdr/C1HA200392008), Nov 27, 2003: POWER SUPPLY. INOPERATIVE. EXTERIOR EMERGENCY LIGHTS FOR DOORS L2 AND R2 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M983 AND BOTH OPS CKD GOOD IAW MM 33-50-01. - [SDR C1HA200392009](https://openairdocs.org/sdr/C1HA200392009), Nov 26, 2003: SUPPORT. CORRODED. WEB SUPPORT AT BS 312 BETWEEN RBL10 / 60 (IN DOG HOUSE AREA) IS EXFOLIATED AT IB WEB. - [SDR C1HA200392006](https://openairdocs.org/sdr/C1HA200392006), Oct 27, 2003: LIGHT. MALFUNCTIONED. EMERGENCY EXIT LIGHTS ILLUMINATED DURING TAXI. RAN ALL 3 ENGINES UNDER NORMAL ELEC POWER CONFIG, EMERGENCY LIGHTS DID NOT ILLUMINATE. OPERATION NORMAL. COULD NO - [SDR C1HA200392005](https://openairdocs.org/sdr/C1HA200392005), Oct 23, 2003: DUCT. DAMAGED. INFLIGHT NR 2 ENG FIRE LT, BELL ON HIGH EGT AND OIL TEMP CHECKLIST SHUTDOWN NR 2 ENG RETURN. DUMP FUEL, NR 2 ENG THROTTLE FELT STIFF, POSSIBLY BINDING. FUEL CUT - [SDR C1HA200392004](https://openairdocs.org/sdr/C1HA200392004), Aug 4, 2003: FUEL CONTROL. MALFUNCTIONED. ON TAKEOFF ROLL, NR 2 ENGINE EGT PEAKED AT 650 DEG, THEN HEATED TO 670 FOR 5 SECONDS. ABORTED TAKEOFF, FULL POWER USED FOR T/O. REMOVED AND REPLACED NR 2 ENGINE - [SDR C1HA200392003](https://openairdocs.org/sdr/C1HA200392003), Jul 15, 2003: WIRE. BROKEN. MID CABIN EMERGENCY PATH FLOOR LIGHTING INOPERATIVE. FOUND BROKEN WIRE AT ROW 21. - [SDR C1HA200392002](https://openairdocs.org/sdr/C1HA200392002), Jun 16, 2003: COMPRESSOR. STALLED. ON POWER UP 1.4 EPR CHECK NR 3 ENGINE COMPRESSOR STALL FOLLOWED BY EPR FLUCTUATION APPROX .2 TO .3. ALL OTHER ENGINE INDICATIONS NORMAL. - [SDR CH1A200392001](https://openairdocs.org/sdr/CH1A200392001), Apr 11, 2003: COMPRESSOR. STALLED. ON TAKEOFF, AN ENGINE EXPERIENCED COMPRESSOR STALL AT 1.2 EPR WINDS 300 AT 5. NO OTHER INDICATIONS - [SDR C1HA200292033](https://openairdocs.org/sdr/C1HA200292033), Dec 22, 2002: LIGHT. BROKEN. EMERGENCY LIGHT FEEL DURING TAXI OUT-RETURNED TO GATE.INSTALLED SERVICEABLE EMERG. LIGHT COVER AT DOOR 1. OK FOR SERVICE. - [SDR C1HA200292031](https://openairdocs.org/sdr/C1HA200292031), Nov 19, 2002: BATTERY. L-2 DOOR O/H INTERIOR EMERGENC LIGHT IS INOPREMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD - [SDR C1HA200292032](https://openairdocs.org/sdr/C1HA200292032), Nov 18, 2002: SOCKET. CORRODED. LEFT OVERWING EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED CORROSION FROM LIGHT SOCKETS AND RELAMPED. OPS CHECK WAS GOOD. - [SDR C1HA200292030](https://openairdocs.org/sdr/C1HA200292030), Aug 17, 2002: BATTERY. L-2 DOOR EMERGENCY LIGHT INOPREMOVED AND REPLACED BATTERY IAW M/M 33-50-00 OPS CHECK GOOD - [SDR C1HA200292007](https://openairdocs.org/sdr/C1HA200292007), Jun 24, 2002: ENGINE. LEAKING. DURING CLIMB THROUGH FL280 NR 2 ENGINE OIL TEMP INDICATED BEYOND REDLINE RADIAL. NR 2 ENGINE SHUTDOWN 2 GALLONS OF OIL LOST, OIL PRESSURE 5PSI DURING DESCENT. O - [SDR C1HA200292010](https://openairdocs.org/sdr/C1HA200292010), Jun 20, 2002: FRAME. CORRODED. CORROSION AT FS 720C BETWEEN STR 28 LT AND 28 RT UNDER LEVELING COMPOUND IN FWD PIT - [SDR C1HA200292006](https://openairdocs.org/sdr/C1HA200292006), Jun 16, 2002: SMOKE DETECTOR. INOPERATIVE. LEFT AFT LAV SMOKE DETECTION INOP. INSPECTED AND RESCHEDULED PLACARD INSTALLED AND LAV LOCKED OUT. - [SDR C1HA200292020](https://openairdocs.org/sdr/C1HA200292020), Jun 8, 2002: SKIN. CORRODED. SKIN IS EXFOLIATED AT STA 1130 O/B OF STR 27L. - [SDR C1HA200292009](https://openairdocs.org/sdr/C1HA200292009), Jun 8, 2002: STRINGER. CORRODED. STR 27 LT IS EXFOLIATED AT STA 1120 - [SDR C1HA200292008](https://openairdocs.org/sdr/C1HA200292008), Jun 7, 2002: STRINGER. CORRODED. STR 27 LT CORRODED FROM STA 950F - 1010 IN NUMEROUS AREAS - [SDR C1HA200292019](https://openairdocs.org/sdr/C1HA200292019), Jun 6, 2002: STRINGER. CORRODED. STR 27 RT AT APPROX STA 1060 IS CORRODED - [SDR C1HA200292027](https://openairdocs.org/sdr/C1HA200292027), May 31, 2002: STRINGER. CORRODED. STR 30 IS EXFOLIATED ON RT SIDE BETWEEN STA 950 AND 950A. - [SDR C1HA200292021](https://openairdocs.org/sdr/C1HA200292021), May 31, 2002: SHEAR TIE. CORRODED. SHEAR TIE HAS LIGHT SURFACE CORROSION AT STA 965 JUST OUT BOARD OF RBL 28 - [SDR C1HA200292025](https://openairdocs.org/sdr/C1HA200292025), May 26, 2002: SHEAR TIE. CORRODED. SHEAR TIE AT STA 950B IS CORRODED ON FWD SIDE BETWEEN INTERCOSTAL AND STR 29 LT. - [SDR C1HA200292029](https://openairdocs.org/sdr/C1HA200292029), May 24, 2002: FLOORBEAM. CORRODED. FLOORBEAM STA 1030 LBL 45 - RBL 8 HAS CORROSION AND LBL 12 HAS A HOLE WITH NO EDGE DISTANCE. - [SDR C1HA200292024](https://openairdocs.org/sdr/C1HA200292024), May 23, 2002: FRAME. CORRODED. FRAME 950A IS CORRODED ON FWD SIDE BETWEEN STR 28R AND 30 - [SDR C1HA200292015](https://openairdocs.org/sdr/C1HA200292015), May 23, 2002: ATTACH FITTING. CORRODED. LT MLG FWD TRUNION BEARING ATTACH FITTING HAS CORROSION AND PITTING ON INBD SIDE OF INBD FLANGE All 80: https://openairdocs.org/deregistered/N292AS-2009-01-20/reports.md ## 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 19870913069589I](https://openairdocs.org/incident/19870913069589I), Sep 13, 1987: Boeing 727212 (N292AS), Juneau, AK. Aircraft touched down 40 feet prior to the displaced threshold. Aircraft rolled over plastic conduit and broke it. ## Other aircraft with N292AS - [Cancelled 2013-03-11](https://openairdocs.org/deregistered/N292AS-2013-03-11): Boeing 747-4B5, S/N 24198. Owner: [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables) --- 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.