# N295AS: 1980 Boeing 727-290, registration cancelled 2014-10-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 29, 2014
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-290](https://openairdocs.org/model/boeing-727-290) (registry code 138408W)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22147
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 28, 1980
- Certificate issued: January 8, 2009
- Last registry action: January 8, 2009
- Mode S code: A3081E
- Owner when cancelled: [Airlease International Inc](https://openairdocs.org/faa-owner/AIRLEASE%20INTERNATIONAL%20INC)
- Location: [Hot Springs, AR](https://openairdocs.org/faa-place/AR/Hot%20Springs)
- Owner type: Corporation
- Owner's area on the map: 34.5267° N, 92.9735° W: Placed by OpenAirDocs at the center of ZIP code 71901, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N295AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=295AS
- Page: https://openairdocs.org/deregistered/N295AS-2014-10-29

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 727-290: https://openairdocs.org/model/boeing-727-290.md

## Service difficulty reports (139, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CIHA200759026](https://openairdocs.org/sdr/CIHA200759026), May 4, 2007: SUPPORT ANGLE. CORRODED. STRINGER 26L TO FRAME SUPPORT ANGLE CORRODED BS 950F. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW B727 SRM 51-10-3 FIG 2 & 51-30-2 FIG
- [SDR C1HA200795011](https://openairdocs.org/sdr/C1HA200795011), May 4, 2007: SUPPORT. CORRODED. SURFACE CORROSION ON MAIN CABIN FWD LAV AFT WALL SUPPORT BS 344 RBL 15 - RBL 65. REPLACED LAV SUPPORT BS 344 RBL 15 TO 65 IAW B727 SRM 53-10-2.
- [SDR C1HA200795006](https://openairdocs.org/sdr/C1HA200795006), May 4, 2007: FRAME. CRACKED. COCKPIT FRAME AT STA 277 AND STR 16RT IS CRACKED APPROX 1 INCH LONG, VERIFED BY HFEC (BEHIND FE CONSOLE). REPAIRED COCKPIT FRAME AT STA 277, STR 16RT IAW B727 S
- [SDR C1HA200795008](https://openairdocs.org/sdr/C1HA200795008), May 4, 2007: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BS 420-480 RBL 55. REPLACED SEAT TRACK FROM BS 420 TO 480 RBL 55 IAW B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 7.
- [SDR CIHA200795010](https://openairdocs.org/sdr/CIHA200795010), May 4, 2007: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BS 344 - 380 RBL 45. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7.
- [SDR C1HA200795004](https://openairdocs.org/sdr/C1HA200795004), May 4, 2007: SUPPORT ANGLE. CRACKED. LEFT VENTRAL STAIRWELL LT TORQUE BOX SUPPORT ANGLE IS CRACKED AT STA 1253 BELOW BAZOOKA TUBES. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1253 LEFT TORQUE BO
- [SDR C1HA200795001](https://openairdocs.org/sdr/C1HA200795001), May 4, 2007: ANGLE. CRACKED. RIGHT WING L/E STA 130.7 INTERNAL ANGLE AT FRONT SPAR LWR CRACKED. FABRICATED AND INSTALLED REPAIR PART IAW B727 M/M 57-20-21 PG 801 AND SEALED AS REQUIRED IAW 
- [SDR C1HA200795021](https://openairdocs.org/sdr/C1HA200795021), May 4, 2007: ANGLE. CORRODED. ANGLE CORRODED RIGHT CUSP ANGLE TO FRAME SPLICE ATTACHED AFT SIDE OF STA 740 RIB AT FLOOR LEVEL STA 740-743 RBL 61. CORROSION FOUND OUT OF LIMITS. REPLACED ANGL
- [SDR C1HA200795020](https://openairdocs.org/sdr/C1HA200795020), May 4, 2007: STRINGER. CRACKED. FOUND STRINGER 15R CRACKED AT BS 720B. REPAIRED STR 15R AT BS 720B IAW B727 SRM 53-10-3 FIG 5.
- [SDR C1HA200795003](https://openairdocs.org/sdr/C1HA200795003), May 4, 2007: SKIN. CRACKED. FOUND FUSE BS 1098 RBL 1 HAS 1/2" CRACK IN FASTENER HOLE. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SB 727-53A0204 REV 3 FIG 2 AND 
- [SDR C1HA200795014](https://openairdocs.org/sdr/C1HA200795014), May 4, 2007: BRACKET. CORRODED. FOUND CORROSION EMANATING FROM BENEATH ANGLE BRACKET O/B OF AFT LAV FITTINGS AT STA 1165 RBL 45. REPLACED BRACKET ANGLE IAW B727 SRM 51-40-3 AND 53-10-2 AND REP
- [SDR C1HA200795012](https://openairdocs.org/sdr/C1HA200795012), May 4, 2007: ANGLE. CORRODED. FOUND CORROSION ON WEB ANGLE IN SEVERAL MARKED AREAS BETWEEN STA 1148-1165 RBL 60. REPLACED ANGLE BETWEEN STA 1148 TO 1165 RBL 60 IAW B727 SRM 53-10-2 AND 51-40
- [SDR C1HA200795016](https://openairdocs.org/sdr/C1HA200795016), May 4, 2007: SEAT TRACK. CORRODED. FOUND SEAT TRACK CORRODED IN SEVERAL MARKED AREAS STA 999-1110 LBL 25. REMOVED AND REPLACED SEAT TRACK ON STA 1010-1130 LBL 25 IAW B727 SRM 51-30-2 AND 53-10-5 
- [SDR C1HA200795033](https://openairdocs.org/sdr/C1HA200795033), May 4, 2007: STRINGER SPLICE. CORRODED. FOUND FWD CARGO COMPARTMENT AT BS 540 STR 26R HAS HEAVY CORROSION AT SPLICE. REMOVED AND REPLACED FWD CARGO BS 540 STR 26R SPLICE ANGLE IAW B727 SRM 53-10-2 AND
- [SDR C1HA200795032](https://openairdocs.org/sdr/C1HA200795032), May 4, 2007: STRINGER. CORRODED. FOUND CORROSION IN E/E BAY AT BS 475 STR 27L. REPAIRED STR 27L AT BS 475 IAW B727 SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1.
- [SDR C1HA200795031](https://openairdocs.org/sdr/C1HA200795031), May 4, 2007: STRINGER SPLICE. CORRODED. FOUND CORROSION IN E/E BAY AT BS 475 STR 26L. REMOVED EXISTING MANUFACTURE SPLICE, FABRICATED AND INSTALLED NEW SPLICE IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200795022](https://openairdocs.org/sdr/C1HA200795022), May 4, 2007: SEAT TRACK. CORRODED. FOUND CABIN SEAT TRACK AT BS 740-760 LBL 24 IS CORRODED BEYOND LIMITS. REPLACED MAIN CABIN SEAT TRACK AT BS 740-760 LBL 24 IAW B727 SRM 53-10-2 AND 53-10-5.
- [SDR C1HA200795019](https://openairdocs.org/sdr/C1HA200795019), May 4, 2007: STRINGER. CRACKED. FOUND STR 15L CRACKED AT BS 720C. REPAIR STR 15L AT BS 720C IAW B727 SRM 53-10-3 FIG 5.
- [SDR C1HA200795024](https://openairdocs.org/sdr/C1HA200795024), May 4, 2007: FLOORBEAM. CORRODED. BS 1130 FLOORBEAM AT LOWER FORWARD FLANGE HAS CORROSION (RBL-10). FOUND CORROSION OUT LIMITS, CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLERS, ANGLE, RADIUS FI
- [SDR C1HA200795027](https://openairdocs.org/sdr/C1HA200795027), May 4, 2007: STRINGER. CORRODED. FOUND CORROSION ON FRAME STA 420 BL 0 TO STR 28R. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED AND INSTALLED NEW SECTION FROM BS 400-420 STR 28R IAW B727 SRM
- [SDR C1HA200795005](https://openairdocs.org/sdr/C1HA200795005), May 4, 2007: PLENUM. CORRODED. A/C RAM AIR PLENUM HAS SURFACE CORROSION ON NR 2 TANK LWR SKIN ABOVE LT PRIMARY HEAT EXCHANGER. BLENDED OUT CORROSION DAMAGE, MAT LOSS .050, ORIGINAL THK .225. 
- [SDR C1HA200795023](https://openairdocs.org/sdr/C1HA200795023), May 4, 2007: SHEAR WEB. CORRODED. AFT CABIN LT SHEAR WEB BS 1166 LBL 35 HAS HEAVY PITTED CORROSION. REPAIRED AFT CABIN LT SHEAR WEB AT BS 1166 LBL 35 IAW B727 SRM 53-10-2 AND 51-40-2.
- [SDR C1HA200795009](https://openairdocs.org/sdr/C1HA200795009), May 4, 2007: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK BS 380 - 460 RBL 45. REPLACED SEAT TRACK AT BS 380 TO 460 RBL 45 IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7.
- [SDR C1HA200795002](https://openairdocs.org/sdr/C1HA200795002), May 4, 2007: SKIN. CRACKED. EXT FUSE BS 303 AT L-1 DOOR LOWER HINGE HAS REPAIR DOUBLER CRACKED IN FWD CUTOUT. REMOVED EXISTING REPAIR DOUBLER, HFEC INSP AND FOUND SKIN AND INNER DOUBLER CR
- [SDR C1HA200795025](https://openairdocs.org/sdr/C1HA200795025), May 4, 2007: STRINGER. CORRODED. FOUND CORROSION AT STA 740. CUT OUT DAMAGED AREA FROM STR 27L AT STA 740, FAB`D STR REPAIR AND SPLICE. TREATED AND PRIMED. REMOVED AND REPLACED DAMAGED FITTING 
- [SDR C1HA200795029](https://openairdocs.org/sdr/C1HA200795029), May 4, 2007: FRAME. CORRODED. FOUND CORROSION STA 351.2 FRAME AT 28R. REMOVED EXISTING TEE CHORD FRAME, FABRICATED AND INSTALLED NEW TEE CHORD IAW B727 SRM 53-10-2 FIG 1.
- [SDR C1HA200795017](https://openairdocs.org/sdr/C1HA200795017), May 4, 2007: SEAT TRACK. CORRODED. FOUND MAIN CABIN STA 880 TO 950 LBL 24 SEAT TRACK HAS CORROSION ON TOP SURFACE. FABRICATED AND INSTALLED NEW SEAT TRACK P/N BAC1520-792 (91") IAW B727 SRM 53-10
- [SDR C1HA200795007](https://openairdocs.org/sdr/C1HA200795007), May 4, 2007: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK AT AFT CUTOUT AND MOUNT POINT STA 1130 LBL 25. REPLACED SEAT TRACK AT BS 1110-1130 LBL 25, P/N BAC1520-792 IAW B727 SRM 53-10-5 FI
- [SDR C1HA200795028](https://openairdocs.org/sdr/C1HA200795028), May 4, 2007: STRINGER. CORRODED. FOUND CORROSION STR 28L AT STA 410. REPAIRED STRINGER AT BS 410 28L IAW B727 SRM 53-10-2 AND 53-10-3 FIG 1.
- [SDR C1HA200795030](https://openairdocs.org/sdr/C1HA200795030), May 4, 2007: STRINGER. CORRODED. FOUND CORROSION STR 26R STA 470. FABRICATED AND INSTALLED REPAIR PARTS FOR STRINGER 26R BS 450 - 490 IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200795015](https://openairdocs.org/sdr/C1HA200795015), May 4, 2007: FLOORBEAM. CORRODED. FOUND FLOORBEAM CORRODED AT STA 1110 LBL 25-45. REPAIRED FLOORBEAM STA 1110 FROM RBL 20 TO LBL 65 IAW B727 SRM 53-10-8 FIG 3.
- [SDR C1HA200795018](https://openairdocs.org/sdr/C1HA200795018), May 4, 2007: STRINGER. CRACKED. FOUND STRINGER 15L CRACKED AT BS 720B. REPAIRED STRINGER 15L AT BS 720B IAW B727 SRM 53-10-3 FIG 5.
- [SDR C1HA200695003](https://openairdocs.org/sdr/C1HA200695003), Nov 25, 2006: VALVE. STUCK. NR 1 ENGINE WAS SHUT DOWN ON START-EGT 550 DEG AND IT APPEARED THAT IT WOULD NOT STABILIZE AT OR BELOW 550 DEG. RAN COM 2-72.9 FOUND NR 1 ENG 13 TH STAGE BLEED 
- [SDR C1HA200695002](https://openairdocs.org/sdr/C1HA200695002), Jun 12, 2006: UNKNOWN. MALFUNCTIONED. AFTER TAKEOFF AC FAILED TO PRESSURIZE, RAN COM PROCEDURE 2.21.5. ON DESCENT EQUIP ENTRY LIGHT FLICKERD, RAN COM PROCEDURE 2.52.3. RETURNED TO DEN. INSPECTED BOT
- [SDR C1HA200695001](https://openairdocs.org/sdr/C1HA200695001), May 13, 2006: SEAL. DAMAGED. ON TAXI INTO DEN, UPPER RUDDER INDICATOR DIDN'T MOVE FULLY TO THE LIMIT LINE WHEN RIGHT RUDDER WAS FULLY APPLIED. LEFT RUDDER OPERATED NORMALLY FOUND FIN FAIRIN
- [SDR C1HA200595007](https://openairdocs.org/sdr/C1HA200595007), May 5, 2005: CONNECTOR. LOOSE. UPON APPLICATION OF T/O THRUST (FULL), NR 1 ENGINE WOULD NOT MAKE FULL EPR OF 2.14 ONLY 2.05. ALL OTHER PARAMETERS IN YELLOW ARC + POWER LEVER AT FORWARD STOP. 
- [SDR C1HA200595006](https://openairdocs.org/sdr/C1HA200595006), Apr 9, 2005: FRAME. CORRODED. E & E COMPT STA 320 RBL 17 FRAME LOWER END HAS CORROSION. EGG NEW FLOOR & CLEAR TIE AT FS 320 RBL 17 7075-0 PO 0420685 H/T TO T-6 ON PEMCO TRAVELER 795N000486. 
- [SDR C1HA200595005](https://openairdocs.org/sdr/C1HA200595005), Apr 8, 2005: SKIN. DENTED. FUSELAGE SKIN 2.7 INCH AFT OF STA 259 AND JUST BELOW STR 17L HAS OUTWARD DENT, MARKED P4. CUT OUT DENT DAMAGE, FAB FILLER USING .050 2024T3 PO 0440785 AND REPAI
- [SDR C1HA200595003](https://openairdocs.org/sdr/C1HA200595003), Apr 8, 2005: ANGLE. CRACKED. LEFT WING LOWER ANGLE CRACKED AT STA WS 124 BELOW NR 7 SPOILER SUPPORT FITTING. REMOVED 2 EA AFT ATTACH BOLTS FROM I/B FLAP TRACK, REMOVED TRACKED LOWER ANGLE C
- [SDR C1HA200595004](https://openairdocs.org/sdr/C1HA200595004), Apr 5, 2005: KEELBEAM. CRACKED. RIGHT WHEEL WELL STA 875 ANGLE CRACKED KEELBEAM APPROX 1 INCH LONG. REMOVED AND REPLACED ANGLE IN RIGHT WHEEL WELL AT STA 875 AT KEEL BEAM IAW B727 SRM 51-30-2.
- [SDR C1HA200595002](https://openairdocs.org/sdr/C1HA200595002), Apr 5, 2005: SKIN. CRACKED. LEFT WING - L/E NR 3 SLAT AT O/B SLAT TRACK ATTACH POINT SLAT SKIN IS CRACKED APPROX .5 INCH. TRIMMED CRACKED AREA LENGTH OF CRACK APPROX .500 LONG IAW BOEING 7
- [SDR C1HA200595001](https://openairdocs.org/sdr/C1HA200595001), Apr 5, 2005: SKIN. CRACKED. LEFT WING - L/E NR 3 SLAT AT I/B SLAT TRACK ATTACH POINT SLAT SKIN IS CRACKED APPROX .5 INCH. TRIMMED CRACKED AREA LENGTH OF CRACK APPROX .500 LONG IAW BOEING 7
- [SDR C1HA200495001](https://openairdocs.org/sdr/C1HA200495001), Feb 27, 2004: SUPPORT BRACKET. BROKEN. NOSE GEAR FAILED TO EXTEND. COMPLIED WITH COM PROCEDURE, CRANKED ALL GEAR MANUALLY.
- [SDR C1HA200395071](https://openairdocs.org/sdr/C1HA200395071), Dec 1, 2003: BATTERY PACK. INOPERATIVE. OVERHEAD EMERGENCY LIGHT INOP AT ROW 4. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW 727 MM 33-50-22, ALL OPS NORMAL.
- [SDR C1HA200395069](https://openairdocs.org/sdr/C1HA200395069), Sep 19, 2003: UPLOCK. WORN. DURING TAKEOFF ROLL RED DOORS LIGHT ON FORWARD PANEL ILLUMINATED, LT GEAR DOOR LIGHT (AMBER) ON ENGINEERS PANEL ILLUMINATED TAKE OFF WAS ABORTED AT 80 KTS. VERY
- [SDR C1HA200395068](https://openairdocs.org/sdr/C1HA200395068), Sep 17, 2003: JACKSCREW. LACK OF LUBE. DURING FLAP RETRACTION AFTER TAKEOFF OUTBOARD FLAPS RETRACTED TO 2 DEGREE POSITION WHILE INBOARDS REMAINED AT 5 DEGREE POSITION. RAN SPLIT FLAP EMERGENCY PROCED
- [SDR C1HA200395066](https://openairdocs.org/sdr/C1HA200395066), Aug 25, 2003: BATTERY. INOPERATIVE. STA. 950 EMERGENCY CABIN AREA LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY CABIN BATTERY ASSEMBLY PER M/M 33-50-21.
- [SDR C1HA200395065](https://openairdocs.org/sdr/C1HA200395065), Jun 30, 2003: BATTERY PACK. INOPERATIVE. LEFT FWD OVERWING OUTSIDE EMERGENCY EXIT LIGHT INOP.
- [SDR C1HA200395064](https://openairdocs.org/sdr/C1HA200395064), Jun 30, 2003: BATTERY PACK. INOPERATIVE. RIGHT FWD OVERWING OUTSIDE EMERGENCY EXIT LIGHT INOP.
- [SDR C1HA200395063](https://openairdocs.org/sdr/C1HA200395063), Jun 30, 2003: BATTERY PACK. INOPERATIVE. LEFT FWD OVERWING EMERGENCY EXIT LIGHT INOP.

All 139: https://openairdocs.org/deregistered/N295AS-2014-10-29/reports.md

## 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 20041029028569I](https://openairdocs.org/incident/20041029028569I), Oct 29, 2004: Boeing 727290 (N295AS), Columbia, MO. (-23) Champion airlines (ccp) flight 616 was taxiing for departure on runway 20 at Columbia, Missouri (cou). Columbia ATCT cleared ccp 616 for takeoff. The…
- [Incident 19890918054079I](https://openairdocs.org/incident/19890918054079I), Sep 18, 1989: Boeing 727290 (N295AS), Juneau, AK. Fuel leak from top of left wing. Lost 1500 lbs of fuel. Reinstalled fuel cap.

## Other aircraft with N295AS

- [Registered now](https://openairdocs.org/aircraft/N295AS): Ea Vision EA J100, S/N EAVUAV502585878

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