# N817AL: 1982 Boeing 737-2X6C, registration cancelled 2010-11-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 16, 2010
- Exported to: South Africa
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-2X6C](https://openairdocs.org/model/boeing-737-2x6c) (registry code 138447B)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 23292
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 19, 1998
- Certificate issued: December 4, 1995
- Last registry action: September 16, 2008
- Mode S code: AB2368
- Owner when cancelled: [Bjet Inc](https://openairdocs.org/faa-owner/BJET%20INC)
- Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston)
- Owner type: Corporation
- Owner's area on the map: 29.7441° N, 95.4892° W: Placed by OpenAirDocs at the center of ZIP code 77057, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N817AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=817AL
- Page: https://openairdocs.org/deregistered/N817AL-2010-11-16

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 737-2X6C: https://openairdocs.org/model/boeing-737-2x6c.md

## Service difficulty reports (117, newest 50)

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

- [SDR TSAA0753060](https://openairdocs.org/sdr/TSAA0753060), Oct 28, 2007: SKIN. CRACKED. IN THE PROCESS OF ECO 3512, NDT INSPECTION DISCOVERED THE AFT CARGO DOOR CUTOUT AFT FRAME CRACKED. REPLACED THE FRAME IN ACCORDANCE WITH ECO 3512.
- [SDR TSAA0628053](https://openairdocs.org/sdr/TSAA0628053), Jul 12, 2006: PUMP. MALFUNCTIONED. AFTER LEVELING OFF AT 21,000 FEET, THE NR 2 FORWARD FUEL BOOST PUMP LIGHT BEGAN FLICKERING ON AND OFF. THE CREW REVIEWED THEIR QRH AND CONTACTED MAINTENANCE CON
- [SDR TSAA0577041](https://openairdocs.org/sdr/TSAA0577041), Sep 19, 2005: LINE. OBSTRUCTED. CARGO FLT 820 HNL-OGG. AT CRUISE, CREW NOTED NR 1 ENGINE EPR 0.30 LESS THAN NR 2 ENGINE. N1 AND N2 SAME ON BOTH ENGINES. CREW RETURNED TO HNL WITHOUT FURTHER IN
- [SDR TSAA0577033](https://openairdocs.org/sdr/TSAA0577033), Jul 27, 2005: TRANSMITTER. DEFECTIVE. FLT 850 HNL - ITO. ON TAKEOFF, NUMBER 1 ENGINE PRESSURE RATIO INDICATION STOPPED INCREASING AT 170 WHILE THE NUMBER 2 ENGINE INDICATION OPERATED NORMALLY. CREW 
- [SDR TSAA0475073](https://openairdocs.org/sdr/TSAA0475073), Sep 29, 2004: LINE. LOOSE. NR 1 ENGINE WILL NOT REACH TAKEOFF POWER; REPORTED BY CREW. MAINTENANCE TROUBLE SHOOTING FOUND THE AFT PT7 LINE LOOSE. SECURED THE LINE; RAN ENGINE TO POWER. AL
- [SDR TSAA0475050](https://openairdocs.org/sdr/TSAA0475050), Jun 28, 2004: DUCT. FAILED. DURING CLIMB-OUT, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON. RETURNED TO HNL. REMOVED AND REPLACED THE NR 2 ENGINE NOSE-COWL ANTI-ICE DUCT DUE TO LEAK AT THE BELLO
- [SDR TSAA0434049](https://openairdocs.org/sdr/TSAA0434049), Jun 21, 2004: INDICATOR. FAILED. CAPTAINS VERTICAL SPEED INDICATOR INOPERATIVE. RETURN TO HNL. REPLACED VERTICAL SPEED INDICATOR, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0434043](https://openairdocs.org/sdr/TSAA0434043), Jun 1, 2004: PITOT TUBE. CONTAMINATED. CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS READ 20 KTS DIFFERENCE. RETURNED TO HNL. REMOVED FOD FROM PITOT TUBE, SYS OPS & LEAK CHECK GOOD IAW AMM 34-11-00
- [SDR TSAA0353108](https://openairdocs.org/sdr/TSAA0353108), Apr 24, 2003: SKIN. CRACKED. TRIMMED OUT DAMAGED AREA. VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED REPAIR DOUBLER FORM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED RE
- [SDR TSAA0353060](https://openairdocs.org/sdr/TSAA0353060), Apr 7, 2003: SKIN. CRACKED. CUT OUT DAMAGED AREA. VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR PLATE. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS USING FASTENERS IDE
- [SDR TSAA0333052](https://openairdocs.org/sdr/TSAA0333052), Feb 13, 2003: BATTERY PACK. DISCHARGED. REPLACED NR 2 FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0249213](https://openairdocs.org/sdr/TSAA0249213), Oct 17, 2002: APU. FAILED. JUST AFTER TAKEOFF THE APU OVERSPEED LIGHT CAME ON AND THE APU SHUTDOWN. THE AIRCRAFT RETURNED AND LANDED, WITH NO FURTHER INCIDENT. REPLACED THE APU ACCESSORY 
- [SDR TSAA0253202](https://openairdocs.org/sdr/TSAA0253202), Sep 25, 2002: FLAP TRACK. DAMAGED. FLAP TRACK ATTACHMENT FITTING HOLE ELONGATED. REPAIRED AND AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0251192](https://openairdocs.org/sdr/TSAA0251192), Aug 26, 2002: SKIN. CRACKED. BS 380 STRING 15R CRACK ON FUS SKIN. HFEC INSP EDGES ON CUTOUT, .040 IN INSUR CUT, FAB 2024-T3, CLAD SHEET .032 IN FILLER, .050 IN FILLER, AND .050 DOUBLER, MAI
- [SDR TSAA0277173](https://openairdocs.org/sdr/TSAA0277173), Aug 11, 2002: TRANSMITTER. INOPERATIVE. NR 1 ENGINE EPR DROPPED OFF ON CLIMB OUT OF 7,000 FEET. NR 1 ENGINE EPR WAS 1.73 AND NR 2 ENGINE EPR WAS 1.85. BOTH THE NR 1 AND NR 2 ENGINES NR 1 WAS 89 PERCEN
- [SDR TSAA0271172](https://openairdocs.org/sdr/TSAA0271172), Aug 11, 2002: LINE. OBSTRUCTED. DURING CLIMB THE NR 1 ENGINE EGT INDICATED 600 DEGREES C WITH THRUST LEVER 4 INCHES AHEAD OF THE NR 2 ENGINE THRUST LEVER. THE NR 1 ENGINE EPR WAS 1.73 AND THE 
- [SDR TSAA0253164](https://openairdocs.org/sdr/TSAA0253164), Jul 8, 2002: SKIN. CRACKED. IDENTIFIED A TWO AND A HALF INCH CRACK ON FUSELAGE SKIN AT BS 942 STRINGER 24R. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRI
- [SDR TSAA0253163](https://openairdocs.org/sdr/TSAA0253163), Jul 8, 2002: SKIN. CRACKED. IDENTIFIED A TWO INCH CRACK ON FUSELAGE SKIN AT BS962 STRINGER 21L. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED A FILL
- [SDR TSAA0253162](https://openairdocs.org/sdr/TSAA0253162), Jul 8, 2002: SKIN. CRACKED. IDENTIFIED ONE INCH CRACK ON FUSELAGE SKIN AT BS 277 STRINGER 11L. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED A FILLE
- [SDR TSAA0253161](https://openairdocs.org/sdr/TSAA0253161), Jul 8, 2002: SKIN. CRACKED. IDENTIFIED A TWO INCH CRACK ON FUSELAGE SKIN AT BS274 STRINGER 15R. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED FILLER
- [SDR TSAA0233154](https://openairdocs.org/sdr/TSAA0233154), Jun 29, 2002: LIGHT. DAMAGED. REPLACED FORWARD ENTRY DOOR IDENTIFIER LIGHT ASSEMBLY DUE TO DAMAGE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233153](https://openairdocs.org/sdr/TSAA0233153), Jun 29, 2002: BATTERY PACK. DISCHARGED. REPLACED FORWARD ENTRY DOOR IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSA2002F00000](https://openairdocs.org/sdr/TSA2002F00000), Jun 19, 2002: WIRE HARNESS. WORN. ENROUTE , THE APU SHUTDOWN DUE TO AN OVERSPEED. THE AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE RESTARTED THE APU AND CONDUCTED AN OPERATIONAL CHECK
- [SDR TSAA0233044](https://openairdocs.org/sdr/TSAA0233044), Feb 14, 2002: BATTERY PACK. INOPERATIVE. REPLACED NR 2 FLOOR PATH EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133171](https://openairdocs.org/sdr/TSAA0133171), Dec 2, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 2 FLOOR PROXIMATELY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153154](https://openairdocs.org/sdr/TSAA0153154), Nov 15, 2001: SKIN. CORRODED. DISCOVERED BULGING AT BS 1088, S-20R FUSELAGE SKIN. REMOVED THE CORRODED PORTION OF THE STRAP, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER. RECEIVED 811
- [SDR TSAA0153157](https://openairdocs.org/sdr/TSAA0153157), Nov 14, 2001: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN NUMEROUS AREAS AT LT FUSELAGE WINDOW CORNERS; 2 BETWEEN BS 500-
- [SDR TSAA0157155](https://openairdocs.org/sdr/TSAA0157155), Nov 9, 2001: SKIN. CORRODED. DISCOVERED CORROSION ON LEFT LOWER WING SURFACE, WS 500. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRCRA
- [SDR TSAA0157156](https://openairdocs.org/sdr/TSAA0157156), Nov 7, 2001: SKIN. CORRODED. DISCOVERED CORROSION AT LEFT LOWER WING SURFACE, WS 515.5. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRC
- [SDR TSAA0179120](https://openairdocs.org/sdr/TSAA0179120), Sep 28, 2001: PRESSURE SWITCH. FAULTY. FLT 953 - ITO-HNL - DURING A NON-ETOPS QC CARGO FLIGHT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON. SHUTDOWN THE NR 1 ENGINE AND DECLARED AN EMERGENCY. UNE
- [SDR TSAA0133114](https://openairdocs.org/sdr/TSAA0133114), Aug 31, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133094](https://openairdocs.org/sdr/TSAA0133094), Jul 20, 2001: BATTERY PACK. INOPERATIVE. REPLACED NR 1 FLOOR EMERGENCY LGIHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0124078](https://openairdocs.org/sdr/TSAA0124078), Jun 20, 2001: CSD. FAILED. FLT 915 - HNL-LIH - DURING FLIGHT, THE LOW OIL PRESSURE LIGHT CAME ON AND THE NR 1 ENGINE CSD GENERATOR WAS DISCONNECTED AQ MAINTENANCE WAS CONTACTED AND ADVISE
- [SDR TSAA0153057](https://openairdocs.org/sdr/TSAA0153057), May 8, 2001: SKIN. DAMAGED. FUSELAGE SKIN WRINKLE BETWEEN BS 663.75 AND BS 706, S13 AND S16. (M)
- [SDR TSAA0153058](https://openairdocs.org/sdr/TSAA0153058), May 8, 2001: SKIN. DAMAGED. FOUND FUSELAGE SKIN WRINKLE BETWEEN BS 663.75 AND BS 706, S13L AND S16L. (M)
- [SDR TSAA0153059](https://openairdocs.org/sdr/TSAA0153059), May 7, 2001: FRAME. CRACKED. FUSELAGE BS 727, STRINGER 18A LEFT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M)
- [SDR TSAA0153060](https://openairdocs.org/sdr/TSAA0153060), May 7, 2001: FRAME. CRACKED. FOUND FUSELAGE BS 727, STRINGER 18A RIGHT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M)
- [SDR TSAA0153061](https://openairdocs.org/sdr/TSAA0153061), May 1, 2001: PRESSURE PANEL. CRACKED. FOUND CRACK NOTED AT LEFT UPPER CORNER NLG PRESSURE PANEL. CONFIRMED CRACK BY UTILIZING HFEC METHOD. (M)
- [SDR TSAA0153062](https://openairdocs.org/sdr/TSAA0153062), May 1, 2001: SKIN. CRACKED. DURING HARD LANDING INSPECTION, DISCOVERED 2 INCHES CRACK AT BS 540, STRINGER 1R AND 2R, VERIFIED BY USING HFEC. (M)
- [SDR TSAA0133041](https://openairdocs.org/sdr/TSAA0133041), Apr 21, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133029](https://openairdocs.org/sdr/TSAA0133029), Mar 3, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 1 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0152018](https://openairdocs.org/sdr/TSAA0152018), Feb 18, 2001: DOOR. CRACKED. IDENTIFIED CRACKS AT 3.25 INCH PROPAGATING FROM ONE RIVET TO ADJACENT RIVET ON MAIN CARGO DOOR AT BS 430, 2 INCHES BELOW STRINGER 14L CONFIRMED BY UTILIZING HFE
- [SDR TSAA0033258](https://openairdocs.org/sdr/TSAA0033258), Sep 3, 2000: BATTERY PACK. DISCHARGED. REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0032192](https://openairdocs.org/sdr/TSAA0032192), Aug 15, 2000: SELECTOR VALVE. LEAKING. FLT 248 - LIH-HNL - CLIMBING THROUGH 10,000 FT, BOTH MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED WITH THE LANDING GEAR HANDLE IN THE OFF POSITION. AFTER REVIEWIN
- [SDR TSAA0033183](https://openairdocs.org/sdr/TSAA0033183), Aug 1, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033176](https://openairdocs.org/sdr/TSAA0033176), Jun 23, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033156](https://openairdocs.org/sdr/TSAA0033156), Jun 23, 2000: LIGHT. INOPERATIVE. REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0053158](https://openairdocs.org/sdr/TSAA0053158), May 25, 2000: DOOR FRAME. DAMAGED. REPAIRED MAIN CARGO DOOR CUTOUT FRAME LEFT SIDE STATION 500, WBL 264.5 BY BLENDOUT OF ELONGATED FRAME HOLE IAW ECO 3145. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0027157](https://openairdocs.org/sdr/TSAA0027157), May 23, 2000: SKIN. CORRODED. REPAIRED RIGHT AILERON CONTROL QUADRANT AT WING STATION 519 BY BLENDOUT AND TREATING CORROSION IAW ECO 3147. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033124](https://openairdocs.org/sdr/TSAA0033124), Apr 24, 2000: BATTERY PACK. INOPERATIVE. REPLACED FORWARD EXIT IDENTIFIER POWER PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

All 117: https://openairdocs.org/deregistered/N817AL-2010-11-16/reports.md

## Other aircraft with N817AL

- [Registered now](https://openairdocs.org/aircraft/N817AL): Zipline International P2 ZIP, S/N 18736P22570

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