# N816AL: 1984 Boeing 737-2X6C, registration cancelled 2008-07-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 9, 2008
- Exported to: Canada
- 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: 23122
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: July 28, 1995
- Certificate issued: June 5, 1995
- Last registry action: June 19, 2007
- Mode S code: AB1FB1
- Owner when cancelled: [Ajet Inc](https://openairdocs.org/faa-owner/AJET%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/N816AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=816AL
- Page: https://openairdocs.org/deregistered/N816AL-2008-07-09

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 (147, newest 50)

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

- [SDR TSAA0753059](https://openairdocs.org/sdr/TSAA0753059), Oct 28, 2007: SKIN. CRACKED. IN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED LT SKIN CRACKED INSIDE LT WING TO BODY FAIRING. CRACK LOCATED AT BS 747 +19 BETWEEN STRINGER 21L AND 22L. CRAC
- [SDR TSAA0753058](https://openairdocs.org/sdr/TSAA0753058), Oct 28, 2007: SKIN. CRACKED. IN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED RT SKIN CRACKED IS BETWEEN LAP JOINT AND LARGE EXISTING REPAIR. CRACK LOCATED AT BS 927 +13 BETWEEN STRINGER 2
- [SDR TSAA0734041](https://openairdocs.org/sdr/TSAA0734041), Jul 18, 2007: HSI. FAILED. CARGO FLIGHT 944 HNL-KOA - DURING CLIMB, THE CAPTAIN NOTED THE NR 1 HORIZONTAL SITUATION INDICATOR HAD THE COMPASS FLAG IN VIEW. THE CAPTAIN ATTEMPTED TO TRANSF
- [SDR TSAA0752039](https://openairdocs.org/sdr/TSAA0752039), Jun 29, 2007: PROXIMITY SENSOR. DIRTY. FLIGHT 940 HNL-KOA - ON TAKEOFF ROLL, CREW NOTED THE DOOR ANNUNCIATOR LIGHT ILLUMINATED AND ABORTED THE TAKEOFF AT 110 KNOTS INDICATED AIRSPEED. CREW RETURNED T
- [SDR TSAA0652092](https://openairdocs.org/sdr/TSAA0652092), Oct 29, 2006: PITOT TUBE. OBSTRUCTED. FLIGHT 940 HNL-KOA. AFTER TAKEOFF, CREW NOTED THE LOSS OF FIRST OFFICER'S AIRSPEED INDICATION AND THE ILLUMINATION OF THE DOOR ANNUNCIATOR LIGHT. CREW RETURNED 
- [SDR TSAA0649012](https://openairdocs.org/sdr/TSAA0649012), Feb 11, 2006: SPEED SWITCH. FAILED. FLIGHT 922 HNL OGG- APU OVER-SPEED INDICATION ILLUMINATED AND THE APU AUTO SHUT-DOWN. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 3-
- [SDR TSAA0527019](https://openairdocs.org/sdr/TSAA0527019), Apr 20, 2005: SENSOR. FAILED. NON-ETOPS CARGO FLIGHT 913, HNL-LIH: AFTER TAKEOFF, THE STICK-SHAKER ENGAGED AND REMAINED ON UNTIL LANDING. RETURNED TO HNL. REMOVED AND REPLACED AOA SENSOR VAN
- [SDR TSAA0471076](https://openairdocs.org/sdr/TSAA0471076), Nov 11, 2004: LINE. OBSTRUCTED. FLT 840, NR 2 ENGINE PUTTING OUT LESS POWER THAN THE NR 1 ENGINE AT 1.89 EPR. SUSPECT NR 2 PT2 PROBE. REMOVED DEBRIS FROM THE PT2 SENSE TUBE BETWEEN THE ENGINE 
- [SDR TSAA0429054](https://openairdocs.org/sdr/TSAA0429054), Jul 16, 2004: PUMP. FAILED. HYDRAULIC SYSTEM FAILED. TURNED TO HNL. REMOVE AND REPLACE NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-11-32. LEAK AND OPS CHECK GOOD. REMOVE AND REPLACE NR 1 AND NR 
- [SDR TSAA0352107](https://openairdocs.org/sdr/TSAA0352107), Apr 27, 2003: SKIN. CORRODED. REMOVED DAMAGED AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR DOUBLER FROM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED DOUBLER PER FIGUR
- [SDR TSAA0352106](https://openairdocs.org/sdr/TSAA0352106), Apr 27, 2003: DOOR FRAME. CRACKED. REMOVED DAMAGED INBOARD DORR FRAME AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED AN ANGLE DOUBLER FROM .063 INCH 2024-T3 CLAD MATERIAL. ALODINED AND PRIMED A
- [SDR TSAA0233256](https://openairdocs.org/sdr/TSAA0233256), Dec 20, 2002: BATTERY PACK. INOPERATIVE. REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0233219](https://openairdocs.org/sdr/TSAA0233219), Oct 29, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 3 AND NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0234226](https://openairdocs.org/sdr/TSAA0234226), Oct 22, 2002: INDICATOR. FAULTY. PRIOR TO TAXI, THE CREW NOTICED A STRONG SMELL OF ELECTRIC FUMES FOLLOWED BY SMOKE IN COCKPIT. THE AIRCRAFT WAS SECURED FOR MAINTENANCE. MAINTENANCE REMOVED AND
- [SDR TSAA0277212](https://openairdocs.org/sdr/TSAA0277212), Oct 17, 2002: LINE. CONTAMINATED. ON TAKEOFF, THE NR 2 ENGINE WAS AT W.01 EPR, N1-80 PERCENT, EGT-400 DEGREES C, N2-82 PERCENT WITH FUEL FLOW AT 4000 LBS. THE AIRCRAFT RETURNED AND LANDED, WITH 
- [SDR TSAA0229193](https://openairdocs.org/sdr/TSAA0229193), Oct 14, 2002: RELIEF VALVE. DIRTY. AT THE TOP OF CLIMB WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE THE NR 2 ENGINE MADE A LOUD BANG LIKE A COMPRESSOR STALL. THE AIRCRAFT CONTINUED THE APPROA
- [SDR TSAA0275194](https://openairdocs.org/sdr/TSAA0275194), Sep 5, 2002: BLEED VALVE. MALFUNCTIONED. THE NR 2 ENGINE COMPRESSOR STALLED WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE AT TOP OF DECENT. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED UNEVENTFULL
- [SDR TSAA0233135](https://openairdocs.org/sdr/TSAA0233135), May 13, 2002: BATTERY PACK. DISCHARGED. REPLACED LEFT OVERWING IDENT EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233118](https://openairdocs.org/sdr/TSAA0233118), Apr 18, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0252092](https://openairdocs.org/sdr/TSAA0252092), Mar 27, 2002: GUIDE. OUT OF ADJUST. FLT 46 - HNL-ITO - FORWARD ENTRY DOOR LIGHT CAME ON DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBL
- [SDR TSAA0251083](https://openairdocs.org/sdr/TSAA0251083), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 26 LEFT UPP
- [SDR TSAA0251066](https://openairdocs.org/sdr/TSAA0251066), Feb 26, 2002: BULKHEAD. CORRODED. REMOVED CORROSION AT 1016 SKIN BULKHEAD AND ATTACHING FRAME AFT SIDE OF BULKHEAD BETWEEN LBL 5 TO RBL 5 IAW SRM 53-10-1 FIGURE 1 DETAIL 16. CUT OUT ACCESS HOLE 
- [SDR TSAA0251075](https://openairdocs.org/sdr/TSAA0251075), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 10 RT AT BS 500B PLUS 10 UPPER FORWARD CORNER HOLE NR 8. T
- [SDR TSAA0251076](https://openairdocs.org/sdr/TSAA0251076), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10, BS 4200 PLUS 10 AND BS 500 PLUS 10 ON WINDOW NR
- [SDR TSAA0251077](https://openairdocs.org/sdr/TSAA0251077), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 1 RIGHT UPPER FORWARD CORNER HOLE N
- [SDR TSAA0251078](https://openairdocs.org/sdr/TSAA0251078), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 2 RIGHT UPPER FORWARD CORNER HOLE N
- [SDR TSAA0251079](https://openairdocs.org/sdr/TSAA0251079), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S14L BS 727 PLUS 10 ON WINDOW NR 20 LEFT LOWER FORWARD HOLE NR 9. TR
- [SDR TSAA0251080](https://openairdocs.org/sdr/TSAA0251080), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10L BS 827 PLUS 10 ON WINDOW NR 24 LEFT UPPER AFT HOLES NR 8 AND NR
- [SDR TSAA0251081](https://openairdocs.org/sdr/TSAA0251081), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 25 LEFT UPP
- [SDR TSAA0251082](https://openairdocs.org/sdr/TSAA0251082), Feb 26, 2002: SKIN. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R AND S14R ON WINDOW NR 24 RT UPPER AFT HOLE NR 8. TRIMMED OUT HO
- [SDR TSAA0251067](https://openairdocs.org/sdr/TSAA0251067), Feb 26, 2002: FLOORBEAM. CORRODED. FOUND CORROSION ON THE EXISTING UPPER FLANGE FLOORBEAM REPAIR AT STATION 1016, WL 208 BBI 0 TO LBL 15. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIG
- [SDR TSAA0251069](https://openairdocs.org/sdr/TSAA0251069), Feb 26, 2002: KEELBEAM. CORRODED. FOUND CORROSION ON THE KEEL BEAM ON RIGHT LOWER FLANGE IN RIGHT AC BAY AT STATION 557 TO STATION 567, STATION 584 AND STATION 608. BLENDOUT THE CORROSION THEN F
- [SDR TSAA0255063](https://openairdocs.org/sdr/TSAA0255063), Feb 26, 2002: SPAR. CORRODED. FOUND CORROSION ON LEFT REAR SPAR CHORD 6 INCHES UP FROM VERTICAL STABILIZER ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPL
- [SDR TSAA0255064](https://openairdocs.org/sdr/TSAA0255064), Feb 26, 2002: SPAR. CORRODED. FOUND CORROSION ON LEFT REAR SPAR CHORD 46 INCHES UP FROM VERTICAL STABILIZER FIN BETWEEN STATION 99.5 AND 108.7 ATTACH LUG. BLENDED OUT THE CORROSION AND INSTA
- [SDR TSAA0251074](https://openairdocs.org/sdr/TSAA0251074), Feb 26, 2002: FLOOR SUPPORT. CORRODED. IDENTIFIED CORROSION ON FLOOR SUPPORT DIAGONAL LEFT BETWEEN STATION 1006 AND STATION 1016 LBL 5. REMOVED CORROSION IAW SRM 53-10-1 DETAIL I, FABRICATED AND INST
- [SDR TSAA0251068](https://openairdocs.org/sdr/TSAA0251068), Feb 26, 2002: KEELBEAM. CORRODED. FOUND CORROSION ON THE KEEL BEAM LOWER CHORD. CONFIRMED CORROSION REMOVED AND NO EVIDENCE OF CRACKS USING HFEC METHOD. REPAIR COMPLETED IAW ECO 3269. AIRCRAFT R
- [SDR TSAA0251084](https://openairdocs.org/sdr/TSAA0251084), Feb 26, 2002: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R ON WINDOW NR 26 RIGHT LOWER FORWARD HOLE NR 10. TRIMMED OUT HOL
- [SDR TSAA0251085](https://openairdocs.org/sdr/TSAA0251085), Feb 26, 2002: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R AND S14R ON WINDOW NR 26 RIGHT UPPER AFT HOLES NR 9 AND NR 10.
- [SDR TSAA0251086](https://openairdocs.org/sdr/TSAA0251086), Feb 26, 2002: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R BS 867 PLUS 10 ON WINDOW NR 29 RIGHT UPPER AFT HOLE NR 8. TRIM
- [SDR TSAA0251087](https://openairdocs.org/sdr/TSAA0251087), Feb 26, 2002: WINDOW FRAME. CRACKED. PEFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S-14R BS 420 ONWINDOW NR 4 RIGHT LOWER AFT CORNER HOLE NR 8. TRIMMED 
- [SDR TSAA0251088](https://openairdocs.org/sdr/TSAA0251088), Feb 26, 2002: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 5 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES 
- [SDR TSAA0251089](https://openairdocs.org/sdr/TSAA0251089), Feb 26, 2002: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 6 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES 
- [SDR TSAA0251090](https://openairdocs.org/sdr/TSAA0251090), Feb 26, 2002: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATION ON WINDOW NR 8 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OU
- [SDR TSAA0251091](https://openairdocs.org/sdr/TSAA0251091), Feb 26, 2002: STRINGER. CRACKED. FOUND CRACKES ON STRINGER 6L AND 7L FORWARD LAV SIDEWALL AREA. TRIMMED OUT DAMAGED PORTIONS OF INTERCOSTAL IAW SRM 51-40-3 FIGURE 1. VERIFIED NO FURTHER CRACKS 
- [SDR TSAA0251094](https://openairdocs.org/sdr/TSAA0251094), Feb 26, 2002: RIB. CRACKED. FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CRACKS ON VARIOUS SUPPORT RIBS LISTED FROM INBOARD TO OUTBOARD NR 2, 3, 4, 5, 6, 7, AND 8. CUT AND REMOVED PO
- [SDR TSAA0251095](https://openairdocs.org/sdr/TSAA0251095), Feb 26, 2002: STRINGER. DAMAGED. DAMAGED STRINGER BETWEEN FS 1040 AND FS 1064 STRINGER 27L. REMOVED DAMAGED SECTION IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR DOUBLER USING .040 INCH THICK 202
- [SDR TSAA0133170](https://openairdocs.org/sdr/TSAA0133170), Dec 1, 2001: BATTERY PACK. DISCHARGED. REPLACED AFT ENTRY EMERGENCY IDENT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0124097](https://openairdocs.org/sdr/TSAA0124097), Jul 27, 2001: CIRCUIT BREAKER. FLT 242 - LIH-OGG - THE CREW NOTICED A STRONG ELECTRICAL SMELL COMING FROM THE CENTER OF THE CABIN DURING DESCENT. SMELL DISSIPATED AFTER LANDING. MAUI MAINTENA
- [SDR TSAA0133093](https://openairdocs.org/sdr/TSAA0133093), Jul 25, 2001: BATTERY PACK. INOPERATIVE. REPLACED AFT SERVICE DOOR IDENT POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133081](https://openairdocs.org/sdr/TSAA0133081), Jul 7, 2001: BATTERY PACK. INOPERATIVE. REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

All 147: https://openairdocs.org/deregistered/N816AL-2008-07-09/reports.md

## Other aircraft with N816AL

- [Registered now](https://openairdocs.org/aircraft/N816AL): Zipline International P2 ZIP, S/N 18736P22572

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