# N810AL: 1988 Boeing 737-2Y5, registration cancelled 2009-01-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 26, 2009
- Exported to: Venezuela
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-2Y5](https://openairdocs.org/model/boeing-737-2y5) (registry code 1384554)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 24031
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Special flight permit
- Airworthiness date: March 31, 1995
- Certificate issued: October 22, 2008
- Last registry action: October 22, 2008
- Mode S code: AB0967
- Owner when cancelled: [Aviation Technologies Inc](https://openairdocs.org/faa-owner/AVIATION%20TECHNOLOGIES%20INC)
- Location: [Avoca, PA](https://openairdocs.org/faa-place/PA/Avoca)
- Owner type: Corporation
- Owner's area on the map: 41.3364° N, 75.7284° W: Placed by OpenAirDocs at the center of ZIP code 18641, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N810AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=810AL
- Page: https://openairdocs.org/deregistered/N810AL-2009-01-26

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 737-2Y5: https://openairdocs.org/model/boeing-737-2y5.md

## Service difficulty reports (76, newest 50)

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

- [SDR TSAA0732043](https://openairdocs.org/sdr/TSAA0732043), Jul 31, 2007: MODULE. FAILED. NON-ETOPS FLIGHT 221 OGG - HNL. WHEN THE CREW SELECTED THE LANDING GEAR TO UP, THE LT MAIN GEAR DOWN LIGHT TOOK A FEW SECONDS LONGER TO EXTINGUISH THAN THE OTHE
- [SDR TSAA0729040](https://openairdocs.org/sdr/TSAA0729040), Jul 7, 2007: HOSE. FAILED. FLIGHT 26 HNL-OGG - AFTER TAKEOFF FROM HNL, CREW NOTED LOSS OF SYSTEM A HYDRAULIC PRESSURE. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE TOWED THE
- [SDR TSAA0726029](https://openairdocs.org/sdr/TSAA0726029), May 31, 2007: FIRE DETECTOR. FAILED. FLIGHT 93 HNL-LIH - AFTER STARTING THE NR 1 ENGINE, THE CREW NOTED THE NR 1 ENGINE FIRE INDICATION LIGHT ILLUMINATED. CREW FOLLOWED THE QRH PROCEDURES: SHUT DOW
- [SDR TSAA0632057](https://openairdocs.org/sdr/TSAA0632057), Jul 24, 2006: WHEEL. SEPARATED. ON LANDING, CREW HEARD AN UNUSUAL (BUMP) NOISE WITH NORMAL LANDING. TAXI TO GATE WITHOUT FURTHER INCIDENT. CREW FOUND NR 1 MAIN LANDING GEAR WHEEL ASSEMBLY HAD 
- [SDR TSAA0651040](https://openairdocs.org/sdr/TSAA0651040), May 24, 2006: SPAR. CORRODED. HORIZONTAL STABILIZER RT REAR SPAR UPPER CHORD CORROSION (3 AREAS).
- [SDR TSAA0651039](https://openairdocs.org/sdr/TSAA0651039), May 24, 2006: SPAR. CORRODED. VERTICAL STABILIZER RIGHT T/E REAR SPAR CORROSION (3 AREAS).
- [SDR TSAA0653018](https://openairdocs.org/sdr/TSAA0653018), Mar 17, 2006: SKIN PANEL. CRACKED. A 2 INCH SKIN CRACK AT BS 929 STR 24L. A .04 INSURANCE MADE IAW SRM 53-30-3. RIVET PATTERN LAID OUT AND DRILLED AND MANUFACTURED REPAIR DOUBLER, TRIPLER, AND 2 
- [SDR TSAA0653017](https://openairdocs.org/sdr/TSAA0653017), Mar 11, 2006: SPAR. CORRODED. CORROSION ON UPPER & LOWER SURFACE OF FRONT SPAR LOWER CORD BETWEEN FSS 297 & FSS-306 AT SLAT NR 4. BLENDED INBOARD - OUTBOARD DIRECTION 10:1 DEPTH TO BLEND RAT
- [SDR TSAA0621007](https://openairdocs.org/sdr/TSAA0621007), Jan 27, 2006: FAN. DEFECTIVE. ON APPROACH THE PILOT SMELLED SMOKE AND AFTER LANDING THE SMELL GREW STRONGER. AIRPLANE TAXIED BACK TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED GASPER FA
- [SDR TSAA0653006](https://openairdocs.org/sdr/TSAA0653006), Jan 24, 2006: SKIN. CRACKED. A 4 INCH FUSELAGE SKIN CRACK BS 937 AT STRINGER 21L. MAINTENANCE REPAIRED WITH APPROXIMATELY 24 X 20 INCH SKIN PATCH, FABRICATED DOUBLER, TRIPLER, AND STRUCTURA
- [SDR TSAA0575031](https://openairdocs.org/sdr/TSAA0575031), Jul 20, 2005: BLEED VALVE. DEFECTIVE. ON TAKE-OFF NR 2 ENGINE COMPRESSOR STALL ON INITIAL RUN-UP FROM IDLE. R & R NR 2 ENG PRBC IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED PER P&W MM 72-00-00.
- [SDR TSAA0575029](https://openairdocs.org/sdr/TSAA0575029), Jul 12, 2005: BLEED VALVE. DEFECTIVE. RUNNING UP ENGINES FOR TAKE-OFF, GOT STEADY BANGING. RPM BARELY PAST IDLE. FLIGHT ATTENDANTS GUESS THE NR 2 ENGINE. TAKE-OFF ABORTED. R&R PRBC IAW MM 75-31-11 O
- [SDR TSAA0479019](https://openairdocs.org/sdr/TSAA0479019), Jan 16, 2004: ENGINE. LEAKING. FLT 224 - LIH-HNL - LOW OIL PRESSURE ILGHT ON NR 1 ENGINE ILLUMINATED. OIL PRESSURE DROPPED TO 20 PSI. FOLLOWED QRH AND SHUTDOWN THE NR 1 ENGINE. DECLARED EMERG
- [SDR TSAA0429001](https://openairdocs.org/sdr/TSAA0429001), Dec 30, 2003: LINE. FAILED. FLT 240 - HNL-OGG - ON GEAR RETRACTION 'A' SYSTEM HYDRAULIC ANNUNCIATOR LIGHT CAME ON. SYSTEM QUANTITY AT 1.5 GALLONS. RETURNED TO HNL. FOUND RIGHT MAIN GEAR UP
- [SDR TSAA0333205](https://openairdocs.org/sdr/TSAA0333205), Nov 29, 2003: BATTERY PACK. INOPERATIVE. REPLACED AFT ENTRY DOOR IDENT EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0353037](https://openairdocs.org/sdr/TSAA0353037), Feb 9, 2003: SKIN. CRACKED. NINE RIVETS ON STRINGER 16R SHOW SIGNS OF STRESS CRACKS EMANATING FROM THE FASTENER HOLES. REMOVED RIVETS, OVERSIZED HOLES BY 1/16, HFEC VERIFIED FASTENER HOLES
- [SDR TSAA0233228](https://openairdocs.org/sdr/TSAA0233228), Nov 8, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0233229](https://openairdocs.org/sdr/TSAA0233229), Nov 8, 2002: LIGHT. INOPERATIVE. REPLACED LT OVERWING IDENT LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253201](https://openairdocs.org/sdr/TSAA0253201), Oct 2, 2002: STRUCTURE. GOUGED. CUTOUT DAMAGE, PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. FABRICATED
- [SDR TSAA0253183](https://openairdocs.org/sdr/TSAA0253183), Jun 29, 2002: FRAME. CORRODED. AUXILIARY POWER UNIT COMPARTMENT CORRODED AT BS 1156 REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER FROM SRM, AIRCRAFT RETU
- [SDR TSAA0253152](https://openairdocs.org/sdr/TSAA0253152), Jun 17, 2002: SKIN. CRACKED. FOUND CRACK ON FUSELAGE SKIN, STRINGER 21L AT BS 985.5. TRIMMED OUT DAMAGED AREA AND VERIFIED USING HFEC METHOD NO DEFECTS NOTED. FABRICATED AND INSTALLED FILLE
- [SDR TSAA0253142](https://openairdocs.org/sdr/TSAA0253142), May 15, 2002: SKIN. CORRODED. FOUND CORROSION ON THE LEFT HAND OUTBOARD WING MAIN BOX UPPER SKIN AT WBL 71.24, STR 5, 7 AND WBL92.5 STR 1, 5. BLENDED OUT CORROSION AT A 10:1 RATIO MINIMUM PE
- [SDR TSAA0253141](https://openairdocs.org/sdr/TSAA0253141), May 13, 2002: SKIN. WORN. FOUND SKIN WORN THROUGH ON THE RIGHT LEADIN EDGE LOWER WING SKIN SURFACE AT FS 413. CUT OUT DAMAGED LEADING EDGE FILLER AND SKIN. FABRICATED REPAIR PARTS, ALODI
- [SDR TSAA0253134](https://openairdocs.org/sdr/TSAA0253134), May 13, 2002: PRESSURE PANEL. CORRODED. FOUND CORROSION ON NOSE LANDING GEAR BULKHEAD AT BS 227.8. CUT OUT CORROSION AND VERIFIED REMOVED BY VISUAL INSPECTION. FABRICATED CHORD AND REPAIR ANGLES. INST
- [SDR TSAA0251133](https://openairdocs.org/sdr/TSAA0251133), May 10, 2002: SKIN. GOUGED. FOUND GOUGE IN SKIN AT STRINGER 16L AT BS 843. BLENDED OUT DAMAGED AREA TO A SMOOTH SURFACE. VERIFIED NO CRACKS USING HFEC. REPAIR COMPLETED IAW SRM. AIRCRAFT R
- [SDR TSAA0251132](https://openairdocs.org/sdr/TSAA0251132), May 10, 2002: BRACKET. CHAFED. FOUND NR 8 FLAP JACKSCREW TRAILING EDGE MOUNT BRACKET CHAFFING AT FLAP TRACK FAIRING. BLENDED OUT DAMAGED AREA. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0251130](https://openairdocs.org/sdr/TSAA0251130), May 10, 2002: SLAT. CORRODED. FOUND CORROSION ON THE RIGHT WING AFT OF THE NR 5 SLAT FITTING. BLENDED OUT CORROSION. FABRICATED AND INSTALLED PARTS. REWORK COMPLETED. AIRCRAFT RETURNED TO SE
- [SDR TSAA0253146](https://openairdocs.org/sdr/TSAA0253146), Apr 25, 2002: SKIN. WORN. RIGHT WING LEADING EDGE LOWER SKIN AT FSS 413 WORN BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER, SPLICE PLATE AND DOUBLER. AIRCRAFT RETU
- [SDR TSAA0253125](https://openairdocs.org/sdr/TSAA0253125), Apr 25, 2002: SPAR. CORRODED. FOUND CORROSION ON RIGHT WING FRONT SPAR, LOWER CHORD FORWARD HORIZONTAL FLANGE FORWARD LIP AT FSS 413. REMOVED CORROSION BY BLEND OUT. HFEC AREA TO ENSURE FREE
- [SDR TSAA0253127](https://openairdocs.org/sdr/TSAA0253127), Apr 23, 2002: BULKHEAD. CRACKED. FOUND CRACK ON THE BLK 178 AT WL 212, RBL 5.7 DURING INSPECTION. CUTOUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED 
- [SDR TSAA0253126](https://openairdocs.org/sdr/TSAA0253126), Apr 23, 2002: BULKHEAD. CRACKED. FOUND CRACK ON THE BLK 178 AT WL 212, LBL 5.7 DURING INSPECTION PER ECO 3137. CUT OUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFE
- [SDR TSAA0253128](https://openairdocs.org/sdr/TSAA0253128), Apr 23, 2002: STRINGER. DENTED. FOUND DENT ACROSS STRINGER 15L AT BS 900. CUTOUT STRINGER SEGMENT AT BS 900. REMOVED THE SEGMENT OF THE STRINGER AFT TO THE PRODUCTION SPLICE. FABRICATED NEW ST
- [SDR TSAA0253131](https://openairdocs.org/sdr/TSAA0253131), Apr 23, 2002: FLOORBEAM. CRACKED. FOUND CRACKS AT BL 0 FLOOR BEAM AT BS 663 AND BETWEEN BS 700-717 WEB. REMOVED AND DISCARDED A SECTION OF THE WEB AND DOUBLER CONTAINING THE CRACKS. FABRICATED A
- [SDR TSAA0253006](https://openairdocs.org/sdr/TSAA0253006), Jan 1, 2002: FRAME. CORRODED. REMOVED CORROSION DAMAGE ON STRINGER 5R UPPER CHORD AT BS 1093. REMOVED FORWARD PORTION OF DAMAGED CHORD. FABRICATED REPLACEMENT CHORD AND SPLICE ANGLES AND INS
- [SDR TSAA0133092](https://openairdocs.org/sdr/TSAA0133092), Jul 20, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0132070](https://openairdocs.org/sdr/TSAA0132070), Jun 13, 2001: DOWNLOCK SENSOR. FAILED. INBOUND TO HNL FROM LIH - REPORTED TO MAINTENANCE CONTROL OF THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ON IN-FLIGHT. CAPTAIN PERFORMED FLYBY FOR TOWER TO CHECK G
- [SDR TSAA0033216](https://openairdocs.org/sdr/TSAA0033216), Oct 16, 2000: BATTERY. INOPERATIVE. REPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA0053198](https://openairdocs.org/sdr/TSAA0053198), Jul 30, 2000: SKIN. DENTED. REPAIRED A DENT AT LEFT FUSELAGE BS 360-380 STRINGER 17L, AFT OF FORWARD ENTRY DOOR. CUT OUT DAMAGED AREA PERFORMED HFEC INSPECTION. FABRICATED AND INSTALLED DO
- [SDR TSAA0033182](https://openairdocs.org/sdr/TSAA0033182), Jul 30, 2000: BATTERY. INOPERATIVE. REPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0073139](https://openairdocs.org/sdr/TSAA0073139), May 29, 2000: FCU. FAILED. FLT 71 - OGG-HNL - THE NR 1 ENGINE RPM GAGE IMMEDIATELY DECREASED TO ZERO THE MOMENT THE AIRCRAFT LIFTED OFF THE RUNWAY. DID NOT ATTEMPT A RESTART, ACCOMPLISHED
- [SDR TSAA9933479](https://openairdocs.org/sdr/TSAA9933479), Nov 9, 1999: BATTERY. DISCHARGED. REPLACED NR 3, 4, 5, AND 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 99ZZZM807](https://openairdocs.org/sdr/99ZZZM807), Oct 26, 1999: SENSOR. INTERMITTENT. FLT 101 - OGG-HNL - LEFT MAIN GEAR RED UNSAFE GEAR LIGHT COMES ON INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED UPLOCK SENSOR LEFT GEAR PER MM 32-61-21 AND
- [SDR TSAA9933408](https://openairdocs.org/sdr/TSAA9933408), Aug 21, 1999: BATTERY PACK. DISCHARGED. REPLACED NR 3 EMERGENCY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933368](https://openairdocs.org/sdr/TSAA9933368), Jul 31, 1999: BATTERY PACK. DISCHARGED. REPLACED NR 5 EMERGENCY FLOOR BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933362](https://openairdocs.org/sdr/TSAA9933362), Jul 25, 1999: BATTERY PACK. DISCHARGED. REPLACED NR 4 EMERGENCY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9921300](https://openairdocs.org/sdr/TSAA9921300), Jul 6, 1999: RELIEF VALVE. FAILED. HNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED, BUT DIDN'T CONTROL CABIN. LATER, MANUAL AND STANDB
- [SDR TSAA9921292](https://openairdocs.org/sdr/TSAA9921292), Jul 6, 1999: CONTROLLER. FAILED. HNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED BUT DID NOT CONTROL CABIN. LATER, MANUAL AND STANDB
- [SDR TSAA9933285](https://openairdocs.org/sdr/TSAA9933285), Jun 8, 1999: BATTERY. DISCHARGED. REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933246](https://openairdocs.org/sdr/TSAA9933246), May 31, 1999: BATTERY. DISCHARGED. REPLACED NR 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK FOR LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933223](https://openairdocs.org/sdr/TSAA9933223), Apr 19, 1999: BATTERY. DISCHARGED. REPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT POWER SUPPLY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)

All 76: https://openairdocs.org/deregistered/N810AL-2009-01-26/reports.md

## Other aircraft with N810AL

- [Registered now](https://openairdocs.org/aircraft/N810AL): Zipline International P2 ZIP, S/N 18736P22632

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