# N808AL: 1985 Boeing 737-2T4, registration cancelled 2008-06-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 16, 2008
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-2T4](https://openairdocs.org/model/boeing-737-2t4) (registry code 1384492)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 23445
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 26, 1994
- Certificate issued: April 29, 2008
- Last registry action: April 29, 2008
- Mode S code: AAFFA0
- Owner when cancelled: [Palm Capital LLC](https://openairdocs.org/faa-owner/PALM%20CAPITAL%20LLC)
- Location: [Hopkinton, MA](https://openairdocs.org/faa-place/MA/Hopkinton)
- Owner type: Corporation
- Owner's area on the map: 42.2241° N, 71.5405° W: Placed by OpenAirDocs at the center of ZIP code 01748, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N808AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=808AL
- Page: https://openairdocs.org/deregistered/N808AL-2008-06-16

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 737-2T4: https://openairdocs.org/model/boeing-737-2t4.md

## Service difficulty reports (140, newest 50)

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

- [SDR TSAA0832009](https://openairdocs.org/sdr/TSAA0832009), Feb 18, 2008: VALVE. LEAKING. NON-ETOPS FLIGHT 88 HNL-KOA, DURING TAKEOFF, THE CREW NOTED THE HYDRAULIC QUANTITY DROP FROM 3 GALLONS TO LESS THAN 1 GALLON. THE CREW ELECTED TO ABORT THE TAKE
- [SDR TSAA0653101](https://openairdocs.org/sdr/TSAA0653101), Nov 13, 2006: DOOR FRAME. DAMAGED. AFT CARGO DOOR CUT-OUT DAMAGED (LOWER AFT CORNER). ALOHA ECO 3622 ISSUED.
- [SDR TSAA0624080](https://openairdocs.org/sdr/TSAA0624080), Sep 29, 2006: SWITCH. FAILED. NON-ETOPS FLIGHT 206 HNL OGG. ON TAKEOFF THE CONFIGURATION WARNING ALARM SOUNDED WHEN THROTTLES WERE ADVANCED. CREW ABORTED TAKEOFF AT 15 KTS. AIRCRAFT WAS CONF
- [SDR TSAA0678059](https://openairdocs.org/sdr/TSAA0678059), Jul 29, 2006: WARNING LIGHT. ILLUMINATED. NON-ETOPS FLT 224 LIH-HNL. ON TAKE OF ROLL, CREW NOTED THE NR 2 ENGINE THRUST REVERSER UNLOCKED LIGHT ON WITH ALL OTHER ENGINE INDICATIONS NORMAL. CREW ABORTED 
- [SDR TSAA0678054](https://openairdocs.org/sdr/TSAA0678054), Jul 15, 2006: LATCH. LACK OF LUBE. ON TAKEOFF ABOVE 80 KNOTS AND CLIMB, CREW NOTED NR 2 THRUST REVERSER UNLOCKED LIGHT ILLUMINATED INTERMITTENTLY. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. M
- [SDR TSAA0653046](https://openairdocs.org/sdr/TSAA0653046), Jun 12, 2006: SKIN PANEL. CRACKED. 2.25 INCH SKIN CRACK FOUND LEFT SIDE OF FUSELAGE BS 786 JUST ABOVE STRINGER 24L. MAINTENANCE REPAIRED WITH APPROXIMATELY 11 IN X 15 IN EXTERNAL SKIN PATCH, FABR
- [SDR TSAA0653045](https://openairdocs.org/sdr/TSAA0653045), Jun 12, 2006: SKIN PANEL. CRACKED. 2.5 INCH SKIN CRACK FOUND RIGHT SIDE OF FUSELAGE AT BS 941 JUST ABOVE STRINGER 24R. MAINTENANCE REMOVED TWO EXISTING REPAIRS AND REPAIRED WITH 36 IN X 46 IN EXT
- [SDR TSAA0653042](https://openairdocs.org/sdr/TSAA0653042), Jun 11, 2006: SKIN PANEL. CRACKED. 3 INCH CRACK FOUND RT SIDE OF FUSELAGE SKIN AFT OF AFT CARGO DOOR CUTOUT AS BS 867 STRINGER 23R. MAINTENANCE REMOVED ONE EXISTING REPAIR AND REPAIRED WITH APPRO
- [SDR TSAA0627016](https://openairdocs.org/sdr/TSAA0627016), Mar 11, 2006: SLAT. BIRD STRIKE. ON CLIMB AT 1000 FT AIRCRAFT STRUCK A LARGE BIRD AT NR 1 LEADING EDGE SLAT. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH FORM M-
- [SDR TSAA0653010](https://openairdocs.org/sdr/TSAA0653010), Feb 8, 2006: SKIN. CRACKED. FOUND 3 CRACKS AROUND CENTER UPSTOP OF NR 2 SLAT; WING LEADING EDGE. BETWEEN LEFT WS 453 AND WS 479. L/E SKIN FABRICATED, TRIMMED, CLEANED, ALODINED, PRIMED, AN
- [SDR TSAA0672008](https://openairdocs.org/sdr/TSAA0672008), Feb 2, 2006: ENGINE. DEFECTIVE. OGG-HNL: ON TAKEOFF NR 2 ENGINE EGT ROSE TO 650 DEGREES CELSIUS. ENGINE THROTTLED BACK UNTIL EGT WAS WITHIN LIMITS AND AIRCRAFT RETURNED TO FIELD WITHOUT INCIDE
- [SDR TSAA0553057](https://openairdocs.org/sdr/TSAA0553057), Dec 13, 2005: SKIN PANEL. CRACKED. A 3.5 INCH CRACK FOUND RIGHT SIDE OF FUSELAGE SKIN AFT OF AFT CARGO DOOR AT BS 927 STRINGER 23R. CUT OUT CRACK .040 INCH INSURANCE CUT. PERFORMED HFEC AROUND CU
- [SDR TSAA0527048](https://openairdocs.org/sdr/TSAA0527048), Oct 19, 2005: ACTUATOR. LEAKING. CREW HAD INDICATION OF HYDRAULIC SYSTEM A, DROP IN PRESSURE. CREW DECLARED AN EMERGENCY AND WERE ABLE TO DEPLOY THE LANDING GEAR. LANDED WITHOUT FURTHER INCIDEN
- [SDR TSAA0527047](https://openairdocs.org/sdr/TSAA0527047), Oct 12, 2005: ACTUATOR. FAILED. COOPESA TO BROWNSVILLE TX FERRY FLIGHT 808. NR 5 SLAT DID NOT RETRACT. LEFT WING TO BODY OVERHEAT INDICATION. THE CREW RETURNED TO COOPESA WITHOUT FURTHER INCID
- [SDR TSAA0557027](https://openairdocs.org/sdr/TSAA0557027), Jul 18, 2005: SLAT. INFLT SEPARATION. AFTER ARRIVAL IN LIH A PASSENGER ADVISED THE FLIGHT ATTENDANT THAT PART OF THE WING SEPARATED IN FLIGHT. CAPTAIN THEN OBSERVED A SECTION OF THE NUMBER THREE LEA
- [SDR TSAA0529014](https://openairdocs.org/sdr/TSAA0529014), Mar 8, 2005: SEAL. LEAKING. NON-ETOPS FLT 104, HNL-KOA: LOST A SYSTEM HYDRAULICS DURING CLIMB-OUT. RETURNED TO HNL. FLAPS WOULD NOT EXTEND TO 15 USING ALTERNATE FLAP SYSTEM. MAINTENANCE RE
- [SDR TSAA0529013](https://openairdocs.org/sdr/TSAA0529013), Mar 8, 2005: SEAL. LEAKING. NON-ETOPS FLT 104, HNL-KOA: LOST A SYSTEM HYDRAULICS DURING CLIMB-OUT. RETURNED TO HNL. FLAPS WOULD NOT EXTEND TO 15 USING ALTERNATE FLAP SYSTEM. MAINTENANCE RE
- [SDR TSAA0529012](https://openairdocs.org/sdr/TSAA0529012), Mar 7, 2005: LINE. LEAKING. LOST A SYSTEM HYDRAULICS ON SHORT FINAL. MAINTENANCE MET THE AIRCRAFT ON THE RUNWAY. MAINTENANCE REPLACED THE NOSE GEAR DOWN ACTUATOR LINE PER AMM 32-3-11. SERV
- [SDR TSAA0529008](https://openairdocs.org/sdr/TSAA0529008), Feb 23, 2005: LINE. LEAKING. FLT 89, KOA-HNL: A SYSTEM HYDRAULICS FAILED ON SHORT FINAL. LEFT MAIN GEAR LEAKING. FOUND THE LEFT HAND MAIN LANDING GEAR ACTUATOR UP PRESSURE HOSE ASSEMBLY LEA
- [SDR TSAA0432083](https://openairdocs.org/sdr/TSAA0432083), Dec 17, 2004: DOWNLOCK SENSOR. DEFECTIVE. NON-ETOPS FLT. 82, HNL-KOA - DURING DESCENT, LEFT GEAR RED LIGHT WAS ON WITH THE LANDING GEAR HANDLE IN THE DOWN POSITION. FLEW BY TOWER TO VERIFY GEAR DOWN. UN
- [SDR TSAA0427065](https://openairdocs.org/sdr/TSAA0427065), Sep 7, 2004: INDICATOR. FAILED. NON-ETOPS FLIGHT 110, HNL-OGG: FLAPS DID NOT DEPLOY DURING NORMAL FLAP EXTENSION, USED ALTERNATE MODE TO DEPLOY LEADING EDGE FLAPS. THE TRAILING EDGE FLAPS WERE
- [SDR TSAA0456033](https://openairdocs.org/sdr/TSAA0456033), Mar 15, 2004: WINDSHIELD. FAILED. CAPTAIN'S NR 1 WINDOW OUTER PANE CRACKED. RETURNED TO HNL. REMOVED AND REPLACED CAPTAIN'S NR 1 WINDOW IAW AMM 56-11-11, PAGES 401-411 AND 580. OPS CHECK GOOD. A
- [SDR TSAA0475030](https://openairdocs.org/sdr/TSAA0475030), Feb 20, 2004: DUCT. FAILED. FLT 286 - LIH-HNL - PASSING 10,000 FEET ON CLIMB-OUT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. ALL OTHER ENGINE INSTRUMENTS IN GREEN. RETARDED NR 1 ENGINE AN
- [SDR TSAA0433024](https://openairdocs.org/sdr/TSAA0433024), Jan 16, 2004: BATTERY PACK. INOPERATIVE. REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0453003](https://openairdocs.org/sdr/TSAA0453003), Dec 17, 2003: SKIN. CRACKED. TRIMMED OUT THE SKIN CRACK. VERIFIED HFEC CUTOUT AND ROTARY PROBE INSPECTION OF LAP SPLICE FASTENER HOLES. FABRICATED AND INSTALLED STRUCTURAL FILLERS, A DOUBLE
- [SDR TSAA0326199](https://openairdocs.org/sdr/TSAA0326199), Dec 9, 2003: FIRE DETECTOR. FAILED. APPROXIMATELY 25 MILES FROM HNL, A WHEEL WELL FIRE LIGHT CAME ON. DEFER IAW MEL 26-4, SYSTEM DEACTIVATED IAW MEL. PLACARDS INSTALLED. REMOVED AND REPLACED WHEEL
- [SDR TSAA0333204](https://openairdocs.org/sdr/TSAA0333204), Nov 29, 2003: BATTERY PACK. DISCHARGED. REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333203](https://openairdocs.org/sdr/TSAA0333203), Nov 29, 2003: BATTERY PACK. DISCHARGED. REPLACED RIGHT OVERWING IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333202](https://openairdocs.org/sdr/TSAA0333202), Nov 29, 2003: BATTERY PACK. DISCHARGED. REPLACED LT OVERWING IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333020](https://openairdocs.org/sdr/TSAA0333020), Feb 2, 2003: BATTERY PACK. INOPERATIVE. REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333019](https://openairdocs.org/sdr/TSAA0333019), Jan 31, 2003: BATTERY PACK. INOPERATIVE. REPLACED FORWARD PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333018](https://openairdocs.org/sdr/TSAA0333018), Jan 31, 2003: BATTERY PACK. INOPERATIVE. REPLACED AFT PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0353035](https://openairdocs.org/sdr/TSAA0353035), Jan 18, 2003: KEELBEAM. CORRODED. TRIMMED OUT FUSELAGE SKIN BETWEEN KEEL BEAMS AND AFT OF BS 727. REMOVED AND REPLACED LEFT AND RIGHT KEEL BEAM FROM BS 500 TO BS 727 PLUS 16. VISUALLY AND HFEC I
- [SDR TSAA0353027](https://openairdocs.org/sdr/TSAA0353027), Jan 18, 2003: SKIN. DAMAGED. REMOVED ALL EXISTING REPAIRS COMMON TO THE LAP JOINT AREAS. ACCOMPLISHED A HFEC OF FASTENERS HOLES TO ASSURE CRACK FREE CONDITION. FABRICATED TWO TAPERED FILLER
- [SDR TSAA0351036](https://openairdocs.org/sdr/TSAA0351036), Jan 15, 2003: SPLICE. CORRODED. TRIMMED WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO LBL 24.5. FABRICATED NEW PERSSURE WEB SECTION AND STEP FILLERS FOR TRANSVERSE I BEAM. FABRICATED FOUR DOU
- [SDR TSAA0355034](https://openairdocs.org/sdr/TSAA0355034), Jan 15, 2003: FITTING. CORRODED. THE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER FITTING ASSEMBLY FAIL/SAFE AND LOWER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 7
- [SDR TSAA0351031](https://openairdocs.org/sdr/TSAA0351031), Jan 15, 2003: SPLICE. CORRODED. TRIMMED LEFT WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO LBL 24.5. FABRICATED NEW PRESSURE WEB SECTION AND STEP FILLERS FOR TRANSVERSE I BEAM. FABRICATED FOU
- [SDR TSAA0351029](https://openairdocs.org/sdr/TSAA0351029), Jan 15, 2003: PRESSURE PANEL. CORRODED. FABRICATED NEW PRESSURE WEB REPAIR DOUBLER. ALODINED AND PRIMED ALL BARE ALUMINUM. FAY SURFACE SEAL INSTALLED REPAIR DOUBLER WITH BMS 5-95 AND FASTENERS IDENTIF
- [SDR TSAA0351030](https://openairdocs.org/sdr/TSAA0351030), Jan 15, 2003: WEB. CORRODED. TRIMMED RIGHT WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO RBL 70. FABRICATED NEW PRESSURE WEB SECTION, STIFFENERS AND FILLERS. SHOT PEENED, ALODINED AND PRIM
- [SDR TSAA0355032](https://openairdocs.org/sdr/TSAA0355032), Jan 15, 2003: FITTING. CRACKED. THE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR ATTACHMENT FITTING CLEVIS LUGS BUSHINGS REMOVED. EDDY CURRENT INSPECTED LUGS FOR CRACKS BEFORE AND AFTER
- [SDR TSAA0355033](https://openairdocs.org/sdr/TSAA0355033), Jan 14, 2003: FITTING. CORRODED. THE LEFT HORIZONTAL STABILIZER CENTER CENTER SECTION REAR SPAR UPPER FITTING ASSEMBLY UPPER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1
- [SDR TSAA0353026](https://openairdocs.org/sdr/TSAA0353026), Jan 11, 2003: SKIN. CANNING. TRIMMED OUT THE SKIN SNAP DAMAGE AND OIL-CANNING. VISUALLY INSPECTED FOR DISBONDING. FABRICATED AND INSTALLED THREE STRUCTURAL FILLERS, AND DOUBLER AND TEARSTRA
- [SDR TSAA0134180](https://openairdocs.org/sdr/TSAA0134180), Oct 14, 2002: GPS. FAILED. ENROUTE, THE NR 1 AND NR 2 GPS WERE UNABLE TO LOCK ON TO THE SATELLITE SIGNAL. THE AIRCRAFT RETURNED FOR MAINTENANCE WITH NO FURTHER INCIDENT. REMOVED AND REPLA
- [SDR TSAA0233207](https://openairdocs.org/sdr/TSAA0233207), Oct 11, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED, OK. AIRCRAFT RETURNED TO SERVICE. (TSAA80003325)
- [SDR TSAA0133168](https://openairdocs.org/sdr/TSAA0133168), Dec 2, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133167](https://openairdocs.org/sdr/TSAA0133167), Nov 30, 2001: LIGHT. INOPERATIVE. REPLACED NR 2 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133166](https://openairdocs.org/sdr/TSAA0133166), Nov 29, 2001: BATTERY PACK. INOPERATIVE. REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 2001F00721](https://openairdocs.org/sdr/2001F00721), Nov 16, 2001: COUPLER. DEFECTIVE. FLT 351 - HNL-JON - DURING THE VERIFICATION PHASE OF FLIGHT AND CHECKING THE HF RADIO SYSTEM, THE NR 1 HF HAD NO TUNE AND THE TRANSMIT WAS INOPERATIVE. RETURNED
- [SDR TSAA0123113](https://openairdocs.org/sdr/TSAA0123113), Nov 16, 2001: TRANSCEIVER. MALFUNCTIONED. FLT 351 - HNL-JON - DURING THE VERIFICATION PHASE OF FLIGHT AND CHECKING THE HF RADIO SYSTEM, THE NR 1 HF HAD NO TUNE AND THE TRANSMIT WAS INOPERATIVE. RETURNED
- [SDR TSAA0133142](https://openairdocs.org/sdr/TSAA0133142), Oct 20, 2001: BATTERY PACK. DISCHARGED. REPLACED AFT OVERHEAD PATH EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

All 140: https://openairdocs.org/deregistered/N808AL-2008-06-16/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 20010307003689I](https://openairdocs.org/incident/20010307003689I), Mar 7, 2001: Boeing 7372T4 (N808AL), Lanai City, HI, Minor damage. (-23) After applying takeoff power and as the a/c accelerated to approx. 20 knots, a loud bang was heard from the no. 1 engine. Engine was secured and a/c…

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