# N807AL: 1985 Boeing 737-2T4, registration cancelled 2008-07-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 30, 2008
- Status when cancelled: Sale reported
- Airframe: [Boeing 737-2T4](https://openairdocs.org/model/boeing-737-2t4) (registry code 1384492)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 23443
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 6, 1994
- Last registry action: July 30, 2008
- Mode S code: AAFBE9
- Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie)
- Owner type: Individual
- Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N807AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807AL
- Page: https://openairdocs.org/deregistered/N807AL-2008-07-30

From the FAA registry file of October 28, 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 (104, newest 50)

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

- [SDR TSAA0631102](https://openairdocs.org/sdr/TSAA0631102), Nov 18, 2006: LEVER. LACK OF LUBE. ON TAKEOFF, THE CREW NOTED THE TAKEOFF CONFIGURATION WARNING ALARM AND PERFORMED A LOW SPEED ABORTED TAKEOFF. CREW RECYCLED THE SPEED BRAKE AND THE ALARM CLEARE
- [SDR TSAA0663089](https://openairdocs.org/sdr/TSAA0663089), Oct 18, 2006: SKIN PANEL. CRACKED. A .5 INCH CRACK FOUND LT SIDE OF FUSELAGE SKIN AT BS 270 STRINGER 16L. MAINTENANCE REPAIRED WITH APPROXIMATELY 9"X14" EXTERNAL SKIN PTACH FABRICATED DOUBLER AND
- [SDR TSAA0653076](https://openairdocs.org/sdr/TSAA0653076), Sep 20, 2006: BULKHEAD. CRACKED. 3 CRACKED HOLES COMMON TO BS 178 BULKHEAD WEB BETWEEN WL 240 AND WL 230.5
- [SDR TSAA0653068](https://openairdocs.org/sdr/TSAA0653068), Aug 23, 2006: DOOR FRAME. CRACKED. CRACK NOTED ON FWD CARGO DOOR CUTOUT, AFT LOWER CORNER UNDER DOOR STOP.
- [SDR TSAA0653030](https://openairdocs.org/sdr/TSAA0653030), Apr 6, 2006: BULKHEAD. CRACKED. THREE CRACKS AROUND BS 1016 AFT PRESSURE BULKHEAD GORE WEBS NEAR DOME CAP. WEB SPLICE AND REPAIR DOUBLERS COMPLETED IAW ALOHA'S ECO 3567. HFEC COMPLIED IAW NDT 
- [SDR TSAA0653028](https://openairdocs.org/sdr/TSAA0653028), Apr 4, 2006: SKIN. CRACKED. APPROXIMATE 2 INCH SKIN CRACK AT BS 747 +10 STR 24L. REPAIR COMPLETED IAW SRM 53-30-3 FIG 48. REPAIR SIZE APPROX 15 X 11 INCHES. INSURANCE CUT MADE .040 INCH. D
- [SDR TSAA0627026](https://openairdocs.org/sdr/TSAA0627026), Mar 27, 2006: INDICATION SYS. MALFUNCTIONED. ON APPROACH TO KOA, CREW NOTED TRAILING EDGE FLAP INDICATOR SHOWING LEFT SIDE AT 4 DEGREES AND RIGHT SIDE AT 7 DEGREES WITH 5 DEGREES OF FLAPS SELECTED. CREW UN
- [SDR TSAA0652004](https://openairdocs.org/sdr/TSAA0652004), Jan 16, 2006: SKIN. CRACKED. A 4.25 INCH SKIN CRACK ON AFT CARGO DOOR. CRACK LOCATED 18.5 INCHES FROM LOWER FWD CORNER AND 5 INCHES FROM FWD CUTOUT. MAINTENANCE REPAIRED WITH APPROXIMATELY 
- [SDR TSAA0529052](https://openairdocs.org/sdr/TSAA0529052), Oct 23, 2005: FILTER. CONTAMINATED. NON-ETOPS FLIGHT 278 HNL - KOA, AFTER TAKEOFF, NR 1 ENGINE HYDRAULIC SYSTEM A LOW PRESSURE LIGHT ILLUMINATED. CREW DISENGAGED ENGINE DRIVEN HYDRAULIC PUMP AND R
- [SDR TSAA0529051](https://openairdocs.org/sdr/TSAA0529051), Oct 23, 2005: HOSE. LEAKING. NON-ETOPS FLIGHT 88 LIH-HNL - AFTER GEAR UP, HYD PRESSURE INDICATOR SHOWED ZERO. LEFT MAIN LANDING GEAR INDICATOR LIGHTS SHOWED BOTH RED AND GREEN (UNSAFE). WHE
- [SDR TSAA0532032](https://openairdocs.org/sdr/TSAA0532032), Jul 27, 2005: CIRCUIT BREAKER. FAILED. FLT 71 OGG-HNL, AFTER DEPARTURE, CREW WAS UNABLE TO MOVE LANDING GEAR LEVER TO THE UP POSITION. CREW FOUND CIRCUIT BREAKER POPPED OUT AND THEN RESET IT. GEAR HA
- [SDR TSAA0532028](https://openairdocs.org/sdr/TSAA0532028), Jul 15, 2005: LANDING GEAR. MALFUNCTIONED. GEAR WOULD NOT RETRACT ON T/O FROM KONA. ISOLATION VALVE LIGHT CAME ON AND GEAR HANDLE COULD NOT BE RAISED PAST THE OFF POSITION. WITH GEAR HANDLE DOWN, WE HAD 
- [SDR TSAA0526026](https://openairdocs.org/sdr/TSAA0526026), Jun 25, 2005: ELEMENT. FAILED. DURING PUSHBACK AND PRIOR TO ENGINE START, THE CREW NOTED NR 2 ENGINE OVERHEAT INDICATION ILLUMINATED. THE CREW COMPLETED THE ENGINE OVERHEAT AND ENGINE FIRE CH
- [SDR TSAA0526025](https://openairdocs.org/sdr/TSAA0526025), Jun 19, 2005: CONNECTOR. DIRTY. ON CLIMB BETWEEN 11,000 FT AND 13,00 FT, PILOTS REPORTED NR 2 ENGINE OVERHEAT LIGHT FLICKERING AND THEN BECOMING STEADY. THE ENGINE OVERHEAT CHECKLIST WAS COMPL
- [SDR TSAA0425082](https://openairdocs.org/sdr/TSAA0425082), Dec 17, 2004: SLIDE. DEPLOYED. DURING GROUND MAINTENANCE, GROUND CREW INADVERTENTLY DEPLOYED THE FORWARD SERVICE DOOR ESCAPE SLIDE. NO INJURIES. REMOVED AND REPLACED THE FORWARD SERVICE DOOR 
- [SDR TSAA0477063](https://openairdocs.org/sdr/TSAA0477063), Aug 26, 2004: TRANSMITTER. INOPERATIVE. ON TAKE-OFF ROLL THE NR 1 ENGINE ONLY INDICATED 1.76 EPR; THE THROTTLES WERE ADVANCED WITH NO RESPONSE FROM ANY INSTRUMENTS. REJECTED TAKE-OFF AND RETURNED TO G
- [SDR TSAA0479046](https://openairdocs.org/sdr/TSAA0479046), Jun 9, 2004: BEARING. FAILED. NON-ETOPS FLIGHT 206, HNL-OGG: ON DESCENT ONTO OGG THE NR 2 ENGINE OIL PRESSURE LIGHT CAME ON, THE OIL PRESSURE DECREASED TOWARD ZERO AND THE OIL QUANTITY BEGAN
- [SDR TSAA0453002](https://openairdocs.org/sdr/TSAA0453002), Dec 24, 2003: SKIN. CRACKED. FOUND AN INCH AND A HALF AND A TWO INCH FUSELAGE CRACK AT BS 767 AND BS 792, ON STRINGER 18L. TRIMMED OUT CRACKS AND VERIFIED CUTOUTS USING HFEC METHOD, NO DEFE
- [SDR TSAA0375198](https://openairdocs.org/sdr/TSAA0375198), Dec 10, 2003: DUCT. FAILED. FLT 240 - HNL-OGG - ENGINE NR 1 OVERHEAT LIGHT CAME ON JUST AFTER TAKEOFF. PULLED THROTTLE BACK AND THE LIGHT WENT OUT. EGT IN GREEN THE ENTIRE TIME. REMOVED AN
- [SDR TSAA0329180](https://openairdocs.org/sdr/TSAA0329180), Nov 15, 2003: HOSE. FAILED. AFTER GEAR RETRACTION LOST ENTIRE 'A'SYSTEM HYD QTY. MAINTENANCE REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR PRESSURE RETURN HOSE ASSEMBLY. (M)
- [SDR TSAA0333126](https://openairdocs.org/sdr/TSAA0333126), May 31, 2003: BATTERY PACK. INOPERATIVE. REPLACED NR 4 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0357059](https://openairdocs.org/sdr/TSAA0357059), Apr 4, 2003: SKIN. DENTED. GAINED ACCESS TO DENTED AREA. CUTOUT DAMAGE BY SLICING THE LEADING EDGE SKIN PER FIGURE 1. INSTALLED A SPLICE REPAIR AT SS205.46 AND SS 238.71. REPAIR COMPLETED
- [SDR TSAA0352053](https://openairdocs.org/sdr/TSAA0352053), Mar 18, 2003: GUIDE. MISALIGNED. AFTER TAKEOFF, THE CABIN HAD AN EXCESSIVE RATE OF CLIMB, (2,500 FPM). AUTO FAILED ON THE PRESSURIZATION SYSTEM. LANDED HNL WITH NO FURTHER INCIDENT. MAINTENANCE
- [SDR TSAA0251181](https://openairdocs.org/sdr/TSAA0251181), Aug 19, 2002: STRAP. CORRODED. KEEL BEAM VERTICAL STRAP CORRODED AT BS 532. BLENDED AND FLAP PEENED REPAIR AREA, FABRICATED TWO FILLER STRAPS, INSTALLED FILLERS AND STRAP.
- [SDR TSAA0251178](https://openairdocs.org/sdr/TSAA0251178), Aug 16, 2002: STRINGER. CORRODED. FOUND CORROSION ON BS 500 AT STRINGER 26R. CUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. FABRICATED REPAIR ANGLES AND DOUBLER IAW SRM. REPAIR COMPLETED IAW
- [SDR TSAA0251180](https://openairdocs.org/sdr/TSAA0251180), Aug 15, 2002: STRINGER. CRACKED. CRACK LOCATED AT BS 767, S-14L. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES.
- [SDR TSAA0251177](https://openairdocs.org/sdr/TSAA0251177), Aug 15, 2002: SKIN. CRACKED. SKIN CRACK AT BS 380 BETWEEN STRINGER 28L AND 28R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0251179](https://openairdocs.org/sdr/TSAA0251179), Jun 17, 2002: STRINGER. CRACKED. CRACKS BS 739, S-18R AND BS 745, S-19R. REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL USING HFEC METHOD, FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR TSAA0253038](https://openairdocs.org/sdr/TSAA0253038), Feb 12, 2002: SKIN. CRACKED. REPAIRED 2.5 INCH LONG SKIN CRACK AT FUSELAGE BS 937 STRINGER 26R. CONFIRMED 2.5 INCH REMOVED USING HFEC METHOD. THE REPAIR CONSISTED OF CUTTING OUT THE SKIN CR
- [SDR TSAA0133182](https://openairdocs.org/sdr/TSAA0133182), Dec 24, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 3 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153149](https://openairdocs.org/sdr/TSAA0153149), Nov 5, 2001: SKIN. CRACKED. FOUND FUSELAGE CRACKED AT BS 767, S19L. TRIM OUT CRACK COMPLETED AND VERIFIED CUT OUT USING HFEC METHOD, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBL
- [SDR TSAA0133145](https://openairdocs.org/sdr/TSAA0133145), Oct 27, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 3 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133023](https://openairdocs.org/sdr/TSAA0133023), Mar 1, 2001: LIGHT. INOPERATIVE. REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0157009](https://openairdocs.org/sdr/TSAA0157009), Jan 24, 2001: SPAR. CORRODED. IDENTIFIED CORROSION AT RT WING FRONT SPAR LOWER CHORD FSS 475. REPAIRED CONSISTS OF REMOVING DAMAGED AREA AT HORIZONTAL FLANGE AND INSTALLING A TAPERED FILLER,
- [SDR TSAA0053255](https://openairdocs.org/sdr/TSAA0053255), Dec 27, 2000: KEEL. CORRODED. IDENTIFIED CORROSION AT THE VERTICAL LEG OF THE KEEL BEAM AT BS 535 APPROXIMATELY LBL 6.30. REPAIRED BY REMOVING CORROSION, BLEND OUT COMPLETED, CLEANED AND TRE
- [SDR TSAA0053253](https://openairdocs.org/sdr/TSAA0053253), Dec 22, 2000: SKIN. CRACKED. IDENTIFIED 3.7 INCH CRACK AT BS 747, STRINGER 18L. CONFIRMED USING HFEC METHOD. (M)
- [SDR TSAA0057142](https://openairdocs.org/sdr/TSAA0057142), May 22, 2000: BEAM. GOUGED. REPAIRED LT MLG BEAM AT THE OUTBOARD STABILIZER ATTACH POINT. REPAIR CONSISTS OF BLENDING OUT GOUGE AND REAMING OUT FASTENER HOLES AND INSTALLATIONS OF BUSHINGS
- [SDR TSAA0053141](https://openairdocs.org/sdr/TSAA0053141), May 18, 2000: SKIN. CRACKED. REPAIRED FUSELAGE SKIN 3 INCH CRACK AT BS 886 STRINGER 24 IAW SRM 53-30-3 FIG 1. VERIFIED BY HFEC METHOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033117](https://openairdocs.org/sdr/TSAA0033117), Apr 12, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 1 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033116](https://openairdocs.org/sdr/TSAA0033116), Apr 9, 2000: LIGHT. INOPERATIVE. REPLACED NR 1 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0053098](https://openairdocs.org/sdr/TSAA0053098), Mar 16, 2000: SKIN. CRACKED. REPAIRED 1.5 INCH CRACK ON FUSELAGE SKIN AT BS 744, STRINGER 19L IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033073](https://openairdocs.org/sdr/TSAA0033073), Mar 1, 2000: BATTERY PACK. INOPERATIVE. REPLACED THE AFT SERVICE DOOR EXIT IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033072](https://openairdocs.org/sdr/TSAA0033072), Mar 1, 2000: BATTERY PACK. INOPERATIVE. REPLACED THE FORWARD ENTRY EXIT IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA200033061](https://openairdocs.org/sdr/TSAA200033061), Feb 12, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 3 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933499](https://openairdocs.org/sdr/TSAA9933499), Dec 7, 1999: BATTERY PACK. INOPERATIVE. REPLACED NR 6 FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA9933470](https://openairdocs.org/sdr/TSAA9933470), Oct 24, 1999: BATTERY PACK. DISCHARGED. REPLACED NR 2 FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933469](https://openairdocs.org/sdr/TSAA9933469), Oct 24, 1999: LIGHT. INOPERATIVE. REPLACED NR 2 FLOOR LIGHT ASSY DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9972466](https://openairdocs.org/sdr/TSAA9972466), Oct 20, 1999: BLEED VALVE. FAILED. FLT 263 - HNL-LIH - COMPRESSOR STALL NR 2 ENGINE THROTTLE UP OFF OF IDLE. ABORTED TAKEOFF. RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENGINE PRESSURE BLEED CON
- [SDR TSAA9933452](https://openairdocs.org/sdr/TSAA9933452), Oct 8, 1999: LIGHT. INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9953404](https://openairdocs.org/sdr/TSAA9953404), Aug 16, 1999: SKIN. CRACKED. FOUND 4.125 INCH CRACK 2 INCH FORWARD OF BS 947 AT STRINGER 24L. SKIN REPAIR IAW SRM 53-30-3 FIGURE 6 SHEET 4 PAGE 12B. AIRCRAFT RETURNED TO SERVICE. (M)

All 104: https://openairdocs.org/deregistered/N807AL-2008-07-30/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 19970709022739I](https://openairdocs.org/incident/19970709022739I), Jul 9, 1997: Boeing 7372T4 (N807AL), Honolulu, HI. Loud bang yaw and roll on climbout returned. Unable to find source. Replaced yaw damper and dfdr.

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