# N819AL: 1987 Boeing 737-25A, registration cancelled 2005-11-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 14, 2005 - Exported to: Nigeria - Status when cancelled: Second triennial mailing, no response - Airframe: [Boeing 737-25A](https://openairdocs.org/model/boeing-737-25a) (registry code 1384481) - 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: 23791 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 17, 1987 - Certificate issued: August 11, 1998 - Last registry action: September 28, 2004 - Mode S code: AB2AD6 - Owner when cancelled: [Boeing Capital Corporation](https://openairdocs.org/faa-owner/BOEING%20CAPITAL%20CORPORATION) - Location: [Long Beach, CA](https://openairdocs.org/faa-place/CA/Long%20Beach) - Owner type: Corporation - Owner's area on the map: 33.8239° N, 118.1113° W: Placed by OpenAirDocs at the center of ZIP code 90808, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N819AL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=819AL - Page: https://openairdocs.org/deregistered/N819AL-2005-11-14 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 737-25A: https://openairdocs.org/model/boeing-737-25a.md ## Service difficulty reports (115, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TSAA0524018](https://openairdocs.org/sdr/TSAA0524018), Apr 4, 2005: CIRCUIT BREAKER. DAMAGED. CREW REPORTED SMOKE IN THE COCKPIT. SMOKE FROM CB PANEL BEHIND F/O. SLIDING WINDOW OPENED TO VENT SMOKE. RETURNED TO GATE. REMOVED AND REPLACED THE APU GCU. DID - [SDR TSAA0421081](https://openairdocs.org/sdr/TSAA0421081), Nov 30, 2004: CLAMP. LOOSE. PRESSURIZATION CHECKED BEFORE TAKEOFF, CABIN CLIMBED TO 1,000 FT BY THE TIME AIRCRAFT LEVELED AT 3,000 FT. RETURNED TO OGG. NOTE THAT THE RIGHT PACK WAS DEACTIV - [SDR TSAA0472079](https://openairdocs.org/sdr/TSAA0472079), Nov 27, 2004: ENGINE. FAILED. NON-ETOPS FLT. 241, HNL-LIH: CLIMBING THROUGH 8,000 FEET, HEARD A LOUD BANG AND THE AIRCRAFT YAWED RIGHT. THE NR 2 ENGINE EPR DROPPED FROM 1.82 TO 1.76. REPORTE - [SDR TSAA0473068](https://openairdocs.org/sdr/TSAA0473068), Sep 14, 2004: FCU. MALFUNCTIONED. ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, ENGINE POWER ADVANCED NORMALLY UNTIL 1.96-1.97 EPR INDICATION. MAX-POWER OBTAINED WAS 1.97 EPR WITH N1 AT - [SDR TSAA0431067](https://openairdocs.org/sdr/TSAA0431067), Sep 12, 2004: INDICATOR. SLOW. NON-ETOPS FLIGHT 62, HNL-OGG: ON TAKEOFF 80KTS CROSS-CHECK WAS OK, AFTER LIFTOFF THE FIRST-OFFICERS AIRSPEED INDICATOR READ 50KTS SLOWER THAN CAPTAIN’S STANDBY - [SDR TSAA0477066](https://openairdocs.org/sdr/TSAA0477066), Sep 11, 2004: ENGINE. MALFUNCTIONED. ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, MAX-EPR INDICATION OF 1.96. RETURNED TO HNL. CLEANED DEBRIS FROM PT2 LINE AND VERIFIED SECURITY OF ALL EPR - [SDR TSAA0452026](https://openairdocs.org/sdr/TSAA0452026), Feb 4, 2004: DOOR FRAME. CORRODED. FOUND CORROSION ON FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED REPAIR DOUBLERS AND TRIPLER. ALODINED AND PRIMED - [SDR TSAA0477018](https://openairdocs.org/sdr/TSAA0477018), Jan 9, 2004: CIRCUIT BREAKER. TRIPPED. FLT 280 - HNL-KOA - ABORTED TAKEOFF DUE TO BOTH EPR GAUGES INOPERATIVE. C/B'S RESET, NO FLAGS. RAN BOTH NR 1 AND NR 2 ENGINE AFTER EPR C/B RESET. OPS CHECK GOOD - [SDR TSAA0333147](https://openairdocs.org/sdr/TSAA0333147), Jun 7, 2003: BATTERY PACK. INOPERATIVE. REPLACED AFT ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0333146](https://openairdocs.org/sdr/TSAA0333146), Jun 7, 2003: BATTERY PACK. INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0353150](https://openairdocs.org/sdr/TSAA0353150), May 22, 2003: CREASE BEAM. CORRODED. FOUND CORROSION DISCOVERED ON LEFT CREASE BEAM BETWEEN BS 307 AND 310. REMOVED AND REPLACED SECTION BETWEEN BS 307 AND BS 310. ALODINE, PRIMED, AND INSTALLED RE - [SDR TSAA0357117](https://openairdocs.org/sdr/TSAA0357117), May 7, 2003: WEB. CORRODED. CORROSION DISCOVERED ON RIGHT WING SPAR WEB AT FSS 540-552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED SECTION OF WEB. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOL - [SDR TSAA0353133](https://openairdocs.org/sdr/TSAA0353133), May 6, 2003: FLOORBEAM. CORRODED. FOUND CORROSION DISCOVERED AT BS 312 FLOORBEAM UPPER TEE. CUTOUT DAMAGED SECTION OF STRINGER. FABRIATED NEW CHORD SECTION AND SPLICE ANGLE. DRILLED FASTENER HOL - [SDR TSAA0353132](https://openairdocs.org/sdr/TSAA0353132), May 6, 2003: STRINGER. CRACKED. CRACK DISCOVERED ON STRINGER 4 LEFT, LOCATED AT BS 907. CUTOUT DAMGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DIRLLED FASTENER HOLES. ALODINE, PRIMED, - [SDR TSAA0353120](https://openairdocs.org/sdr/TSAA0353120), May 6, 2003: SKIN. DENTED. DENT DISCOVERED ON FUSELAGE SKIN BETWEEN BS 981 AND 996 ALONG STRINGER 14L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED A REPAIR DOUBLER AND TRIPLER - [SDR TSAA0353119](https://openairdocs.org/sdr/TSAA0353119), May 6, 2003: STRINGER. DENTED. DENT DISCOVERED AT BS 376 ALONG STRINGER 17L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, - [SDR TSAA0353118](https://openairdocs.org/sdr/TSAA0353118), May 6, 2003: STRINGER. CORRODED. CORROSION DISCOVERED ON STRINGER LOCATED AT BS 967, LBL 7. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIM - [SDR TSAA0353138](https://openairdocs.org/sdr/TSAA0353138), May 5, 2003: SKIN. DENTED. DISCOVERED A 15 INCH GOUGE WITH A DENT LOCATED AT BS 981 THROUGH BS 996, 4 INCHES ABOVE STRINGER 4 LT. CUTOUT GOUGE AND DENTED PORTION OF THE SKIN. FABRICATED D - [SDR TSAA0353139](https://openairdocs.org/sdr/TSAA0353139), May 5, 2003: SKIN. DENTED. DISCOVERED A DENT LOCATED AT BS 346, BETWEEN STRINGER 24 AND 25 RIGHT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED A REPAIR PLATE, DRILLED FASTENER HOLES, ALO - [SDR TSAA0353137](https://openairdocs.org/sdr/TSAA0353137), May 5, 2003: SKIN. DENTED. DENT DISCOVERED AT BS 376 ALONG STRINGER 17 LT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED AND INSTALL - [SDR TSAA0353141](https://openairdocs.org/sdr/TSAA0353141), May 5, 2003: STRINGER CLIP. DAMAGED. DISCOVERED A DAMAGED STRINGER CLIP LOCATED AT BS 380, STRINGER 2 RIGHT. REMOVED AND REPLACED DAMAGED CLIP. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH - [SDR TSAA0353140](https://openairdocs.org/sdr/TSAA0353140), May 5, 2003: SHEAR TIE. DAMAGED. DISCOVERED A DAMAGED SHEAR TIE LOCATED AT BS 360, BETWEEN STRINGER 14 AND 15 RIGHT. CUTOUT DENTED PORTION. FABRICATED A NEW SHEAR TIE, DRILLED FASTENER HOLES, A - [SDR TSAA0351142](https://openairdocs.org/sdr/TSAA0351142), May 5, 2003: ANGLE. CRACKED. DISCOVERED A CRACKED ATTACHMENT ANGLE LOCATED AT BS 289, WL 239. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET W - [SDR TSAA0353136](https://openairdocs.org/sdr/TSAA0353136), May 5, 2003: STRINGER. CORRODED. CORROSION DISCOVERED AT BS 967, LBL 7, AND WL 171. CUTOUT DAMAGED PORTION OF THE STRINGER. FABRICATED NEW STRINGER SECTION, DRILLED FASTENER HOLES, ALODINED, PR - [SDR TSAA0353135](https://openairdocs.org/sdr/TSAA0353135), May 5, 2003: WEB. CORRODED. CORROSION DISCOVERED BETWEEN FSS 540 AND 552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED PORTION OF THE WEB. FABRICATED NEW WEB SECTION, DRILLED FASTENER HOLES, ALODIN - [SDR TSAA0353134](https://openairdocs.org/sdr/TSAA0353134), May 5, 2003: SHEAR TIE. DAMAGED. DAMAGED SHEAR TIE DISCOVERED AT BD 908 BETWEEN STRINGERS 14 AND 15 LEFT. CUTOUT DAMAGED SECTION. FABRICATED NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRI - [SDR TSAA0351124](https://openairdocs.org/sdr/TSAA0351124), May 5, 2003: STRINGER CLIP. CRACKED. CLIP DISCOVERED CRACKED OR TORN ON STRINGER 2R LOCATED AT BS 380. REMOVED DAMAGED CLIP. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND - [SDR TSAA0353121](https://openairdocs.org/sdr/TSAA0353121), May 5, 2003: SHEAR TIE. DAMAGED. DAMAGE DISCOVERED ON SHEER TIE BETWEEN STRINGER 14 AND 15L AT BS 360. CUTOUT DAMAGED SECTION OF SHEAR TIE. FABRICATED A REPAIR SHEAR TIE AND RADIUS FILLER. ALOD - [SDR TSAA0353123](https://openairdocs.org/sdr/TSAA0353123), May 5, 2003: SKIN. DENTED. DENT LOCATED AT BS 396 BETWEEN STRINGER 24 AND 25R. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED A NEW STRINGER REPAIR SECTION. ALODINE, PRIMED, AND INSTALLED - [SDR TSAA0351143](https://openairdocs.org/sdr/TSAA0351143), May 5, 2003: STRINGER. DAMAGED. DAMAGED STRINGER 2 RIGHT WHILE REMOVING STRINGER CLIP. CUTOUT DAMAGED STRINGER SECTION BETWEEN BS 360 AND BS 389. FABRICATED NEW STRINGER SECTION, ALODINED, PRI - [SDR TSAA0351148](https://openairdocs.org/sdr/TSAA0351148), May 4, 2003: CHANNEL. CORRODED. FOUND CORROSION ON C-CHANNEL UPPER STRUCTURE LOCATED BETWEEN BS 312 AND BS 344 AT WL 208, LBL 57. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 312 AND BS 344. - [SDR TSAA0353149](https://openairdocs.org/sdr/TSAA0353149), May 4, 2003: CREASE BEAM. CORRODED. FOUND CORROSION ON RIGHT CREASE BEAM AROUND NUT PLATE HOLES BETWEEN BS 290 AND 358. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 290 AND BS 358. ALODINE, PRIM - [SDR TSAA0353151](https://openairdocs.org/sdr/TSAA0353151), Apr 30, 2003: STRINGER. GOUGED. DAMAGED OR GOUGE STRINGER DISCOVERED AT BS 382. CUTOUT GOUGED AREA. FABRICATED FILLER, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A F - [SDR TSAA0353110](https://openairdocs.org/sdr/TSAA0353110), Apr 23, 2003: FRAME. CRACKED. FOUND BS 244 FRAME CRACKED AT RIGHT CREASE BEAM. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED RE - [SDR TSAA0353111](https://openairdocs.org/sdr/TSAA0353111), Apr 23, 2003: FLOORBEAM. CORRODED. FOUND CORROSION ON UPPER FLOORBEAM AT BS 344 BLENDED OUT 1 INCH BY 1 INCH AREA IN TWO PLACES. CUTOUT DAMAGED AREA. FABRICATED NEW FLOORBEAM SECTION PER TABLE II - [SDR TSAA0333021](https://openairdocs.org/sdr/TSAA0333021), Feb 2, 2003: BATTERY PACK. INCORRECT. REPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0233215](https://openairdocs.org/sdr/TSAA0233215), Oct 15, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 1,2,4, AND 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0253203](https://openairdocs.org/sdr/TSAA0253203), Oct 1, 2002: SKIN. GOUGED. REMOVED DAMAGE ON FWD CARGO DOOR CUT OUT. PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, N - [SDR TSAA0225160](https://openairdocs.org/sdr/TSAA0225160), Jul 11, 2002: SLIDE. DEFECTIVE. DURING A ROUTINE TRAINING EXERCISE AND AFTER SUCCESSFUL SLIDE DEPLOYMENT, THE SLIDE ASSEMBLY EXPLODED AT THE SEAM. NO HARM TO PERSONNEL. REMOVED AND REPLACED SL - [SDR TSAA0232137](https://openairdocs.org/sdr/TSAA0232137), May 12, 2002: SWITCH. STUCK. ANTI-SKID INOPERATIVE LIGHT ILLUMINATED ON BOTH SYSTEMS DURING FLIGHT. DUE TO WEATHER CONDITIONS, RUNWAY LENGTH AND AIRCRAFT WEIGHT FOR THE AIRPORT, THE AIRCRAF - [SDR TSAA0257032](https://openairdocs.org/sdr/TSAA0257032), Jan 8, 2002: STRUCTURE. CRACKED. REPAIRED CRACK AT NR 5 SLAT STATION 195.53. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MI - [SDR TSAA0257033](https://openairdocs.org/sdr/TSAA0257033), Jan 8, 2002: STRUCTURE. CRACKED. REPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MIN - [SDR TSAA0253034](https://openairdocs.org/sdr/TSAA0253034), Jan 8, 2002: FLOORBEAM. CRACKED. FOUND CABIN INTERIOR LONGITUDINAL FLOORBEAM UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITUDINAL FLOORBEAM IA - [SDR TSAA0253035](https://openairdocs.org/sdr/TSAA0253035), Jan 8, 2002: SKIN. CRACKED. REPAIRED A 4 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 18 RT. VERIFEID CUTOUT USING HFEC. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM - [SDR TSAA0253036](https://openairdocs.org/sdr/TSAA0253036), Jan 8, 2002: SKIN. CRACKED. REPAIRED A 2.5 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 19 RT. VERIFIED CUTOUT USING HFEC. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SR - [SDR TSAA0253037](https://openairdocs.org/sdr/TSAA0253037), Jan 8, 2002: SKIN. DELAMINATED. FOUND DELAMINATION ON LOWER SURFACE OF RIGHT ELEVATOR. TRIMMED OUT DAMAGED LAMINATION TO A SMOOTH SHAPE WITH ROUNDED CORNERS. FABRICATED, CLEANED AND INSTALLED - [SDR TSAA0257039](https://openairdocs.org/sdr/TSAA0257039), Jan 8, 2002: STRUCTURE. CRACKED. REPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MIN - [SDR TSAA0253040](https://openairdocs.org/sdr/TSAA0253040), Jan 8, 2002: SKIN. CORRODED. BLENDED OUT CORROSION ON THE FUSELAGE SKIN AT BS 990 STRINGER 27L BY CUTTING STRINGER 27L IAW SRM 51-10-2. VERIFIED CORROSION REMOVED, CLEANED AND TREATED IAW S - [SDR TSAA0253041](https://openairdocs.org/sdr/TSAA0253041), Jan 8, 2002: FLOOR SUPPORT. CRACKED. FOUND CABIN INTERIOR LONGITUTIONAL FLOOR SUPPORT UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITIONAL FLOORBEA - [SDR TSAA0257031](https://openairdocs.org/sdr/TSAA0257031), Jan 8, 2002: SLAT. CRACKED. REPAIRED CRACK AT NR 6 SLAT STATION 370.56. BLENDED OUT THE DAMAGED AREA IAW SRM 57-20-1, FIG 1, PAGE 1. AIRCRAFT RETURNED TO SERVICE. (M) All 115: https://openairdocs.org/deregistered/N819AL-2005-11-14/reports.md ## Other aircraft with N819AL - [Registered now](https://openairdocs.org/aircraft/N819AL): Zipline International P2 ZIP, S/N 18736P22639 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.