# N824AL: 1983 Boeing 737-282, registration cancelled 2013-10-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 29, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 737-282](https://openairdocs.org/model/boeing-737-282) (registry code 13844AT)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 23045
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 30, 1998
- Certificate issued: October 22, 2008
- Last registry action: October 22, 2008
- Mode S code: AB3FC2
- Owner when cancelled: [Air Carrier Accessory Service](https://openairdocs.org/faa-owner/AIR%20CARRIER%20ACCESSORY%20SERVICE)
- Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)
- Owner type: Corporation
- Owner's area on the map: 26.0870° N, 80.1530° W: Placed by OpenAirDocs at the center of ZIP code 33315, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N824AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=824AL
- Page: https://openairdocs.org/deregistered/N824AL-2013-10-29

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 737-282: https://openairdocs.org/model/boeing-737-282.md

## Service difficulty reports (78, newest 50)

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

- [SDR TSAA0821016](https://openairdocs.org/sdr/TSAA0821016), Mar 13, 2008: FAN. FAILED. FLIGHT 93 OGG - HNL - THE CREW NOTED AN UNPLEASANT BURNING ODOR IN THE CABIN DURING FLIGHT WITH NO SMOKE PRESENT. THE ODOR DECREASED WITH ENGINES AT LOWER THROT
- [SDR TSAA0853003](https://openairdocs.org/sdr/TSAA0853003), Jan 8, 2008: BULKHEAD. CRACKED. WHILE PERFORMING ECO 1822 PART I (REFERENCE AD 93-08-08 AND AD 90-06-02) A CRACK WAS DISCOVERED ON THE LT BULKHEAD BS 1156 ALONG THE LAST ROW OF RIVETS APPROX W
- [SDR TSAA0721046](https://openairdocs.org/sdr/TSAA0721046), Aug 15, 2007: SENSOR. FAILED. NON-ETOPS FLIGHT 63 HNL-LIH, DURING CLIMB, THE CREW NOTED LOUD NOISE AND ICE EMANATING FROM THE AIR CONDITIONING SYSTEM. THE CREW ATTEMPTED TO CONTROL THE NOISE
- [SDR TSAA0675112](https://openairdocs.org/sdr/TSAA0675112), Nov 24, 2006: CONTROL VALVE. FAILED. FLT 206 HNL-OGG: DURING TAKEOFF ROLL, NR 1 ENGINE EPR WOULD NOT INCREASE ABOVE 1.53 WITH MORE THAN A TWO THROTTLE KNOB WIDTH SPLIT AND EGT RISING TO 580 DEGREES
- [SDR TSAA0632094](https://openairdocs.org/sdr/TSAA0632094), Nov 2, 2006: UPLOCK. DIRTY. AFTER TAKEOFF, THE RT MLG DID NOT RETRACT. CREW CYCLED THE LANDING GEAR LEVER AND WAS ABLE TO RETRACT THE GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MA
- [SDR TSAA0672088](https://openairdocs.org/sdr/TSAA0672088), Oct 16, 2006: NOSE BULLET. LOOSE. NON-ETOPS FLT 281: CLIMBING THRU 16,000 FEET WITH THE ENGINE ANTI-ICE ON, THE CREW HEARD A LOUD BANGING SOUND COMING FROM THE LT SIDE OF THE AIRCRAFT. ENGINE IN
- [SDR TSAA0629060](https://openairdocs.org/sdr/TSAA0629060), Jul 28, 2006: HOSE. FAILED. NON-ETOPS FLT 77 ITO-HNL: DURING LANDING ROLLOUT, THE AIRCRAFT EXPERIENCED SYSTEM ‘A’ HYDRAULIC FAILURE. THE CREW BROUGHT THE AIRCRAFT TO A STOP, NOTIFIED TOWER
- [SDR TSAA0652044](https://openairdocs.org/sdr/TSAA0652044), Jun 6, 2006: SLIDE. OUT OF POSITION. NON-ETOPS: FLT 206 HNL - OGG: ON THE GROUND, FWD SVC DOOR EMERGENCY SLIDE ACCIDENTALLY DISLODGED FROM THE DOOR BUT DID NOT INFLATE. REMOVED AND REPLACED FORWARD
- [SDR TSAA0653002](https://openairdocs.org/sdr/TSAA0653002), Jan 5, 2006: SKIN PANEL. CRACKED. FUSELAGE SKIN CRACK LOWER BL-0, BETWEEN S-28L AND R AT BS 370. TWO 1/2 INCH FUSELAGE SKIN CRACKS LOWER BL-0, BETWEEN S-28L AND R AT BS370 AND BS380. MAINTENANCE
- [SDR TSAA0532055](https://openairdocs.org/sdr/TSAA0532055), Nov 11, 2005: TIRE. FAILED. DURING TAXI AFTER LANDING, CREW HEARD A LOAD POP FOLLOWED BY VIBRATION FROM THE NOSEWHEEL AND STEERING DIFFICULTY. CREW STOPPED AIRCRAFT ON TAXIWAY. MAINTENANCE
- [SDR TSAA0532050](https://openairdocs.org/sdr/TSAA0532050), Oct 20, 2005: ANTI-SKID SYS. DEACTIVATED. ON CLIMB OUT, PILOT OBSERVED THE LT ANTI-SKID LIGHT ON AND STAYED AND RETURNED BACK TO DEPARTURE. THE ANTI-SKID SYSTEM WAS MEL’D WAITING FOR AN ANTI-SKID CONTRO
- [SDR TSAA0552009](https://openairdocs.org/sdr/TSAA0552009), Feb 25, 2005: WARNING LIGHT. FALSE INDICATION. FLT 211, OGG-HNL, FORWARD CARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF PRIOR TO 80 KTS. RETURNED TO GATE. MAINTENANCE OPENED AND CLOSED THE FOR
- [SDR TSAA0527002](https://openairdocs.org/sdr/TSAA0527002), Jan 16, 2005: SENSOR. DEFECTIVE. FLT 278, HNL-KOA: ON INITIAL TAKEOFF ROLL, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED (NR 4 SLAT) WITH THE CONFIGURATION WARNING HORN. ABORTED TAKEOFF AND 
- [SDR TSAA0434084](https://openairdocs.org/sdr/TSAA0434084), Dec 22, 2004: INDICATOR. INOPERATIVE. FLT 220, HNL-OGG: FIRST OFFICE AIRSPEED INDICATOR INOP. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE MACH AIR SPEED INDICATOR. OPS CHECK OKAY. 
- [SDR TSAA0436069](https://openairdocs.org/sdr/TSAA0436069), Sep 17, 2004: BLEED AIR SYS. MALFUNCTIONED. FLIGHT 280, HNL-KOA: PASSING THROUGH 8000 FT ON CLIMB-OUT, THE RT DUCT PRESSURE WAS OBSERVED AT ABOUT 40PSIG WITH THE ISOLATION VALVE CLOSED AND THE RT BLEED & 
- [SDR TSAA0353219](https://openairdocs.org/sdr/TSAA0353219), Nov 2, 2003: SKIN. CORRODED. FOUND LT UPPER WING SURFACE CORRODED BETWEEN FRONT & REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 6 AS NR 1 - 19 AT LOCATIONS, NR 1, 2, & 3 AT WBL 227, NR 4 AT WLB
- [SDR TSAA0353218](https://openairdocs.org/sdr/TSAA0353218), Nov 2, 2003: SKIN. CORRODED. FOUND RIGHT UPPER WING SURFACE CORROSION BETWEEN THE FRONT AND REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 5 AS NR 1 TO NR 15 AT THE FOLLOWING LOCATIONS, NR 1 AT 
- [SDR TSAA0253267](https://openairdocs.org/sdr/TSAA0253267), Sep 24, 2003: SKIN. CRACKED. CLEANED OUTER SKIN AT EACH MOUNTING HOLE. OVER-DRILLED ELONGATED HOLES TO RESTORE HOLES TO CIRCULAR SHAPE. TRIMMED OUT CRACK DAMAGED HOLE LARGE ENOUGH TO REMOVE
- [SDR TSAA0253249](https://openairdocs.org/sdr/TSAA0253249), Sep 17, 2003: FLOORBEAM. CRACKED. REMOVED EXISTING FASTENERS, STIFFENERS, ANGLE AND A SECTION OF THE WEB. REMOVED AND DISCARDED REINFORCING ANGLE, DOUBLER AND A SECTION OF THE WEB. DRILL AND COL
- [SDR TSAA0253268](https://openairdocs.org/sdr/TSAA0253268), Sep 10, 2003: LAP JOINT. DAMAGED. TRIMMED BONDED DOUBLER ABOVE EXISTING FASTENER PATTERN LEAVING ED FOR FINAL FASTENER INSTALL. OPENED DISCREPANT COUNTERSINK HOLE TO .75 INCH DIAMETER. VERIFIED 
- [SDR TSAA0255264](https://openairdocs.org/sdr/TSAA0255264), Sep 5, 2003: SKIN. GOUGED. CUT AND REMOVED GOUGE AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. RE
- [SDR TSAA0255266](https://openairdocs.org/sdr/TSAA0255266), Sep 5, 2003: SKIN. GOUGED. CUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR C
- [SDR TSAA0255265](https://openairdocs.org/sdr/TSAA0255265), Sep 5, 2003: SKIN. DENTED. CUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR C
- [SDR TSAA0253236](https://openairdocs.org/sdr/TSAA0253236), Oct 27, 2002: PRESSURE PANEL. DAMAGED. PERFORMED MODIFICATION TO THE WEB AND DOUBLER OF THE MAIN WHEEL WELL PRESSURE FLOOR TRANSVERSE BEAM BETWEEN BS 650 AND BS 727 AND BETWEEN RT AND LT BBL 45. FABR
- [SDR TSAA0253235](https://openairdocs.org/sdr/TSAA0253235), Oct 27, 2002: BEAM. DAMAGED. OVERSIZED 4 HOLES IN THE RIGHT MLG LOWER BEAM CHORD FLANGE. FABRICATED FOUR FREEZE PLUGS. FABRICATED FOUR 1 INCH DIAMETER RETAINING WASHERS. INSTALLED FREEZE PL
- [SDR TSAA0253232](https://openairdocs.org/sdr/TSAA0253232), Oct 27, 2002: STRUCTURE. CRACKED. TRIMMED OUT THE DAMAGE OF THE HOLES TO A RECTANGULAR SHAPE. VERIFIED CRACK REMOVED USING HFEC. FABRICATED CIRCULAR DOUBLERS FOR EACH HOLE. REPAIR COMPLETED IAW 
- [SDR TSAA0253231](https://openairdocs.org/sdr/TSAA0253231), Oct 27, 2002: FITTING. DAMAGED. REMOVED DAMAGE FROM THE NR 2 AND NR 7 FLAP TRACK ATTACHMENT FITTING HOLE. FABRICATED A 'NEW' REPLACEMENT TUBE AND BUSHING INCREASING THE OUTSIDE DIAMETER .0015 
- [SDR TSAA0253234](https://openairdocs.org/sdr/TSAA0253234), Oct 18, 2002: STRUCTURE. CORRODED. BLENDED THE DAMAGE ON THE LUG. SPOTFACED THE INBOARD AND OUTBOARD SURFACES. OVERSIZED THE TAPERED/ELONGATED HOLE OF THE INBOARD LUG ON THE ORIGINAL CENTERLINE T
- [SDR TSAA0253233](https://openairdocs.org/sdr/TSAA0253233), Oct 18, 2002: STRUCTURE. CRACKED. TRIM OUT ALL THREE HOLES IN THE DAMAGED ZONE. HFEC THE EDGE OF THE TRIM. FABRICATED A DOUBLER AND A TRIPLER. INSTALLED DOUBLER AND TRIPLER. REPAIR COMPLETED IAW
- [SDR TSAA0233136](https://openairdocs.org/sdr/TSAA0233136), May 9, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 6, EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233054](https://openairdocs.org/sdr/TSAA0233054), Feb 18, 2002: BATTERY PACK. DISCHARGED. REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133184](https://openairdocs.org/sdr/TSAA0133184), Dec 27, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 1 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0126181](https://openairdocs.org/sdr/TSAA0126181), Dec 23, 2001: FIRE LOOP. DEFECTIVE. FLT 205 - HNL-LIH - EN ROUTE TO LIH, THE APU FIRE WARNING ILLUMINATED THOUGH THE APU WAS PREVIOUSLY MEL'D. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT R
- [SDR TSAA0133164](https://openairdocs.org/sdr/TSAA0133164), Nov 26, 2001: BATTERY PACK. DISCHARGED. REPLACED LEFT OVERWING IDENT BATTERY PACKED DUE TO LOW VOLTAGE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153151](https://openairdocs.org/sdr/TSAA0153151), Oct 31, 2001: BULKHEAD. CRACKED. FOUND RIVET HOLES CRACKED AT BS 178 LEFT AND RIGHT LBL 9 WL 234. REMOVED CRACK PER SRM 53-10-11 PAGE 1, PROCEDURE 1. VERIFIED CRACK REMOVED USING HFEC. INSTALLE
- [SDR TSAA0133096](https://openairdocs.org/sdr/TSAA0133096), Jul 18, 2001: BATTERY PACK. CORRODED. FOUND LEFT OVERWING EMERGENCY IDENT LIGHT INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133095](https://openairdocs.org/sdr/TSAA0133095), Jul 18, 2001: BATTERY PACK. CORRODED. AFT ENTRY DOOR EMEREGNCY IDENT LIGHT INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133082](https://openairdocs.org/sdr/TSAA0133082), Jul 7, 2001: BATTERY PACK. INOPERATIVE. REPLACED NR 1 AND NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153021](https://openairdocs.org/sdr/TSAA0153021), Feb 20, 2001: FRAME. CRACKED. IDENTIFIED A CRACK AT 2 PLACES ON THE RIGHT SIDE OF BS 1156 CHORD BETWEEN WL 281-269. STOP DRILLED ENDS OF CRACKS, REMOVED FASTENERS ON AFFECTED CHORD ASSEMBLY 
- [SDR TSAA0153019](https://openairdocs.org/sdr/TSAA0153019), Feb 17, 2001: FRAME. CRACKED. IDENTIFIED CRACK AT RIGHT UPPER CHORD BS 727, STRINGER 18A AFT HOLE BY UTILIZING HFEC AND ULTRASONIC METHOD. REMOVED AND REPLACED RIGHT UPPER CHORD ASSEMBLY CLE
- [SDR TSAA0153020](https://openairdocs.org/sdr/TSAA0153020), Feb 16, 2001: FRAME. DENTED. IDENTIFIED DENT ON FRAME ASSEMBLY 5 INCHES BY 7 INCHES AT BS 360-380 STRINGER 17L. (M)
- [SDR TSAA0033206](https://openairdocs.org/sdr/TSAA0033206), Sep 5, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 1, NR 4 AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA200033056](https://openairdocs.org/sdr/TSAA200033056), Feb 3, 2000: BATTERY PACK. INOPERATIVE. REPLACED POSITION 1 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA200032031](https://openairdocs.org/sdr/TSAA200032031), Jan 22, 2000: VALVE. INOPERATIVE. HNL/ITO - FLT 108 - ON TAKOFF ROLL, PARKING BRAKE LIGHT AND ANTI-SKID INOPERABLE. INBOARD/OUTBAORD LIGHT REMAINED ILLUMINATED. PARKING BRAKE LEVER WAS IN RELEAS
- [SDR TSAA9933518](https://openairdocs.org/sdr/TSAA9933518), Dec 29, 1999: BATTERY PACK. DISCHARGED. REPLACED BATTERY PACK FOR NR 2 EMERGENCY FLOOR PROX LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933447](https://openairdocs.org/sdr/TSAA9933447), Sep 29, 1999: BATTERY PACK. DISCHARGED. REPLACED BATTERY PACK FOR CENTER AISLE EMERGENCY LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNE TO SERVICE. (M)
- [SDR TSAA9957416](https://openairdocs.org/sdr/TSAA9957416), Aug 26, 1999: BEAM. CORRODED. LEFT MLG BEAM CORRODED BEYOND LIMITS. REPLACED LEFT MLG BEAM (PERFORMED BY BOEING AOG TEAM). AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9952415](https://openairdocs.org/sdr/TSAA9952415), Aug 26, 1999: FRAME. CRACKED. FORWARD ENTRY DOOR FRAME CORRODED AT LWR AFT CORNER ABOVE DOOR SILL. REPAIRED IAW ECO 2992. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933411](https://openairdocs.org/sdr/TSAA9933411), Aug 23, 1999: BATTERY. DISCHARGED. REPLACED BATTERY PACKS FOR NR 2, NR 4 AND NR 5 EMERGENCY FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933390](https://openairdocs.org/sdr/TSAA9933390), Aug 12, 1999: BATTERY PACK. DISCHARGED. REPLACED BATTERY PACK IN AFT CONTROL MODULE DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

All 78: https://openairdocs.org/deregistered/N824AL-2013-10-29/reports.md

## Other aircraft with N824AL

- [Registered now](https://openairdocs.org/aircraft/N824AL): Zipline International P2 ZIP, S/N 18736P22571

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