# N826AL: 1983 Boeing 737-282C, registration cancelled 2014-04-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 16, 2014 - Status when cancelled: Valid registration - Airframe: [Boeing 737-282C](https://openairdocs.org/model/boeing-737-282c) (registry code 13844AU) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23051 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 30, 1998 - Certificate issued: April 15, 2011 - Last registry action: February 4, 2014 - Mode S code: AB4730 - Owner when cancelled: [Aeko Kula Inc](https://openairdocs.org/faa-owner/AEKO%20KULA%20INC) - Location: [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu) - Owner type: Corporation - Owner's area on the map: 21.3363° N, 157.9207° W: Placed by OpenAirDocs at the center of ZIP code 96820, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N826AL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=826AL - Page: https://openairdocs.org/deregistered/N826AL-2014-04-16 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 737-282C: https://openairdocs.org/model/boeing-737-282c.md ## Service difficulty reports (121, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TSAA20130822007](https://openairdocs.org/sdr/TSAA20130822007), Aug 22, 2013: CLAMP. FAILED. DURING CLIMB, AT 3000 FT, CREW NOTICED THE LT WING TO BODY OVERHEAT WARNING LIGHT ILLUMINATED. AFTER 2 MINUTES, THE RT WING TO BODY OVERHEAT WARNING ALSO ILLUMI - [SDR TSAA20120713004](https://openairdocs.org/sdr/TSAA20120713004), Jul 13, 2012: ENGINE. POWER LOSS. DURING TAKEOFF/CLIMB AT APPROXIMATELY 400 FEET, NR 2 ENGINE FAILURE/LOSS OF POWER WITH HEAVY VIBRATION. COMPLETED ENGINE FAILURE AND SHUTDOWN CHECKLIST. INFLIGH - [SDR TSAA20120531002](https://openairdocs.org/sdr/TSAA20120531002), May 31, 2012: FRAME. CRACKED. CRACK APPROX 2.6250 FOUND AT BS 927, STRINGER 23L. REPAIR COMPLIED WITH IAW SRM 53-30-3, FIG 48, DETAIL XI. - [SDR 7AHR201192030](https://openairdocs.org/sdr/7AHR201192030), Oct 16, 2011: FRAME. CRACKED. AFT PIT CRACKED, FRAME LOWER CHORD AT BS 907 AND STRINGER 26R. - [SDR 7AHR2011092029](https://openairdocs.org/sdr/7AHR2011092029), Oct 8, 2011: SEAT TRACK. CRACKED. MAIN CABIN SEAT TRACK UPPER FLANGE CRACKED STATION 727B AT RBL 24.75 - [SDR 7AHR2011092028](https://openairdocs.org/sdr/7AHR2011092028), Sep 23, 2011: FLOORBEAM. CORRODED. UPPER FUSELAGE FLOOR STRUCTURE HEAVY AMOUNT OF CORROSION UNDER NUTLPLATE ON LOWER CHORD OF FLOORBEAM AT BS 787 AT RBL 24 - [SDR 7AHR2011092027](https://openairdocs.org/sdr/7AHR2011092027), Sep 23, 2011: BEAM. ELONGATED. DURING THE ACCOMPLISHMENT OF ECO 3731 SB 737-57A-1266 INSPECTION OF THE MAIN LANDING GEAR BEAM TO WING ATTACH FITTINGS IT WAS DISCOVERED THAT THE MLG BEAM PIN R - [SDR 7AHR2011092026](https://openairdocs.org/sdr/7AHR2011092026), Sep 23, 2011: SKIN. CORRODED. AFT FUSELAGE HAS EVIDENCE PILLOWING (CORROSION) AT BODY STA 1016 AT STR 25L AND 24L AROUND FASTENERS. - [SDR 7AHR2011092025](https://openairdocs.org/sdr/7AHR2011092025), Sep 23, 2011: FLOOR SUPPORT. CORRODED. AFT FUSELAGE CABIN FLOOR STURCTURE AT BODY STA 947 TO 967 AT LBL 12 HAS EVIDENCE OF CORROSION. - [SDR 7AHR2011092024](https://openairdocs.org/sdr/7AHR2011092024), Sep 23, 2011: FLOOR SUPPORT. CORRODED. AFT BAGAGGE COMPARTMENT FLOOR SUPPORTS AT BODY STATION 770 AT SPLICE STRAP ATTACHED HAS SIGNS OF CORROSION - [SDR 7AHR2011092023](https://openairdocs.org/sdr/7AHR2011092023), Sep 23, 2011: TRANSITION PANEL. CORRODED. AFT PIT TRANSITION PANEL CORRODED JUST AFT OF CARGO DOOR ON THE RT SIDE AT BODY STATION 887. - [SDR 7AHR2011092022](https://openairdocs.org/sdr/7AHR2011092022), Sep 23, 2011: SKIN. CORRODED. AFT FUISELAGE BODY STA 976.6 AT STRINGER 25L, EDGE OF WATER SERVICING DOOR HAS EVIDENCE OF CORROSION. - [SDR 7AHR2011092021](https://openairdocs.org/sdr/7AHR2011092021), Sep 23, 2011: STRINGER. CORRODED. AFT BAGGAGE COMPARTMENT AT BODY STA 947.6, STRINGER 26L, HAS CORROSION OUT OF LIMITS. - [SDR 7AHR2011092020](https://openairdocs.org/sdr/7AHR2011092020), Sep 23, 2011: INTERCOSTAL. CORRODED. AFT BAGGAGE COMPARTMENT INTERCOSTAL UPPER FLANGE CORRODED OUT OF LIMITS BETWEEN BODY STATION 767 AND 787 AT STRINGER 25R - [SDR 7AHR2011092019](https://openairdocs.org/sdr/7AHR2011092019), Sep 23, 2011: THRESHOLD. CORRODED. FORWARD FUSELAGE FLOOR STRUCTURE AT L1 DOOR CENTER THRESHOLD AREA HAS LIGHT CORROSION ON UPPER SURFACE STRUCTURE AND UNDER NUTPLATES - [SDR 7AHR2011092018](https://openairdocs.org/sdr/7AHR2011092018), Sep 23, 2011: FLOOR SUPPORT. CORRODED. FORWARD CABIN FLOOR STRUCTURE HAS CORROSION ON FLOOR SUPPORT AT LBL 6 BETWEEN BODY STATION 294.5 AND 312.0. - [SDR 7AHR2011092017](https://openairdocs.org/sdr/7AHR2011092017), Sep 23, 2011: FLOOR SUPPORT. CORRODED. AFT BAGGAGE COMPARTMENT FLOOR SUPPORT SPLICE PLATE HAS SIGNS OF CORROSION ON BOTTOM SIDE AT BODY STA 770. - [SDR 7AHR2011092016](https://openairdocs.org/sdr/7AHR2011092016), Sep 23, 2011: FLOOR SUPPORT. CORRODED. CORROSION UNDER TIE DOWN AT STRINGER 26R AT SHEAR TIE FLOORBOARD SUPPORT AT BODY STATION 384. - [SDR 7AHR2011092015](https://openairdocs.org/sdr/7AHR2011092015), Sep 23, 2011: FLOORBEAM. CORRODED. AFT FUSELAGE FLOOR STRUCTURE HAS CORROSION AT FLOOR SUPPORT BODY STA 957 BETWEEN RT SIDE OF SEAT TRACKS AT RBL 24 AND 45. - [SDR 7AHR2011092014](https://openairdocs.org/sdr/7AHR2011092014), Sep 23, 2011: FLOOR SUPPORT. CORRODED. AFT FUSELAGE FLOOR STRUCTURE AT LT LAVATORY WALL, FLOOR IS CORRODED AT BODY STATION 947 TO 967. - [SDR 7AHR2011092013](https://openairdocs.org/sdr/7AHR2011092013), Sep 23, 2011: SILL. CORRODED. FORWARD CABIN FLOOR STURCTURE AT BODY STATION 312 TO 344 AT MOP SILL HAS CORROSION AROUND FASTNER HOLES. - [SDR 7AHR2011092012](https://openairdocs.org/sdr/7AHR2011092012), Sep 23, 2011: FLOORBEAM. CORRODED. FORWARD CABIN FLOOR STRUCTURE (FRAME) HAS CORROSION AT BODY STA 312 BETWEEN RBL 24 AND RBL 45. - [SDR 7AHR2011092011](https://openairdocs.org/sdr/7AHR2011092011), Sep 23, 2011: SKIN. CRACKED. DURING THE ACCOMPLISHMENT OF ECO 3735, FORWARD ENTRY AND FORWARD GALLEY SERVICE DOORWAY UPPER AND LOWER HINGE CUTOUT INSPECTION, IT WAS DETERMINED THAT THE FORW - [SDR 7AHR2011092010](https://openairdocs.org/sdr/7AHR2011092010), Sep 22, 2011: SKIN. CORRODED. AFT PIT AT STATION 907 TO 929 AT STRINGER 26R HAS CORROSION AROUND FASTENER. FASTENERS ARE PULLING THROUGH. - [SDR 7AHR2011092009](https://openairdocs.org/sdr/7AHR2011092009), Sep 22, 2011: FLOOR SUPPORT. CORRODED. AFT FUSELAGE FLOOR STRUCTURE HAS CORROSION ON FLOOR SUPPORT AT BODY STATION 955 INBD OF SEAT TRACK AT RBL 24. - [SDR 7AHR2011092008](https://openairdocs.org/sdr/7AHR2011092008), Sep 22, 2011: FLOOR SUPPORT. CORRODED. AFT BAGGAGE COMPARTMENT FLOOR SUPORT AT RBL 8" HAS CORROSION THAT IS OUT OF LIMITS AT SPLICE STRAP BODY STA 770. - [SDR 7AHR2011092007](https://openairdocs.org/sdr/7AHR2011092007), Sep 22, 2011: SKIN. CORRODED. CORROSION AROUND FASTNERS AT LT LOWER SURFACE OF WING AT STATION WRL 167 BEHIND FUEL ACCESS PANEL NR 7204. - [SDR 7AHR2011092006](https://openairdocs.org/sdr/7AHR2011092006), Sep 22, 2011: FLOOR SUPPORT. CORRODED. AFT PIT FLOOR SUPPORT AT BODY STATION 770 HAS CORROSION AND WAS FOUND TO BE OUT OF LIMITS AT SPLICE STRAP - [SDR 7AHR2011092005](https://openairdocs.org/sdr/7AHR2011092005), Sep 22, 2011: ANGLE. CORRODED. AFT FUSELAGE FLOOR STRUCTURE AT AFT LAVATORY FORWARD WALL AS CORROSION AT ATTACH ANGLE AT INBD FASTENER HOLE. - [SDR 7AHR2011092004](https://openairdocs.org/sdr/7AHR2011092004), Sep 22, 2011: SKIN. CORRODED. PILLOWING CORROSION AROUND FASTENERS AT BODY STA 787, STRINGER 27R. - [SDR 7AHR2011092003](https://openairdocs.org/sdr/7AHR2011092003), Sep 22, 2011: STRUCTURE. CORRODED. CORROSION UNDER FLOORBOARD SPLICE AT STA 464 BETWEEN STRINGER 27R AND 26R IN FORWARD PIT. - [SDR 7AHR2011092001](https://openairdocs.org/sdr/7AHR2011092001), Sep 21, 2011: SKIN. CORRODED. FUSELAGE LOWER LOBE AT BODY STATION 807 TO 827 AT STRINGER 26R TO 27R HAS EVIDENCE OF PILLOWING (CORROSION). - [SDR 7AHR2011092002](https://openairdocs.org/sdr/7AHR2011092002), Sep 21, 2011: ACCESS PANEL. CORRODED. AFT FUSELAGE AT POTABLE WATER SERVICING PANEL HAS EVIDENCE OF CORROSION AROUND PANEL. - [SDR TSAA2011F00203](https://openairdocs.org/sdr/TSAA2011F00203), Sep 20, 2011: SKIN. CORRODED. FUSELAGE LOWER LOBE BETWEEN STA 827 AND 807 AT STRINGER 27R AND 26R HAS POSSIBLE PILLOWING AROUND FASTENERS (CORROSION). - [SDR TSAA1155006](https://openairdocs.org/sdr/TSAA1155006), May 11, 2011: SKIN. CRACKED. 2.5 INCH CRACK DISCOVERED AT BS 574 ABOVE STRINGER 18R. REPAIR COMPLIED WITH IAW SRM 53-30-3 DETAIL XI AND XIX FIGURE 48. - [SDR TSAA1126004](https://openairdocs.org/sdr/TSAA1126004), Apr 9, 2011: CONNECTOR. SHORTED. DURING CRUSE FLIGHT, THE CREW NOTED THE NR1 ENGINE OVERHEAT WARNING LIGHT ILLUMINATED. THE CONDITION WAS INTERMITTENT AND EXTINGUISHED. THE CREW RETURNED TO HNL - [SDR TSAA1012020](https://openairdocs.org/sdr/TSAA1012020), Dec 19, 2010: UNKNOWN. ODOR. NON-ETOPS CARGO FLIGHT 25. UPON ARRIVAL, AN ELECTRICAL ODOR WAS REPORTED BY THE PILOT IN THE COCKPIT. MX INSPECTED COCKPIT AND FOUND NO DEFECTS OR ODORS. MX INS - [SDR TSAA1053017](https://openairdocs.org/sdr/TSAA1053017), Oct 5, 2010: STIFFENER. CORRODED. WING CTR SECTION LOWER BEAM AT RBL 40.875 IS CORRODED AT BS 612 AND BS 630. MAINTENANCE ACTION: REPLACED ANGLE IN ACCORDANCE WITH SRM 51-10-1. CLEANED AND TREAT - [SDR TSAA1026012](https://openairdocs.org/sdr/TSAA1026012), Jun 15, 2010: CIRCUIT BREAKER. FAILED. DURING CLIMB, THE CREW NOTED THE NR 2 TRANSFER BUS CIRCUIT BREAKER POPPED. CREW ATTEMPTED TO RESET WITHOUT SUCCESS. CREW RETURNED TO DEPARTURE WITHOUT FURTHER I - [SDR TSAA1026011](https://openairdocs.org/sdr/TSAA1026011), Jun 14, 2010: RELAY. FAILED. NON-ETOPS CARGO FLIGHT 16. DURING CLIMB THE ACFT EXPERIENCED A NR2 BUS POWER FAILURE CAUSING THE LOSS OF USE OF ALL INSTRUMENTS AND SYS POWERED BY THE NR 2 BUS. - [SDR TSAA0977007](https://openairdocs.org/sdr/TSAA0977007), Jul 21, 2009: TRANSMITTER. DEFECTIVE. ON TAKEOFF, NR 1 EPR FROZE AT 1.14 WHILE SETTING TAKEOFF POWER. OTHER NR 1 INDICATIONS NORMAL. ABORTED TAKEOFF AT 70 KTS. RETURNED TO RAMP. MX: REMOVED AND REPL - [SDR TSAA0932003](https://openairdocs.org/sdr/TSAA0932003), Apr 16, 2009: UPLOCK SENSOR. DIRTY. FLT 11, HNL- LIH - NOSE GEAR RED LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO HNL. ALL THREE GREEN LIGHTS ILLUMINATED WHEN LANDING GEAR EXTENDED. FLIGHT TERMINA - [SDR TSAA0932002](https://openairdocs.org/sdr/TSAA0932002), Apr 2, 2009: CONTROL CABLE. OUT OF ADJUST. FLT 320: TEST FLIGHT, LANDING GEAR LEVER WOULD NOT GO UP AFTER TAKEOFF. WARNING HORN ON AFTER FLAP RETRACT. RETURNED TO SJO, UNEVENTFUL LANDING. PERFORMED ADJUS - [SDR TSAA0952001](https://openairdocs.org/sdr/TSAA0952001), Jan 21, 2009: SWITCH. OBSTRUCTED. FLT 952, HNL-ITO -ON TAKEOFF, THE AFT CARGO LIGHT CAME ON. RETURNED TO HNL, NO EMERGENCY. MAINTENANCE FOUND A STRAP LODGED BETWEEN THE DOOR AND SWITCH. REPOSITI - [SDR TSAA0827019](https://openairdocs.org/sdr/TSAA0827019), Apr 8, 2008: INDICATOR. FAILED. CARGO FLIGHT 940 HNL-KOA, ON DESCENT TO KOA, THE CREW WAS ONLY ABLE TO EXTEND THE FLAPS TO 8 UNITS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO HNL WITHOUT F - [SDR TSAA0877012](https://openairdocs.org/sdr/TSAA0877012), Mar 4, 2008: INDICATOR. FAILED. FLIGHT 269 HNL-LIH - AT TAKEOFF, THE CREW NOTED THE NR 1 EGT READ LOW AT APPROXIMATELY 250 DEGREES AND ELECTED TO ABORT THE TAKEOFF AT 90 KTS AIRSPEED. THE AIRC - [SDR TSAA0829008](https://openairdocs.org/sdr/TSAA0829008), Feb 15, 2008: HOSE. FAILED. NON-ETOPS FLIGHT 215 HNL-LIH, DURING CRUISE FLIGHT, THE CREW NOTED THE HYDRAULIC QUANTITY GAUGE DROPPED TO ZERO. CREW COMPLETED THE HYDRAULIC SYSTEM A FAILURE C - [SDR TSAA0734055](https://openairdocs.org/sdr/TSAA0734055), Oct 5, 2007: DADC. FAILED. NON-ETOPS CARGO FLIGHT 946 HNL-KOA - DURING CLIMB, THE CREW NOTED WARNING FLAGS IN THE FIRST OFFICER’S AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED INDICATO - [SDR TSAA0753052](https://openairdocs.org/sdr/TSAA0753052), Sep 20, 2007: SKIN. CRACKED. WHILE ACCOMPLISHING VISUAL INSPECTION DURING SERVICE CHECK, A CRACK WAS DISCOVERED AT BS 306 AT STR 18. MAINTENANCE ALONG WITH ENGINEERING IS RESEARCHING THE RE - [SDR TSAA0731036](https://openairdocs.org/sdr/TSAA0731036), Jun 25, 2007: ACCESSORY UNIT. FAILED. NON-ETOPS FLIGHT 226 HNL-OGG - WHEN THE CREW APPLIED TAKEOFF POWER, THE CONFIGURATION WARNING HORN SOUNDED. CREW ABORTED TAKE OFF AT 60 KNOTS INDICATED AIRSPEED All 121: https://openairdocs.org/deregistered/N826AL-2014-04-16/reports.md ## Other aircraft with N826AL - [Registered now](https://openairdocs.org/aircraft/N826AL): Zipline International P2 ZIP, S/N 18736P22574 --- 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.