# N842AL: 1984 Boeing 737-290C, registration cancelled 2017-08-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 16, 2017 - Status when cancelled: Third renewal notice - Airframe: [Boeing 737-290C](https://openairdocs.org/model/boeing-737-290c) (registry code 138448V) - 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: 23136 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 15, 1984 - Certificate issued: October 28, 2013 - Last registry action: October 28, 2013 - Mode S code: AB8752 - Owners when cancelled: [Aeko Kula Inc DBA](https://openairdocs.org/faa-owner/AEKO%20KULA%20INC%20DBA), [Aloha Air Cargo](https://openairdocs.org/faa-owner/ALOHA%20AIR%20CARGO) - Location: [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu) - Owner type: Corporation - Owner's area on the map: 21.3477° N, 157.8767° W: Placed by OpenAirDocs at the center of ZIP code 96819, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N842AL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=842AL - Page: https://openairdocs.org/deregistered/N842AL-2017-08-16 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 737-290C: https://openairdocs.org/model/boeing-737-290c.md ## Service difficulty reports (79, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TSAA20141128048](https://openairdocs.org/sdr/TSAA20141128048), Nov 25, 2014: SKIN. CRACKED. DISCOVERED 1.25 INCH SKIN CRACK APPROX 2 INCHES FWD OF BS 540 BETWEEN STRINGER 1 & 2L. REPAIRED IAW SRM 53-30-3 FIG 48 DETAIL XXIII PROCEDURE III & VII. - [SDR TSAA20141010009](https://openairdocs.org/sdr/TSAA20141010009), Oct 10, 2014: CONTROL UNIT. FAULTY. APU AUTO SHUTDOWN DUE TO OVERSPEED DURING FLIGHT, EMER DECLARED. ADJUSTED APU ENG SPEED IAW AMM 49-11-00. R & R APU CONTROL UNIT IAW 49-61-11. R & R ELECTRONIC - [SDR TSAA20140722005](https://openairdocs.org/sdr/TSAA20140722005), Jul 22, 2014: UNKNOWN. CRACKED. 1.5 INCH CRACK AT BS 767 STRINGER 19L. REPAIRED IAW ENGINEERING. - [SDR TSAA20140601004](https://openairdocs.org/sdr/TSAA20140601004), Jun 1, 2014: SKIN. CRACKED. SKIN HAS A CRACK INDICATION AT BS 312 BELOW STRINGER 19R. REPAIRED FUSELAGE IAW SRM 53-30-3 FIGURE 48. - [SDR 7AHR20130130001](https://openairdocs.org/sdr/7AHR20130130001), Jan 30, 2013: SKIN. CORRODED. FUSELAGE SKIN AT BS 1121, AT STRINGER 20R HAS FASTENERS PULLING THROUGH SKIN LOCATED ABOVE APU ACCESS DOOR CUT OUT. AFTER REMOVAL OF FASTENERS IT WAS DETERMINED - [SDR 7AHR20130129014](https://openairdocs.org/sdr/7AHR20130129014), Jan 29, 2013: SKIN. WORN. RT ENGINE COWL WORN. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON THE RT ENGINE COWL IAW SRM 51-40-3. - [SDR 7AHR20130129013](https://openairdocs.org/sdr/7AHR20130129013), Jan 29, 2013: RIB. WORN. RT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 11 RIB. AREA OF DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGE AND WORN PARTS (ANGLE) IAW SRM 51-30 - [SDR 7AHR20130129012](https://openairdocs.org/sdr/7AHR20130129012), Jan 29, 2013: RIB. WORN. RT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 10 RIB. AREA OF DAMAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGED PARTS (ANGLES). FABRICATED NEW R - [SDR 7AHR20130129011](https://openairdocs.org/sdr/7AHR20130129011), Jan 29, 2013: RIB. WORN. RT ENGINE COWL HAS AREA OF DAMAGE, AREA NR 7 RIB. REMOVED DAMAGE RIB ANGLE IAW SRM 51-40-3. FABRICATED NEW REPAIR ANGLE IAW SRM 51-40-3. INSTALLED NEW REPAIR AN - [SDR 7AHR20130129010](https://openairdocs.org/sdr/7AHR20130129010), Jan 29, 2013: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL AT BS 727A AND 727B AT STRINGER 27L AND 27R. REMOVED INTERCOSTALS AT STRINGER 27L & 27R SRM 51-30-02, UPON FURTHER EVALUATION BOTH INTE - [SDR 7AHR20130129009](https://openairdocs.org/sdr/7AHR20130129009), Jan 29, 2013: SHEAR TIE. CORRODED. CORROSION IN AFT CARGO BS 767 STRINGER 27L TO 27R AT AFT FRAME, SHEAR TIES. REMOVED FASTENERS FOR ACCESS TO CORROSION IAW SRM 51-30-2. CORROSION AT SHEAR TIE IS - [SDR 7AHR20130129008](https://openairdocs.org/sdr/7AHR20130129008), Jan 29, 2013: SHEAR TIE. CORRODED. EXTERIOR FUSELAGE BELLY, SKIN BULGE AROUND FASTENERS BETWEEN STRINGER 27L AND 27R. REMOVED FASTENERS AT EXTERIOR FUSELAGE SKIN AT BS 747 BETWEEN STRINGER 27L & - [SDR 7AHR20130129007](https://openairdocs.org/sdr/7AHR20130129007), Jan 29, 2013: STRAP. WORN. NR 2 ENGINE UPPER FIXED COWL HAS A CHAFED STRAP. RUB STRAP DOUBLER FOUND TO BE WORN BEYOUD LIMITS IAW SRM 54-10-1. FABRICATED REPAIR PARTS IAW SRM 51-20-1. INST - [SDR 7AHR20130129006](https://openairdocs.org/sdr/7AHR20130129006), Jan 29, 2013: SKIN. CORRODED. EXTERIOR FUSELAGE BELLY SKIN, BULGE AROUND FASTENERS AT BS 727B BETWEEN STRINGER 27L AND 27R. REMOVED FASTENERS AT EXT FUSELAGE AT BS 727B, DICOVERED FRAME BETW - [SDR 7AHR20130129005](https://openairdocs.org/sdr/7AHR20130129005), Jan 29, 2013: SHEAR TIE. CORRODED. LOWER FUESLAGE E/E BAY CORROSION ON SHEAR TIE ANGLE AT BS 312 AT STRINGER 27L, FORWARD OF ACCESS DOOR. REMOVED CORRODED SHEAR TIE ATTACH ANGLE IAW SRM 51-30-2. - [SDR 7AHR20130129004](https://openairdocs.org/sdr/7AHR20130129004), Jan 29, 2013: SHIM. CORRODED. EXTERIOR FUSELAGE, EXTERNAL POWER RECEPTACLE ACCESS DOOR HAS CORRODED SHIMS BENEATH LATCHES ALONG WITH CORRODED HARDWARE. REMOVED CORRODED SHIMS AND HARDWARE, F - [SDR 7AHR20130129003](https://openairdocs.org/sdr/7AHR20130129003), Jan 29, 2013: FLOOR SUPPORT. CORRODED. FORWARD PIT STATION 385 AT RBL 14 CARGO FLOOR SUPPORT IS CORRODED. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-1. CORROSION WAS FOUND TO BE OUT OF LIMITS. - [SDR 7AHR20130129002](https://openairdocs.org/sdr/7AHR20130129002), Jan 29, 2013: ATTACH ANGLE. CRACKED. MAIN CABIN, LT LOWER AFT BULKHEAD SIDE WALL ATTACH ANGLE CRACKED IN 4 PLACES. FABRICATED REPAIR ANGLE FROM MATERIAL 2024 T3 IAW SRM 51-20-1. - [SDR 7AHR20130129001](https://openairdocs.org/sdr/7AHR20130129001), Jan 29, 2013: FLOORBOARD. CORRODED. FORWARD PIT FLOORBOARD SPLICE BETWEEN NR 1 AND NR 2 FLOORBOARD IS CORRODED AND MISSING NUT PLATES. FORWARD PIT FLOORBOARD SPLICE FOUND TO BE OUT OF LIMITS. FABR - [SDR 7AHR2011030803](https://openairdocs.org/sdr/7AHR2011030803), Mar 8, 2011: SKIN. DENTED. A DENT WAS FOUND ON THE RT HORIZ STABILIZER LOWER SURFACE BETWEEN STABILIZER STA 120.0 AND 129.0 JUST FORWARD OF THE REAR SPAR. A/Y RATIO DETERMINED THE DENT WA - [SDR 7AHR2011021802](https://openairdocs.org/sdr/7AHR2011021802), Feb 18, 2011: STRINGER. CORRODED. DURING C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 19 LT AT BODY STA 294.5. A 16 IN SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE W - [SDR 7AHR2011021801](https://openairdocs.org/sdr/7AHR2011021801), Feb 18, 2011: STRINGER. CORRODED. DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 22 LT AT FUSELAGE BODY STA 344. A 20 IN SECTION OF STR WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMA - [SDR 2011F00035](https://openairdocs.org/sdr/2011F00035), Feb 11, 2011: STRINGER. CORRODED. DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 22 LT AT FUSELAGE BODY STA 344. A 20 INCH SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO OTH - [SDR 2011F00034](https://openairdocs.org/sdr/2011F00034), Feb 11, 2011: STRINGER. CORRODED. DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 19 LT AT FUSELAGE BODY STA 294.5. A 16 INCH SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO O - [SDR TSAA1031010](https://openairdocs.org/sdr/TSAA1031010), Jun 10, 2010: WARNING HORN. ACTIVATED. NON-ETOPS CARGO FLIGHT. TAKEOFF WARNING HORN SOUNDED AT THROTTLE UP FOR TAKEOFF. CREW ABORTED TAKEOFF AT 10 KTS. CREW FOUND THE SPEED BRAKE LEVER WAS NOT COMPLE - [SDR TSAA1077009](https://openairdocs.org/sdr/TSAA1077009), May 25, 2010: BULKHEAD. CRACKED. A SCHEDULED INSPECTION REVEALED A CRACK AT THE 1ST RIVET AT BS 1016 AFT PRESSURE BULKHEAD AT THE WEB DOME SECTION ALONG STIFFENER/ STR-17L. TRIMMED DOME WEBS ON - [SDR TSAA1077004](https://openairdocs.org/sdr/TSAA1077004), Feb 17, 2010: TRANSMITTER. INOPERATIVE. ABORTED TAKEOFF, WHEN ADVANCING POWER FOR TAKEOFF NR 1 EPR MOVED SLOWLY AND ONLY WENT TO 1.50. ON TAXI BACK NR 1 EPR WOULD NOT MOVE. R & R NR1 ENGINE EPR TRANSM - [SDR TSAA1026003](https://openairdocs.org/sdr/TSAA1026003), Feb 9, 2010: BULB. INOPERATIVE. DURING APPROACH AFT CARGO COMPARTMENT SMOKE LIGHT ILLUMINATED. R & R AFT CARGO SMOKE DETECTOR BULB ASSY. OPS CK OK IAW AMM 26-16-00. - [SDR TSAA0926013](https://openairdocs.org/sdr/TSAA0926013), Dec 7, 2009: CONTROL PANEL. FAILED. NON-ETOPS CARGO FLIGHT. AFTER TAKEOFF PWR WAS SELECTED, OVERHEAT/FIRE ANNUNCIATOR LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE CREW RETURNED THE ACFT TO FREIG - [SDR TSAA0975015](https://openairdocs.org/sdr/TSAA0975015), Dec 6, 2009: DUCT. FAILED. NON-ETOPS CARGO FLIGHT, DURING CLIMB, THE CREW NOTED THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATE. NR1 ENGINE EGT REMAINED WITHIN LIMITS. THE NR 1 THROTTLE WAS RET - [SDR EE4Y090186](https://openairdocs.org/sdr/EE4Y090186), Jul 7, 2009: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE, CARGO CABIN AT BS 660 RBL 50 FLOOR SUPPORT CORRODED. - [SDR EE4Y090185](https://openairdocs.org/sdr/EE4Y090185), Jul 1, 2009: STRINGER. CRACKED. FUSELAGE TAIL CONE BETWEEN BS 1138 AND BS 1142 STR 5A LT, CRACKED. - [SDR EE4Y090184](https://openairdocs.org/sdr/EE4Y090184), Jun 30, 2009: STRINGER. CRACKED. UPPER FUSELAGE CARGO CABIN, LAVATORY AREA BS 303 STR 14L, CRACKED. - [SDR EE4Y090183](https://openairdocs.org/sdr/EE4Y090183), Jun 30, 2009: STRINGER CLIP. CRACKED. UPPER FUSELAGE CARGO CABIN AT BS 663 STR 10L CLIP CRACKED. - [SDR EE4Y090181](https://openairdocs.org/sdr/EE4Y090181), Jun 30, 2009: FRAME. DAMAGED. LOWER FUSELAGE AT BS 219.8, RBL 17.5 FRAME OTBD CHORD DRILLED. - [SDR EE4Y090179](https://openairdocs.org/sdr/EE4Y090179), Jun 30, 2009: STRINGER CLIP. CRACKED. UPPER FUSELAGE CARGO CABIN AT BS 747 STR 5R CLIP CRACKED. - [SDR EE4Y090178](https://openairdocs.org/sdr/EE4Y090178), Jun 30, 2009: SKIN. SCRATCHED. LWR FUSELAGE AT BS 227.8, RBL 17.5, SKIN SCRATCHED. - [SDR EE4Y090163](https://openairdocs.org/sdr/EE4Y090163), Jun 30, 2009: STRINGER. CRACKED. UPPER FUSELAGE CARGO CABIN AT BS 503, STR 8L, CRACKED. - [SDR EE4Y090147A](https://openairdocs.org/sdr/EE4Y090147A), Jun 30, 2009: STRINGER CLIP. CRACKED. UPPER FUSELAGE,CARGO CABIN AT BS 685 STR 6L, STRINGER CLIP CRACKED. - [SDR EE4Y090174](https://openairdocs.org/sdr/EE4Y090174), Jun 22, 2009: STRINGER. DAMAGED. LOWER FUSELAGE E&E COMPARTMENT,BETWEEN BS 355 AND BS 365,STR 19R WITH DOUBLE HOLE. - [SDR EE4Y090177](https://openairdocs.org/sdr/EE4Y090177), Jun 22, 2009: WEB. CRACKED. LOWER FUSELAGE, NOSE WHEEL WELL AT BS 250, RBL 2" UPPER WEB CRACKED. - [SDR EE4Y090175](https://openairdocs.org/sdr/EE4Y090175), Jun 22, 2009: SHEAR TIE. CRACKED. LOWER FUSELAGE E AND E AT BS 360 BETWEEN STR18R AND 19R, SHEAR TIE CRACKED. - [SDR EE4Y090173](https://openairdocs.org/sdr/EE4Y090173), Jun 22, 2009: ANGLE. CRACKED. LOWER FUSELAGE BS 1040 STR 21 ANGLE CRACKED. - [SDR EE4Y090172](https://openairdocs.org/sdr/EE4Y090172), Jun 22, 2009: SKIN. SCRATCHED. LOWER FUSELAGE AT BS 875.5 STR 17R SKIN WITH SCRATCH. - [SDR EE4Y090171](https://openairdocs.org/sdr/EE4Y090171), Jun 22, 2009: STRINGER. CORRODED. LOWER FUSELAGE AT STA 1016 STR 24L END FITTING CORRODED. - [SDR EE4Y090170](https://openairdocs.org/sdr/EE4Y090170), Jun 22, 2009: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE CARGO CABIN FROM BS 540 TO BS 685, RBL 25 TRANSVERSAL BEAM UPPER FLANGE CORRODED. - [SDR EE4Y090169](https://openairdocs.org/sdr/EE4Y090169), Jun 22, 2009: SHEAR TIE. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT BS 380 BETWEEN STR 19 AND MAIN CARGO DOOR CUTOUT, SHEAR TIE CRACKED. - [SDR EE4Y090168](https://openairdocs.org/sdr/EE4Y090168), Jun 22, 2009: SKIN. CORRODED. LOWER FUSELAGE ST BS 500 BETWEEN STR 27R AND 28R,SKIN CORRODED - [SDR EE4Y090167](https://openairdocs.org/sdr/EE4Y090167), Jun 20, 2009: SKIN. CANNING. LOWER FUSELAGE AT BS 973, BETWEEN STR 21L AND 22L, SKIN OIL CANNING. - [SDR EE4Y090166](https://openairdocs.org/sdr/EE4Y090166), Jun 20, 2009: SKIN. CANNING. LOWER FUSELAGE AT BS 963 BETWEEN STR 21L AND 22L, SKIN OIL CANNING. All 79: https://openairdocs.org/deregistered/N842AL-2017-08-16/reports.md ## Other aircraft with N842AL - [Registered now](https://openairdocs.org/aircraft/N842AL): Talos Drones TALOS T60X, S/N 2104F7EZW25990010XE1 --- 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.