# N841AL: 1984 Boeing 737-2X6C, registration cancelled 2014-10-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 8, 2014 - Status when cancelled: Sale reported - Airframe: [Boeing 737-2X6C](https://openairdocs.org/model/boeing-737-2x6c) (registry code 138447B) - 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: 23123 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 14, 1991 - Last registry action: July 21, 2014 - Mode S code: AB839B - Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage) - Owner type: Individual - Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N841AL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=841AL - Page: https://openairdocs.org/deregistered/N841AL-2014-10-08 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 737-2X6C: https://openairdocs.org/model/boeing-737-2x6c.md ## Service difficulty reports (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TSAA20140113001](https://openairdocs.org/sdr/TSAA20140113001), Jan 9, 2014: STRUCTURE. CORRODED. DURING A SCHEDULED A CHECK INSPECTION, AN AREA CORROSION DAMAGE 1.25 INCHES WIDE & 0.875 INCHES LONG & 0.060 INCHES DEEP WAS FOUND ON THE LT STABILIZER AT ELEVA - [SDR TSAA20130110001](https://openairdocs.org/sdr/TSAA20130110001), Jan 10, 2013: SKIN. CRACKED. DURING SERVICE CHECK FOUND AN APPROX 2" CRACK ON THE LT SIDE FUSELAGE AT BS 802, ABOVE STRINGER 18L. REPAIRED IAW SRM 53-30-3, FIG. 48. - [SDR TSAA20121001005](https://openairdocs.org/sdr/TSAA20121001005), Oct 1, 2012: SKIN. CRACKED. DURING SERVICE CHECK, FOUND AN APPROXIMATELY 2 INCH CRACK ON THE LT SIDE FUSELAGE AT BS 887, ABOVE STRINGER 17L. REPAIRED CRACK IAW SRM 53-30-3, FIG 48, DETAIL - [SDR 7AHR201205252279](https://openairdocs.org/sdr/7AHR201205252279), May 25, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT FUSELAGE BS 277 AT STRINGER 15R. REMOVED DAMAGED STRINGER CLIP IAW SRM 51-30-02. FABRICATED NEW STRINGER CLIP IAW SRM 51-30-06. INSTALL - [SDR 7AHR201205252294](https://openairdocs.org/sdr/7AHR201205252294), May 25, 2012: SKIN. CORRODED. LT HORIZONTAL STABILIZER UPPER SURFACE REAR SPAR HAS A BROKEN RIVET HEAD AND A BULGE IN SKIN AROUND BROKEN RIVET AT STABILIZER STATION 66.5. REMOVED T/E SKIN FA - [SDR 7AHR201205252210](https://openairdocs.org/sdr/7AHR201205252210), May 25, 2012: STRINGER SPLICE. CORRODED. CORROSION ON STRINGER SPLICE AT STA 907 AT STRINGER 26L. FOUND STRINGER SPLICE TO BE EXFOLIATED OUT OF LIMITS. REMOVED STRINGER SPLICE IAW SRM 51-30-2. FABRICAT - [SDR 7AHR201205252424](https://openairdocs.org/sdr/7AHR201205252424), May 25, 2012: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT STA 787 AND RBL 40 THROUGH 55. REMOVED CORROSION IAW SRM 51-30-2. FABRICATED FLOORBEAM REPAIR IAW ECO 53-04407-1. INSTALLED FABRICATED - [SDR 7AHR201205242306](https://openairdocs.org/sdr/7AHR201205242306), May 24, 2012: PLATE. GOUGED. NR 2 ENGINE CROSSBEAM LOWER INBD ENGINE TO WING FAIRING HAS GOUGES ON CROSSBEAM FACE. REMOVED DAMAGED PLATE FROM CROSSBEAM IAW 51-30-2. FABRICATED NEW PLATE IAW - [SDR 7AHR201205242207](https://openairdocs.org/sdr/7AHR201205242207), May 24, 2012: STRINGER. CORRODED. CORROSION AT BS 1016 AT AFT PRESSURE BULKHEAD AT STRINGER 24L. REMOVED STRINGER END FITTING AND ALSO FOUND END OF STRINGER WAS ALSO CORRODED. FABRICATED NEW STI - [SDR 7AHR201205242213](https://openairdocs.org/sdr/7AHR201205242213), May 24, 2012: SUPPORT. CRUSHED. BS 727 AT STRINGER 19R HORIZONTAL BULKHEAD PANEL SUPPORT FRAME IS CRUSHED IN AFT PIT. REMOVED HORIZONTAL BULKHEAD PANEL SUPPORT FRAME AT FUSELAGE STATION 727 IA - [SDR 7AHR201205292272](https://openairdocs.org/sdr/7AHR201205292272), May 24, 2012: SHEAR TIE. CORRODED. CORROSION AT FUSELAGE STA 400 AND STRINGER 26R, FUSELAGE FRAME. REMOVED CORRORED SHEAR TIE IAW SRM 51-30-02, FABRICATED AND ISTALLED A NEW SHEAR TIE IAW SRM 51- - [SDR 7AHR201205222468](https://openairdocs.org/sdr/7AHR201205222468), May 22, 2012: FAIRING. DAMAGED. NR 3 FLAP FAIRING FORWARD LOWER L/E IS DAMAGED. REPAIRED IAW SRM`S 51-30-2, & 51-40-3. - [SDR 7AHR201205222209](https://openairdocs.org/sdr/7AHR201205222209), May 22, 2012: STRINGER SPLICE. CORRODED. CORROSION AT FUSELAGE STA 907 AT STR 27L AT STRINGER SPLICE. REMOVED STRINGER SPLICE AND STRINGER CLIP DUE TO CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30- - [SDR 7AHR201205222466](https://openairdocs.org/sdr/7AHR201205222466), May 22, 2012: FRAME. CORRODED. AFT TAIL CONE ACCESS DOOR PANEL NR 3802 FRAME HAS CORRODED RIVET HEADS AND RUB PADS. REMOVED RIVETS AND RUB PADS FROM TAIL CONE ACCESS DOOR IAW SRM 51-30-2. FAB - [SDR 7AHR201205222074](https://openairdocs.org/sdr/7AHR201205222074), May 22, 2012: SKIN. MISREPAIRED. LOWER FUSELAGE PRESSURIZATION LEAK AT EXTERNAL REPAIR FWD EDGE AT STA 907 AT STRINGER 20L AT LAP SEAM AND BUTT SPLICE DOWN TO STR 25L LAP SEAM. REMOVED FASTENER - [SDR 7AHR38412A2073](https://openairdocs.org/sdr/7AHR38412A2073), May 22, 2012: SKIN. MISREPAIRED. LOWER FUSELAGE, PRESSURIZATION LEAK AT EXTERNAL REPAIR (APPROX 30 RIVETS) BELOW R-1 DOOR. STA 312 AT STRINGER 19R LAP SEAM. REMOVED FASTENERS AT LOWER FUSELAGE - [SDR TSAA1153010](https://openairdocs.org/sdr/TSAA1153010), Aug 24, 2011: SKIN. CRACKED. DURING SERVICE CHECK, FOUND A 2 INCH CRACK ON THE RT SIDE FUSELAGE AT BS 360+5.5, ABOVE STRINGER 15R. THE CRACK WAS REPAIRED IN ACCORDANCE WITH ECO 3826, SB 737 - [SDR TSAA1153005](https://openairdocs.org/sdr/TSAA1153005), Apr 10, 2011: SKIN. CRACKED. DURING THE DAILY SERVICE CHECK, A 2 IN CRACK AT BODY STA 259.5, 1 IN ABOVE STRINGER 16R WAS DISCOVERED DURING THE VISUAL CHECK OF THE FUSELAGE. THE CRACK WAS CO - [SDR TSAA1156003](https://openairdocs.org/sdr/TSAA1156003), Apr 3, 2011: WINDOW. CRACKED. NON-ETOPS FLIGHT 54 HNL-ITO. ON DESCENT, THE CAPTAIN’S NR 2 WINDOW OUTER PANE CRACKED. GLASS REMAINED INTACT AND THERE WAS NO LOSS OF PRESSURIZATION. CREW RETUR - [SDR TSAA1179002](https://openairdocs.org/sdr/TSAA1179002), Feb 18, 2011: OIL FILTER. SEPARATED. FLT 40. AFTER ADVANCING THE THROTTLES THE CREW NOTED THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATE FOLLOWED BY A DECREASE IN NR 2 ENGINE OIL QUANTITY. THE C - [SDR TSAA1027019](https://openairdocs.org/sdr/TSAA1027019), Nov 16, 2010: INDICATOR. FAILED. DURING CLIMB, THE CREW SELECTED FLAPS UP AND NOTED A SPLIT-FLAP INDICATION, WITH NO ROLL ENCOUNTERED. CREW ATTEMPTED TO SELECT FLAPS 1 WITH NO EFFECT. CREW DECL - [SDR EE4Y100357](https://openairdocs.org/sdr/EE4Y100357), Aug 19, 2010: STRUCTURE. CORRODED. FWD CARGO COMPARTMENT BULKHEAD BS 540 BTWN STR 22L AND 23L CHORD HORIZ FLANGE WITH CORROSION (THE CORROSION REQUIRES A MAJOR REPAIR). - [SDR EE4Y100340](https://openairdocs.org/sdr/EE4Y100340), Aug 17, 2010: STRINGER. CRACKED. TAIL COMPARTMENT, STA 1132, STRINGER 5 RIGHT WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR. - [SDR EE4Y100339](https://openairdocs.org/sdr/EE4Y100339), Aug 17, 2010: STRINGER. CRACKED. TAIL COMPARTMENT STA 1132 STRINGER 5 LT WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR. - [SDR EE4Y100338](https://openairdocs.org/sdr/EE4Y100338), Aug 17, 2010: BULKHEAD. CORRODED. LOWER FUSELAGE, FWD CARGO COMPARTMENT, STA 540 BULKHEAD BETWEEN STRINGER 22 LT AND 23 LT CHORD HORIZONTAL FLANGE WITH CORROSION. THE CORROSION REQUIRES A MAJOR - [SDR EE4Y100336](https://openairdocs.org/sdr/EE4Y100336), Aug 13, 2010: FLOORBEAM. CORRODED. UPPER FUSELAGE, FLOORBEAM LOWER FLANGE WITH CORROSION AT STA 847 BETWEEN RBL 42 AND RBL 59. THE CORROSION REQUIRES A MAJOR REPAIR. - [SDR EE4Y100335](https://openairdocs.org/sdr/EE4Y100335), Aug 13, 2010: FLOORBEAM. CORRODED. UPPER FUSELAGE, FLOORBEAM LOWER FLANGE WITH CORROSION AT STA 867 BETWEEN RBL 26 AND RBL 56. THE CORROSION REQUIRES A MAJOR REPAIR. - [SDR EE4Y100337](https://openairdocs.org/sdr/EE4Y100337), Aug 13, 2010: FLOORBEAM. CORRODED. UPPER FUSELAGE, FLOORBEAM WITH CORROSION AT UPPER FLANGE AT STA 344 BETWEEN LBL 43 & RBL 11. THE CORROSION REQUIRES MAJOR REPAIR. - [SDR EE4Y100334](https://openairdocs.org/sdr/EE4Y100334), Aug 12, 2010: BEAR STRAP. CRACKED. MAIN CARGO DOOR, FWD UPPER CORNER CUTOUT, FUSELAGE SKIN, BEAR STRAP WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR. - [SDR EE4Y100333](https://openairdocs.org/sdr/EE4Y100333), Aug 12, 2010: FLOORBEAM. CORRODED. UPPER FUSELAGE, BS 787 FLOORBEAM, LOWER FLANGE CORRODED. THE DAMAGE REQUIRES A MAJOR REPAIR. - [SDR EE4Y100332](https://openairdocs.org/sdr/EE4Y100332), Aug 11, 2010: BULKHEAD. DENTED. FUSELAGE BULKHEAD BS 1016, AFT FACE, WEB DENTED AT WBL 166, RBL 7. THE DENT REQUIRES A MAJOR REPAIR. - [SDR EE4Y100330](https://openairdocs.org/sdr/EE4Y100330), Aug 11, 2010: BEAR STRAP. CRACKED. UPPER FUSELAGE, FWD ENTRY DOOR, LOWER HINGE CUTOUT AT BS 304.5 WL 235, INTERNAL BEAR STRAP WITH CRACK. THE CRACK REQUIRES MAJOR REPAIR. - [SDR EE4Y100319](https://openairdocs.org/sdr/EE4Y100319), Aug 10, 2010: SPAR. CORRODED. RIGHT WING LEADING EDGE FRONT SPAR LOWER CHORD WITH CORROSION ON LOWER FLANGE. THE CORROSION REQUIRES A MAJOR REPAIR. - [SDR EE4Y100309](https://openairdocs.org/sdr/EE4Y100309), Aug 9, 2010: SKIN PANEL. DENTED. LOWER EXTERNAL FUSELAGE AT BS 727A+6.25 BETWEEN STR 22R AND STR 23R SKIN WITH DENT. THE DENT REQUIRES MAJOR REPAIR. - [SDR EE4Y100264](https://openairdocs.org/sdr/EE4Y100264), Aug 5, 2010: SKIN PANEL. DENTED. LOWER FUSELAGE, AT BS 727+12.5 BETWEEN STRINGER 20 RT AND STRINGER 21 RT SKIN WITH DENT. THE DENT REQUIRES MAJOR REPAIR. - [SDR TSAA1053008](https://openairdocs.org/sdr/TSAA1053008), Apr 26, 2010: STRINGER. CRACKED. DISCOVERED 1" CRACK DURING SCHEDULED INSP AT BS 492.4, S-22R (AFT SIDE OF FWD CARGO DOOR CUTOUT FWD END OF STRINGER). R & R STRINGER ASSY IAW SRM 53-10-3, FIG 1 - [SDR TSAA1027006](https://openairdocs.org/sdr/TSAA1027006), Mar 17, 2010: PROXIMITY SENSOR. FAILED. DURING CLIMB, AFTER THE FLAPS WERE RETRACTED, THE FLIGHT CREW NOTED THE LE FLAPS TRANSIT ANNUNCIATOR REMAINED ILLUMINATED. CREW ACCOMPLISHED THE QRH PROCEDURES - [SDR TSAA1026002](https://openairdocs.org/sdr/TSAA1026002), Jan 19, 2010: FIRE DETECTOR. FALSE ACTIVATION. NON-ETOPS. DURING CLIMB THE CREW NOTED A FIRE INDICATION ON THE NR 2 ENG. CREW ACCOMPLISHED ALL RELATED QRH AND CHECKLIST PROCEDURES AND SHUTDOWN THE NR 2 ENGIN - [SDR TSAA1077001](https://openairdocs.org/sdr/TSAA1077001), Jan 11, 2010: DUCT. CRACKED. FLT NR 58 (HNL ITO)- ON CLIMB OUT, NR 1 ENG FIRE WARNING LIGHT STARTED TO FLICKER AND BELL STARTED TO RING. PULLED BACK TO IDLE CONTINUED TO FLY AT IDLE, LIGHT - [SDR TSAA0953011](https://openairdocs.org/sdr/TSAA0953011), Nov 23, 2009: SKIN. CRACKED. DURING SCHEDULED INSP A 3" CRACK WAS DISCOVERED AT BS 440, 450, S-16R FUSELAGE SKIN. REPAIRED SKIN BY REMOVING CRACK DEFECT, CONDUCTED HFEC INSP, ENLARGED TRIM - [SDR TSAA0932009](https://openairdocs.org/sdr/TSAA0932009), Sep 2, 2009: SHUTOFF VALVE. INOPERATIVE. ON TAXI-OUT, THE "ANTI-SKID INOP" LIGHT ILLUMINATED AND THE "FAIL WARN AND PARK BRAKE" CIRCUIT BREAKER POPPED. RETURNED TO RAMP. MX REMOVED AND REPLACED THE PAR - [SDR TSAA0926005](https://openairdocs.org/sdr/TSAA0926005), Jun 26, 2009: FIRE LOOP. MALFUNCTIONED. FLT 42, ENG NR 1 (OVERHEAT WARN) LIGHT FLICKERING DURING TAXI. RETURNED TO BLOCK. TRIED FIRE CONTROL MODULE, FIRE DETECTION UNIT AND DISCONNECTED NR1 ENG FIREWA - [SDR TSAA0879020](https://openairdocs.org/sdr/TSAA0879020), Jun 10, 2008: TRANSMITTER. FAILED. FLIGHT 913 HNL-LIH. DURING TAKEOFF, THE NR 2 ENGINE OIL QUANTITY DECREASED. ELECTED TO ABORT TAKEOFF. INDICATIONS RETURNED TO NORMAL DURING ABORT; ALL ENGINE PA - [SDR TSAA0721065](https://openairdocs.org/sdr/TSAA0721065), Dec 14, 2007: CONTROLLER. MALFUNCTIONED. FLIGHT 48 HNL-ITO - DURING CLIMB THE CREW NOTED THE RIGHT SUPPLY DUCT PRESSURE READING 100 PSI (FULL SCALE). THE CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MA - [SDR TSAA0731057](https://openairdocs.org/sdr/TSAA0731057), Oct 15, 2007: FDAU. FAILED. NON-ETOPS FLIGHT 278 HNL-KOA, AT 5000 FT, THE CREW NOTED THE FLIGHT RECORDER OFF LIGHT ILLUMINATED. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENAN - [SDR TSAA0732044](https://openairdocs.org/sdr/TSAA0732044), Aug 5, 2007: SWITCH. FAILED. NON-ETOPS FLIGHT 62 HNL - OGG - DURING CLIMB-OUT OF HNL, THE CREW REPORTED THE LANDING GEAR HANDLE STAYED IN THE DOWN POSITION WHEN THEY ATTEMPTED TO RAISE IT T ## Other aircraft with N841AL - [Registered now](https://openairdocs.org/aircraft/N841AL): Ceres Air C31, S/N 2157854070302 --- 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.