# N536DA: 1980 Boeing 727-232, registration cancelled 2010-07-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 20, 2010 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22049 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 2, 1980 - Certificate issued: June 29, 2004 - Last registry action: June 15, 2010 - Mode S code: A6C703 - Owner when cancelled: [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC) - Location: [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul) - Owner type: Corporation - Owner's area on the map: 38.5420° N, 95.1245° W: Placed by OpenAirDocs at the center of ZIP code 66079, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N536DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=536DA - Page: https://openairdocs.org/deregistered/N536DA-2010-07-20 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 727-232: https://openairdocs.org/model/boeing-727-232.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL72S010865](https://openairdocs.org/sdr/DL72S010865), May 29, 2001: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN INOP ACROSS FROM ROW 32. RELAMPED EMERGENCY EXIT SIGN. - [SDR DL72S010260](https://openairdocs.org/sdr/DL72S010260), Feb 14, 2001: ENGINE. INTERMITTENT. NR 1 ENG FILTER BY PASS LIGHT ILLUMINATED ON TAKEOFF ROLL AT 100 KTS. RETURNED TO BLOCKS. INSP AND REPLACED NR 1 ENG MAIN OIL SCREEN. FWD FILTER BY PASS LIGHT T - [SDR DL72S001547](https://openairdocs.org/sdr/DL72S001547), Aug 11, 2000: SPAR. CRACKED. THE RT ELEVATOR WAS FOUND WITH A .25 INCH CRACK IN THE REAR SPAR EMANATING FROM THE EDGE OF A SHEAR PLATE. THE CRACK IS TYPICAL OF BAC S/B 727-55-0089. HOWEVER, - [SDR DL72S001383](https://openairdocs.org/sdr/DL72S001383), Jul 21, 2000: LIGHT. INOPERATIVE. OVERHEAD EMERGENCY LIGHT INOP AT STA 680. REPLACED LIGHT ASSY, OPS NORMAL. - [SDR DL72S000966](https://openairdocs.org/sdr/DL72S000966), May 15, 2000: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 26L SKIN LAP JOINT BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC CONFIRMED CR - [SDR DL72S000842](https://openairdocs.org/sdr/DL72S000842), Apr 28, 2000: POWER SUPPLY. INOPERATIVE. DURING CHECK OF THE EMERGENCY LIGHT SYSTEM, ROWS AFT OF 26 AND THE LT, RT AND AFT DOOR WERE INOP. FOUND AFT POWER SUPPLY BAD. REPLACED THE POWER SUPPLY, OPS CHE - [SDR DL72S000644](https://openairdocs.org/sdr/DL72S000644), Apr 5, 2000: PANEL. MISSING. FWD BLOW OUT PANEL ON RT SIDE OF NR 2 ENG COWL MISSING. REPLACED BLOW OUT PANEL, NO DUCT LEAKS NOTED ON ENG RUN. - [SDR DL72S000187](https://openairdocs.org/sdr/DL72S000187), Jan 25, 2000: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED A CRACK IN THE LOWER FASTENER ROW. INTERNAL MFEC INSPECTION CONFIRMED THREE C - [SDR DL72S991416](https://openairdocs.org/sdr/DL72S991416), Jun 23, 1999: TRACK. CORROSION. CORROSION WAS DISCOVERED IN THE TWO BOLT HOLES WHERE THE I/B FLAP O/B FLAP TRACK ATTACHES TO THE SPOILER SUPPORT LWR CHORD. REWORKED PER ERA 333256-14, REV A. - [SDR DL72S991415](https://openairdocs.org/sdr/DL72S991415), Jun 23, 1999: FITTING. CORRODED. RHS BOLT HOLES FOR THE VERT FIN FITTING ATTACH TO TENSION TIE RIB WAS FOUND WITH CORROSION. REWORKED PER ERA 333260-14, REV B. - [SDR DL72S991407](https://openairdocs.org/sdr/DL72S991407), Jun 21, 1999: FRAME. CRACKED. DURING ACCOMPLISHMENT OF INSPECTIONS OF THE OVERWING EXIT FRAMES, UNIDENTIFIED REPAIRS WERE NOTED. THE SUBJECT ERA WILL EVALUATE THE REPAIRS AND ENSURE COMPLIAN - [SDR DL72S991360](https://openairdocs.org/sdr/DL72S991360), Jun 16, 1999: FRAME. CRACKED. FRAME AT BS 620 WAS FOUND CRACKED REMOVAL OF THE CRACK REQUIRED REMOVAL OF APPROX 5 OF THE UPPER FLANGE FROM THE PRODUCTION SPLICE AT RBL 11 INBD TO RBL 6. REPA - [SDR DL72S991359](https://openairdocs.org/sdr/DL72S991359), Jun 16, 1999: SKIN. GOUGED. GOUGE FOUND IN FUSELAGE SKIN AT AFT EDGE OF THE C2 DOOR AT BS 990. DAMAGE AREA IS LOCATED AT S24R PLUS 5 AND IN THE SKIN ONLY. REPAIRED PER ERA 333244-14, REV A - [SDR DL72S990745](https://openairdocs.org/sdr/DL72S990745), Apr 3, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION - [SDR DL72S990408](https://openairdocs.org/sdr/DL72S990408), Feb 26, 1999: LIGHT. INOP. L1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS NOW OK. - [SDR DL72S982252](https://openairdocs.org/sdr/DL72S982252), Oct 31, 1998: COFFEEMAKER. FAILED. INDICATION OF SMOKE OBSERVED BY FLT ATTEND IN AFT GALLEY AND AFT CABIN. REPLACED COFFEEMAKER AND CANNON PLUG. - [SDR DL72S982241](https://openairdocs.org/sdr/DL72S982241), Oct 31, 1998: CONNECTOR. SHORTED. SMOKE IN AFT CABIN. FOUND THE CANNON PLUG FOR THE NR 3 COFFEEMAKER IN THE AFT GALLY SHORTED. PULLED AND COLLARD C/B, DISCONNECTED CANNON PLUG FROM COFFEEMAKER. - [SDR DL72S981541](https://openairdocs.org/sdr/DL72S981541), Jul 20, 1998: WIRE. BROKEN. THE FWD EMER EXIT SIGN IN THE COACH CABIN INOP. FOUND BROKEN GRD WIRE AT C/P FOR LIGHT ON LIGHT SIDE. REPAIRED WIRE, EMER LIGHTS CK OK. - [SDR DL72S980690](https://openairdocs.org/sdr/DL72S980690), Mar 30, 1998: BRACKET. CRACKED. FOUND ON D1 LETTER CK, NR 2 L/E FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER RADIUS. REPAIRED PER MM 57-20-21. - [SDR DL72S980689](https://openairdocs.org/sdr/DL72S980689), Mar 30, 1998: WEB. CRACKED. FOUND ON D1 LETTER CK, LT VERT TORQUE BOX WEB CRACKED AT UPPER END AT STA 1237 LT. REPAIRED PER MM 53-11-0. - [SDR DL72S980673](https://openairdocs.org/sdr/DL72S980673), Mar 27, 1998: INDICATOR. SHORTED. AT FL 310 HAD STRONG ELECT SMELL LIKE PLASTIC BURNING. INDICATOR LTS MASTER SECT 1 C/B POPPED. ODOR SLOWLY SUBSIDED, FOUND COCKPIT INDICATOR SHORTING TO GROUND. - [SDR DL72S972645](https://openairdocs.org/sdr/DL72S972645), Dec 10, 1997: STRUCTURE. DAMAGED. FUSELAGE, SKIN, FRAME, AND STRINGER FS228-252, S24R. REPAIR FOR DENTED AND CRACKED SKIN, STRINGERS, AND FRAMES. THE FUSELAGE SKIN BETWEEN FS 228 AND 252 AT S-24 - [SDR DL72S971692](https://openairdocs.org/sdr/DL72S971692), Aug 28, 1997: STRINGER. CRACKED. 1.25 INCH CRACK IN VERT STAB S-9R AND SECOND BULKHEAD ABOVE CRAWL WAY OPENING. REPAIRED PER MM 55-30-0 PG 803. - [SDR DL72S970112](https://openairdocs.org/sdr/DL72S970112), Jan 20, 1997: FRAME. CRACKED. A .375 INCH VISIBLE CRACK IN MLG UPLOCK FRAME OUTB'D FLANGE STA 913.5 UPPER END OF RADIUS BLOCK. INSTALLED REPAIR PER MM 53-11-0 PG 834. - [SDR DL72S970110](https://openairdocs.org/sdr/DL72S970110), Jan 20, 1997: SKIN. CRACKED. FOUND DURING C-1 LETTER CHECK, 4.5 INCH CRACK LEFT ELEVATOR LWR SKIN AT O/B END. REPAIRED PER SRM 55-20-3. - [SDR DL72S961515](https://openairdocs.org/sdr/DL72S961515), Jun 24, 1996: WEB. CRACKED. A 1.25 IN CRACK IN TORQUE BOX WEB UPPER RT CORNER AT STA 1213 AT UPPER CORD. INSTALLED DOUBLER PER MM 53-11-0 PG 832. - [SDR DL72S960174](https://openairdocs.org/sdr/DL72S960174), Jan 24, 1996: SPAR. CRACKED. DURING SHOP INSPECTION FOR WING SLAT PANEL, FOUND LEADING EDGE SPAR HAD A TEMPORARY REPAIR. REPAIRED SPAR PER MM 7-54-0 FIG 802 A. - [SDR DL72S960173](https://openairdocs.org/sdr/DL72S960173), Jan 23, 1996: BALLAST. FAILED. CEILING POWER FWD C/B ON P18-3 PNL POPPED FOLLOWED BY AN ACRID ELECTRICAL SMELL IN THE FWD PART OF THE AIRCRAFT. PULLED AND COLLARED FWD CONT C/B AND FWD CEILIN - [SDR DL72S954668](https://openairdocs.org/sdr/DL72S954668), Dec 7, 1995: MASK. POPPED INDICATOR. DURING INSPECTION, FOUND FWD CABIN PBE WITH POPPED INDICATOR. REPLACED PBE. - [SDR DL72S954476](https://openairdocs.org/sdr/DL72S954476), Nov 22, 1995: ANGLE. CRACKED. FOUND DURING B-1 LETTER CHECK, NR 5 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED .25 INCH AT O/B END. REPAIRED PER M/M 57-54-0 PAR 5A. - [SDR DL72S954475](https://openairdocs.org/sdr/DL72S954475), Nov 22, 1995: ACTUATOR MOUNT. CRACKED. FOUND DURING B-1 LETTER CHECK, NR 7 L/E SLAT ACTUATOR MOUNT FITTING CRACKED 1 INCH AT LWR I/B MOUNT BOLT. REPAIRED PER M/M 57-42-0 PAR 5. - [SDR DL72S954473](https://openairdocs.org/sdr/DL72S954473), Nov 22, 1995: SPAR STIFFENER. CRACKED. FOUND ON B1 LETTER CK, LE SPAR STIFFENER CRACKED OUTBD TRACK NUMBER 3 SLAT INBD ANGLE. REPAIRED PER MM 57-20-21. - [SDR DL72S954343](https://openairdocs.org/sdr/DL72S954343), Nov 11, 1995: BOLT. MISSING. ON DEPARTURE, NR 2 SLAT FAILED TO RETRACT, AIL WAS DISPLACED 30 UNITS, NR 2 SLAT SHOWED GREEN ON S/O PANEL, NR 2 SLAT FINALLY STOWED WITH SPEED REDUCTION. FOUND - [SDR DL72S953920](https://openairdocs.org/sdr/DL72S953920), Sep 25, 1995: ANGLE. CRACKED. THE NR 5 L/E SLAT, LOWER T/E ATTACH ANGLE CRACKED AT RIB NR 9. REPAIRED PER M/M 57-54-0 PAGE 807A. - [SDR DL72S953394](https://openairdocs.org/sdr/DL72S953394), Aug 14, 1995: EEL BATTERY PACK. DISCHARGED. DURING LAYOVER, FOUND EMERGENCY LIGHTS ABOVE AFT AIRSTAIR INOP. REPLACED BATTERY OPERATION NORMAL. - [SDR DL72S952133](https://openairdocs.org/sdr/DL72S952133), May 15, 1995: ANGLE. CRACKED. DOUBLER CRACKED FOR FLANGE UNDER ANTI ICE DUCT FOR NR 2 SLAT. FOUND DURING A-2 LTR CK. REPAIRED PER MM 57-54-0. - [SDR DL72S952132](https://openairdocs.org/sdr/DL72S952132), May 15, 1995: RIB. CRACKED. ONE-HALF INCH CRACK NR 2 SLAT NOSE RIB ANGLE O/B OF ACTUATOR ATTACH. REPAIRED PER MM 57-54-0. FOUND AT A-2 LETTER CHECK. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19960729027079I](https://openairdocs.org/incident/19960729027079I), Jul 29, 1996: Boeing 727232 (N536DA), Bozeman, MT. Narrative: a delta airlines B-727 encountered moderate to severe turbulence while climbing through 13,500 feet. The seat belt sign had been turned off;… - [Incident 19800721061829I](https://openairdocs.org/incident/19800721061829I), Jul 21, 1980: Boeing 727232 (N536DA), Shreveport, LA. Engine shutdown, flight returned due to high oil temp. Replaced indicator and sensor. ## Other aircraft with N536DA - [Registered now](https://openairdocs.org/aircraft/N536DA): Aeryon Labs SKY RANGER, S/N 4012255 --- 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.