# N292WA: 1980 Boeing 727-247, 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 727-247](https://openairdocs.org/model/boeing-727-247) (registry code 138408F) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 22110 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: May 5, 1980 - Certificate issued: June 29, 2004 - Last registry action: June 15, 2010 - Mode S code: A2FEDD - 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/N292WA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=292WA - Page: https://openairdocs.org/deregistered/N292WA-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 727-247: https://openairdocs.org/model/boeing-727-247.md ## Service difficulty reports (100, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL72W020883](https://openairdocs.org/sdr/DL72W020883), Jul 28, 2002: ENGINE. OUT OF TRIM. REJECTED TAKEOFF. AIRSPEED APPROX 130 KIAS LIGHT BRAKING. EVERYTHING ELSE NORMAL WITH ABORT. COULD NOT GET NORMAL POWER EPR OF 2.06 OUT OF NUMBER 1 ENGINE. N1 A - [SDR DL72W011876](https://openairdocs.org/sdr/DL72W011876), Nov 28, 2001: ANGLE. CRACKED. NBR 7 SLAT ANGLE CRACKED AT INBD STOP PAD ATTACH FOUND AT F1 LETTER CK REPAIRED PER MM 57-54-000-8 - [SDR DL72W011875](https://openairdocs.org/sdr/DL72W011875), Nov 28, 2001: ANGLE. CRACKED. NBR 8 SLAT ANGLE CRACKED AT ANTIICE T DUCT CUTOUT FOUND ON F1 LETTER CHECK REPAIRED PER MM 57-54-000-8 - [SDR DL72W011058](https://openairdocs.org/sdr/DL72W011058), Jun 24, 2001: BATTERY PACK. DISCHARGED. LEFT FWD AND AFT EMERGENCY EXIT EXTERIOR LIGHT INOP. REPLACED BATTERY PACKS. - [SDR DL72W011057](https://openairdocs.org/sdr/DL72W011057), Jun 24, 2001: BATTERY PACK. DISCHARGED. LEFT FWD AND AFT EMERGENCY EXIT EXTERIOR LIGHTS INOP. REPLACED BATTERY PACKS. - [SDR DL72W010952](https://openairdocs.org/sdr/DL72W010952), Jun 12, 2001: ENGINE. MALFUNCTIONED. ON T/O ROLL, NR 3 ENG INSTR WERE UNSTABLE. ABORTED AT 110 KNOTS. ON INITIAL PWR APPLICATION NR 3 ENG WAS STABLE THEN PROGRESSIVELY BECAME UNSTABLE. NORMAL PWR U - [SDR DL72W002230](https://openairdocs.org/sdr/DL72W002230), Nov 14, 2000: BALLAST. SHORTED. BALLAST AT 15 ABC POPPED C/B AND EMITTED BURNING SMELL. REPLACED BALLAST. OP CKS NORMAL. - [SDR DL72W001702](https://openairdocs.org/sdr/DL72W001702), Aug 30, 2000: WEB. CRACKED. AT MIDVISIT, THE RT LOWER CORNER OF THE 1303 WEB WAS CRACKED. DRILLED UP DOUBLER PER DRD 53-10-4D FIG 802D. STOP DRILLED CRACK PER DRD 53-10-4D AND DYE CKED PER - [SDR DL72W001701](https://openairdocs.org/sdr/DL72W001701), Aug 30, 2000: WEB. CRACKED. AT MIDVISIT, THE LT LWR CORNER OF 1303 WEB WAS FOUND CRACKED. DRILLED UP DOUBLER PER DRD 53-10-4 FIG 802. STOP DRILLED CRACK PER DRD 53-10-4 AND DYE CKED PER DR - [SDR DL72W001762](https://openairdocs.org/sdr/DL72W001762), Aug 29, 2000: RIB. CRACKED. AT MV2, RIB CRACKED NR 7 SLAT O/B RIB AT ACTUATOR ATTACH POINT. FABBED DBLR PER 727 MM 57-54-0 FIG 804, INSTALLED DBLR PER 727 MM 57-54-0 FIG 804, INSTALLED COV - [SDR DL72W001761](https://openairdocs.org/sdr/DL72W001761), Aug 29, 2000: RIB. CRACKED. AT MV2 FOUND RW RIB CRACKED NR 7 SLAT I/B RIB AT ACTUATOR ATTACH POINT. FABBD DBLR PER MM 727-57-54-0 FIG 804. INSTALLED DBLR PER MM 57-54-0 FIG 804. - [SDR DL72W001754](https://openairdocs.org/sdr/DL72W001754), Aug 29, 2000: RIB. CRACKED. AT MV2 FOUND RW RIB CRACKED NR 6 L/E SLAT, I/B RIB AT ACTUATOR ATTACH POINT. REMOVED PREV REPAIR AND FABBD REPLACEMENT DBLR PER MM 51-540 FIG 804. REPAIRED PER - [SDR DL72W001733](https://openairdocs.org/sdr/DL72W001733), Aug 29, 2000: RIB. CRACKED. RIB-CRACKED NR 7 SLAT I/B RIB AT ACTUATOR ATTACH POINT W/W NRC 303. FABRICATED DOUBLER PER MM 727-57-54-0 FIG 804. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER - [SDR DL72W001732](https://openairdocs.org/sdr/DL72W001732), Aug 29, 2000: RIB. CRACKED. RIB CRACKED NR 7 SLAT O/B RIB AT ACTUATOR ATTACH POINT W/W NRC 342. FABRICATED DOUBLER PER 727 MM 57-54-0 FIG 804 OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER 7 - [SDR DL72W001301](https://openairdocs.org/sdr/DL72W001301), Jul 9, 2000: LIGHT. FAILED. AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WILL NOT LIGHT. REPLACED LIGHT ASSY, OP CKS GOOD. - [SDR DL72W992389](https://openairdocs.org/sdr/DL72W992389), Oct 28, 1999: O-RING. LEAKING. NR 3 ENGINE FLAMED OUT ON APPROACH AT 6000 FEET. AT LEVEL OFF 6000 FEET DURING FINAL APPROACH SEGMENT NR 3 INSTRUMENTS INDICATED THE FOLLOWING FUEL FLOW 0 / 35 - [SDR DL72W992340](https://openairdocs.org/sdr/DL72W992340), Oct 24, 1999: LIGHT. INOP. AFT STAIR EMERGENCY OVERHEAD LIGHT INOP. REPLACED LIGHT PACK ASSY, OPS CHECK NORMAL. - [SDR DL72W991941](https://openairdocs.org/sdr/DL72W991941), Aug 31, 1999: FITTING. LOOSE. ON TAKEOFF NR 1 ENG HAD LOW OIL PRESSURE AND LOW OIL PRESSURE LIGHT. ALSO, OIL QTY DROPPED. RTO FOUND BANJO FITTING LOOSE AND TIGHTEND SAME. MTC FERRY ATL FOR E - [SDR DL72W990315](https://openairdocs.org/sdr/DL72W990315), Feb 17, 1999: ACTUATOR. LEAKING. INFLIGHT 'A' SYS HYD QTY DECREASED TO NEAR ZERO, ACCOMPLISHED PROD IAW POM. REPLACED INBOARD KRUEGER FLAP ACTUATOR. - [SDR DL72W982254](https://openairdocs.org/sdr/DL72W982254), Nov 1, 1998: BATTERY PACK. DISCHARGED. ON L/O, FOUND EMERGENCY EXIT LIGHT OVER DOOR L2 INOP. REPLACED BATTERY PACK, OPS CKS NORMAL. - [SDR DL72W981344](https://openairdocs.org/sdr/DL72W981344), Jun 16, 1998: FLOORBEAM. CORRODED. CORROSION AT FLOORBEAM STA 344 FROM LBL 13 TO RBL 17-MARKED. REPAIRED PER SRM 53-10-8 FIG 11. - [SDR DL72W981205](https://openairdocs.org/sdr/DL72W981205), Jun 7, 1998: POWER SUPPLY. INOPERATIVE. FOUND ON LAYOVER INSP, AIRSTAIR DOOR EXIT LIGHT FLICKERING. REPLACED ASSOCIATED POWER SUPPLY. - [SDR DL72W981026](https://openairdocs.org/sdr/DL72W981026), May 13, 1998: RIB. CRACKED. FOUND ON C1 LETTER CK, L/E NOSE RIB CRACKED 1.25 INCH PAST, STOP DRILL, NR 5 SLAT ACTUATOR INBD ATTACH RIB. REPAIRED PER MM 57-54-0. - [SDR DL72W981024](https://openairdocs.org/sdr/DL72W981024), May 13, 1998: WEB. CRACKED. FOUND AT C1 LETTER CK, RT TORQUE BOX WEB CRACKED AT UPPER END STA 1214, REPAIRED PER M/M 53-11-0 PG 832 RT TORQUE BOX WEB CRACKED .25 INCH AT UPPER LIGHTENING H - [SDR DL72W962602](https://openairdocs.org/sdr/DL72W962602), Nov 28, 1996: BATTERY PACK. DISCHARGED. DURING L/O CK, FOUND RIGHT SIDE OVERWING EXIT LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS OK. - [SDR DL72W962300](https://openairdocs.org/sdr/DL72W962300), Oct 11, 1996: LIGHT. INOPERATIVE. FWD GALLEY DOOR REMOVABLE EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS CHECKS OK. - [SDR DL72W962299](https://openairdocs.org/sdr/DL72W962299), Oct 11, 1996: BATTERY PACK. DISCHARGED. OVERWING EXIT SIGNS INOP ON RIGHT SIDE. REPLACED BATTERY PACK AT M1086, OPS CHECKS OK. - [SDR DL72W961044](https://openairdocs.org/sdr/DL72W961044), May 1, 1996: HYD PUMP. INOPERATIVE. FLT 893 - AIR TURN BACK DUE TO B-SYSTEM HYDRAULIC WENT TO ZERO WITH LOW PRESSURE LIGHT ON. A-SYSTEM AT 2.5 GALLONS. REPLACED INBOARD B-SYSTEM HYDRAULIC PUMP AND - [SDR DL72W960127](https://openairdocs.org/sdr/DL72W960127), Jan 19, 1996: BATTERY PACK. DISCHARGED. DURING INSPECTION, AFT CABIN BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATT RACK, OPS NORMAL. - [SDR DL72W961585](https://openairdocs.org/sdr/DL72W961585), Jan 18, 1996: TRANSVERSE BEAM. CRACKED. THERE IS A 1 INCH CRACK IN THE ANGLE OF BOTH THE FWD AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRW - [SDR DL72W960119](https://openairdocs.org/sdr/DL72W960119), Jan 17, 1996: ANGLE. CRACKED. FOUND ON A1 LETTER CHECK, TWO .5 INCH CRACKS AT NR 2 L/E SLAT COVE SKIN ANGLE, BELOW TIA DUCT. REPAIRED PER MM 57-50-0. - [SDR DL72W953096](https://openairdocs.org/sdr/DL72W953096), Jul 14, 1995: STRINGER. CORRODED. STRINGER 27L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER. INSTALLED REPAIR PER SRM 53-10-3, FOUND AT HMV. - [SDR DL72W953079](https://openairdocs.org/sdr/DL72W953079), Jul 14, 1995: STRINGER. CORRODED. AT HMV, STR 27 L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER AS PER B-727 SRM 53-10-3. - [SDR DL72W953032](https://openairdocs.org/sdr/DL72W953032), Jul 10, 1995: RIB. CRACKED. NR 3 SLAT RIB CRACKED, I/B OF ACTUATOR ATTACH POINT CRACKED IN RADIUS AT LOWER AFT END OF RIB. INSTALLED DOUBLER PER MM 57-54-0 PG 819. FOUND AT HMV. - [SDR DL72W953006](https://openairdocs.org/sdr/DL72W953006), Jul 8, 1995: RIB. CRACKED. ITEM: NR 6 SLAT RIB CRACKED AT RIVET FWD FLANGE OF RIB NR 7. CORRECTION: REPAIRED PER S.R.M. 57-50-03, FIG 09. DAMAGE FOUND AT HMV. - [SDR DL72W953001](https://openairdocs.org/sdr/DL72W953001), Jul 7, 1995: SKIN. DAMAGED. AT HMV, FOUND NR 4 SLAT INNER ANTI-ICE SKIN BETWEEN NR 12, NR 13 RIBS HAS HOLE. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, FIG 803A. - [SDR DL72W953000](https://openairdocs.org/sdr/DL72W953000), Jul 7, 1995: ANGLE. CRACKED. AT HMV, FOUND NR 4 SLAT ATTACH ANGLE ABOVE NR 13 RIB CRACKED. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, PG 807. - [SDR DL72W952965](https://openairdocs.org/sdr/DL72W952965), Jul 6, 1995: SKIN. CRACKED. NR 6 SLAT SKIN CRACKED AT TAB FOR INBD TRACK FAIRING ATTACH. INSTALLED REPAIR PER MM 57-54-0, PG 820/821. FOUND AT HMV. - [SDR DL72W952934](https://openairdocs.org/sdr/DL72W952934), Jul 5, 1995: BRACKET. CRACKED. BRACKETS CRACKED, NR 2 KRUEGER FLAP ACTUATOR, O/B SUPPORT BRACKET AND I/B SUPPORT BRACKET. DYE CHECKED, FOUND NO DISCREPANCIES PER PS 900-6-301. - [SDR DL72W952932](https://openairdocs.org/sdr/DL72W952932), Jul 5, 1995: RIBS. CRACKED. AT HMV, FOUND NR 4 L/E SLAT WITH RIB NR 1, 10, 13, 15 CRACKED. REPAIRED CRACKED RIBS PER MM 57-54-0. - [SDR DL72W952933](https://openairdocs.org/sdr/DL72W952933), Jul 4, 1995: ANGLE. CRACKED. AT HMV, NR 4 SLAT ANGLE FOR CLOSEOUT PANEL CRACKED AT FWD LOWER EDGE AT RIB NR 12 AND NR 13. REPAIRED PER MM 57-54-0. - [SDR DL72W952937](https://openairdocs.org/sdr/DL72W952937), Jul 2, 1995: SEAT TRACK. CORRODED. AT HMV, SEAT TRACK CORRODED, FROM FS 1070-1110 RT IB TRACK RBL 24.5. REMOVED CORROSION PER SRM 51-10-06. REPLACED TRACK FROM FS 1070 TO 1110 PER MM 53-20-11, PG - [SDR DL72W952866](https://openairdocs.org/sdr/DL72W952866), Jun 30, 1995: SKIN. HOLE. AT HMV SHOP INSPECTION OF NR 1 F/F, WORN AREA FOUND 11 TO 12 INCHES FORM I/B END OF FLAP. ACCOMPLISHED REPAIRS PER SRM 57-50-4. - [SDR DL72W952865](https://openairdocs.org/sdr/DL72W952865), Jun 30, 1995: LE SKIN. WORN. AT HMV SHOP INSPECTION, NR 1 FOREFLAP FOUND WITH A HOLE IN THE L/E 10.5 INCHES FROM I/B END. REPAIRED PER SRM 57-50-4. - [SDR DL72W952918](https://openairdocs.org/sdr/DL72W952918), Jun 29, 1995: FRAME. MISDRILLED. DURING HMV, EDGE DISTANCE COULD NOT BE MAINTAINED ON ONE OF THE FASTENER HOLES THROUGH THE FLOORBEAM UPPER CHORD AT FS 761 ON RT AND LT SIDES. FOUND DURING ACCO - [SDR DL72W952890](https://openairdocs.org/sdr/DL72W952890), Jun 29, 1995: SEAT TRACK. CORRODED. SEAT TRACK CORRODED STA 344 RT SIDE O/B, C53-224-03. REPLACED SEAT TRACK O/B RT SIDE FROM 344 TO 360 PER SRM 53-20-11, FOUND AT HMV. - [SDR DL72W952936](https://openairdocs.org/sdr/DL72W952936), Jun 25, 1995: STRINGER. CORRODED. AT HMV, STR 27L CORRODED AT STA 720F PLUS 10. REPAIRED PER SRM 53-10-3. - [SDR DL72W952898](https://openairdocs.org/sdr/DL72W952898), Jun 25, 1995: SUPPORT. DAMAGED. LT STA 913 UPLOCK SUPPORT FRAME HAS EXISTING TEMP REPAIR. INSTALLED REPAIR PER MM 53-11-0. - [SDR DL72W952825](https://openairdocs.org/sdr/DL72W952825), Jun 25, 1995: BUSHING. WORN. AT HMV, BUSHINGS WORN IN MLG DOOR LUG ON FWD END OF NR 5 FLAP TRACK. REPAIRED PER MM 57-43-0. - [SDR DL72W952894](https://openairdocs.org/sdr/DL72W952894), Jun 24, 1995: FLOORBEAM. CORRODED. AT HMV, FOUND FS 1090 CABIN FLOORBEAM CORRODED AT RBL 45. ACCOMPLISHED REPAIRS PER SRM 53-10-8. All 100: https://openairdocs.org/deregistered/N292WA-2010-07-20/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB SEA83LA039](https://openairdocs.org/ntsb/SEA83LA039), Jan 8, 1983: Boeing 727 (N292WA), Near Yakima, WA, no damage ## FAA accident and incident reports (3) 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 19891002048179I](https://openairdocs.org/incident/19891002048179I), Oct 2, 1989: Boeing 727247 (N292WA), Covington - Cin, OH. A suste, hydraulic failure on climb. Returned. Landed safely. Left gear door actuator upline had ruptured. - [Incident 19870428044309I](https://openairdocs.org/incident/19870428044309I), Apr 28, 1987: Boeing 727247 (N292WA), Salt Lake City, UT. Lost number 3 engine while inbound. Safe landing. Fuel pump garlock seal was leaking. - [Accident 19830127044939A](https://openairdocs.org/incident/19830127044939A), Jan 27, 1983: Boeing 727200 (N292WA), Yakima, WA. Passenger received serious injury as he exited lavatory when aircraft hit severe turbulence. Seat belt signs were on ## Other aircraft with N292WA - [Registered now](https://openairdocs.org/aircraft/N292WA): Dassault-Breguet FALCON 50, S/N 207 --- 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.