# N912UP: 1966 Boeing 727-62C, registration cancelled 2006-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2006 - Status when cancelled: Sale reported - Airframe: [Boeing 727-62C](https://openairdocs.org/model/boeing-727-62c) (registry code 138402C) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Serial number: 19244 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 27, 1991 - Last registry action: October 27, 2004 - Mode S code: AC9FE9 - Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie) - Owner type: Individual - Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N912UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=912UP - Page: https://openairdocs.org/deregistered/N912UP-2006-08-23 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 727-62C: https://openairdocs.org/model/boeing-727-62c.md ## Service difficulty reports (45) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS02237405](https://openairdocs.org/sdr/UPS02237405), Jan 2, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:PFLT ON PREDEPARTURE CHECK, EMERGENCY EXIT LIGHT AT COCKPIT DOOR INOP. INSTALLED NEW BATTERIES AT COCKPIT DOOR EMERGENCY EXIT LIGHT ASSY, OPS CH - [SDR UPS01237341](https://openairdocs.org/sdr/UPS01237341), Nov 27, 2001: SLIDE. UNSECURE. INSPECTION TYPE:N/A ESCAPE SLIDE CAME OFF WHEN CREW CLOSED DOOR. SLIDE RE-INSTALLED NOTE: SLIDE DID NOT DEPLOY. - [SDR UPS01237191](https://openairdocs.org/sdr/UPS01237191), Oct 26, 2001: SLIDE. UNSECURE. INSPECTION TYPE:IN DOOR PARTIALLY OPENED FROM EXTERIOR WITH SLIDE ARMED SLIDE FELL FROM DOOR BUT DID NOT DEPLOY. RESECURED SLIDE ASSY. - [SDR UPS01236903](https://openairdocs.org/sdr/UPS01236903), Sep 17, 2001: BRACKET. CRACKED. INSPECTION TYPE:C #3 THRUST REVERSER O/B LATCH FAIRING MID ANF AFT BRACKETS ARE CRACKE D. BRACKETS REPLACED IAW MM 78-30-01 - [SDR UPS01236902](https://openairdocs.org/sdr/UPS01236902), Sep 17, 2001: STRAP. CRACKED. INSPECTION TYPE:C NDI INSP OF MID GALLEY DOOR CUTOUT INDICATES REINFORCING STRAP CRACK AT UPPER FWD CUTOUT. REPAIRED IAW UPS EO B727-5330-2685. - [SDR UPS01236901](https://openairdocs.org/sdr/UPS01236901), Sep 17, 2001: TRUNNION. CORRODED. INSPECTION TYPE:C ON REMOVAL OF NLG TRUNNION CAPS CORROSION WAS FOUND IN ALL FOUR BOLT HOLES FOR CLAMPING OF TRUNNION CAPS. REPAIRED IAW SMRO EO 2001-044-001 UP - [SDR UPS01236877](https://openairdocs.org/sdr/UPS01236877), Sep 17, 2001: TRUNNION. CORRODED. INSPECTION TYPE:C ON REMOVAL OF TRUNNION CAPS ON NLG TRUNNION AREA WHERE BUSHINGS WERE INSTALLED HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 53-40-1, - [SDR UPS01236876](https://openairdocs.org/sdr/UPS01236876), Sep 17, 2001: DRUM. CORRODED. INSPECTION TYPE:C NLG MANUAL EXTENSION AFT DRUM CORRODED. DRUM ASSY REPLACED IAW OHM 32-34-03. - [SDR UPS01236904](https://openairdocs.org/sdr/UPS01236904), Sep 15, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C NDT INSPECTION FOUND CRACK INDICATION AT BS 880 LBL18-19. STOP DRILLED AND HFEC, CRACK CONTAINED. REPAIRED IAW EO B727-5310-04 60. - [SDR UPS01236890](https://openairdocs.org/sdr/UPS01236890), Sep 14, 2001: SUPPORT FITTING. CRACKED. INSPECTION TYPE:C SUSPECT CRACKS ON LT AND RT 940 SUPPORT FRAME FITTING AT FLOOR BEAM ATTACH FLANGES. HFEC CARRIED OUT LT NDF RT CRACK CONFIRMED ON FWD I/B UPPE - [SDR UPS01236905](https://openairdocs.org/sdr/UPS01236905), Sep 13, 2001: SPAR. CORRODED. INSPECTION TYPE:C EVIDENCE OF CORROSION ON CENTER TANK FRONT SPAR UPPER CHORD VERTICAL FLANGE AT BS 740 RBL 25. REPAIRED IAW SRM 51-30-02 RBL 19 TO 31. - [SDR UPS01236445](https://openairdocs.org/sdr/UPS01236445), Jul 30, 2001: BULKHEAD. CRACKED. INSPECTION TYPE:N/A RT MLG WHEEL WELL FWD BULKHEAD BELOW APU EXHAUST HAS CRACKS AROUND U PPER INBOARD CANNON PLUG RECEPTICLE STA 870 ****MRR FILED AS OPEN*** AI - [SDR UPS01236432](https://openairdocs.org/sdr/UPS01236432), Jul 29, 2001: SKIN. CRACKED. INSPECTION TYPE:N/A CRACKS AT RH WHEEL WELL AREA STA 870 ***MRR FILED AS OPEN*** - [SDR UPS01234964](https://openairdocs.org/sdr/UPS01234964), Feb 6, 2001: LIGHT. FAILED. INSPECTION TYPE:IN COCKPIT EMERGENCY EXIT LIGHT INOP W/OP CHECKED IN FLIGHT. RELAMPED, OPS CHECKS GOOD. - [SDR UPS01234653](https://openairdocs.org/sdr/UPS01234653), Jan 16, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:PFLT 2 INCH CRACK ALONG RT NLG W/W SIDE WALL FWD OF GEAR TRUNNION AT APPROX STA 228 (MARKED). VERIFIED END OF CRACK WITH HFEC. STOP DRILLED RACK - [SDR UPS00232307](https://openairdocs.org/sdr/UPS00232307), Apr 11, 2000: LINE. BURST. INSPECTION TYPE:C, PRESSURE LINE IN B SYS HYD SERVICE BAY BURST ON OPERATION. FAILED UNDER P-CLIP AREA. PRESSURE LINE IN B-SYS HYD SERVICE BAY REPLACED IAW MM 2 - [SDR UPS00232243](https://openairdocs.org/sdr/UPS00232243), Apr 8, 2000: WEB. CRACKED. INSPECTION TYPE:C, WEB BENEATH STAB ACTUATED ELEV TRIM SENSOR CRACKED AT SYS A & SYS B ELEVATOR HYD LINE SUPPORT POINT (PRESS LINES). WEB REPAIRED IAW SRM 51-40 - [SDR UPS00232258](https://openairdocs.org/sdr/UPS00232258), Apr 7, 2000: FRAME. CORRODED. INSPECTION TYPE:C, CORROSION ON VERT STAB ON T-CHORD AFT OF FEEL COMPUTER. REPLACED T-CHORD IAW SRM 51-30-2. REF IPC 55-30-00, FIG 2. - [SDR UPS00232257](https://openairdocs.org/sdr/UPS00232257), Apr 6, 2000: STIFFENER. CORRODED. INSPECTION TYPE:C, WING TO BODY FAIRING NR 3334 HAS CORRODED STIFFENER AROUND GROUND FAN DOOR CUTOUT (RT). ALSO, CORROSION ON DOOR CUTOUT CORRODED STIFFENER REP - [SDR UPS00232245](https://openairdocs.org/sdr/UPS00232245), Apr 6, 2000: CARGO TRACK. CRACKED. INSPECTION TYPE:C, SUSPECT CRACK FOUND ON TIE DOWN TRACK AT STA 1080, STR 28 RT ADJACENT TO FRAME CUTOUT. REPAIR CARRIED OUT IAW SRM 53-10-5. - [SDR UPS00232244](https://openairdocs.org/sdr/UPS00232244), Apr 6, 2000: CHANNEL. CRACKED. INSPECTION TYPE:C, CRACK ON FLOOR LONGITUDINAL Z SECTION AT BS 1000 AT STR 30 IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-5 FIG 4. - [SDR UPS00232242](https://openairdocs.org/sdr/UPS00232242), Apr 6, 2000: FRAME. CRACKED. INSPECTION TYPE:C, CRACK ON FRAME AT BS 1070 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4. - [SDR UPS00232241](https://openairdocs.org/sdr/UPS00232241), Apr 6, 2000: FRAME. CRACKED. INSPECTION TYPE:C, CRACK ON EDGE OF FRAME AT BS 1000 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4. - [SDR UPS00232256](https://openairdocs.org/sdr/UPS00232256), Apr 5, 2000: WEB. CRACKED. INSPECTION TYPE:C, LEFT AND RIGHT WEBS AT BS 1387 OVER THE ENGINE 2 HORIZONTAL FIREWALL ARE CRACKED. LT WEB AND BODY SKIN ATTACH TEE REPLACED IAW DRAWING 65-175 - [SDR UPS99231094](https://openairdocs.org/sdr/UPS99231094), Nov 8, 1999: SUPPORT. CORRODED. INSPECTION TYPE AD V LEFT SUPPORT ASSY I/B FLAP TRACK FWD CORRODED. LEFT I/B FLAP TRACK FWD SUPPORT ASSY REPLACED IAW MM 27-51-31. - [SDR UPS99228532](https://openairdocs.org/sdr/UPS99228532), Jan 26, 1999: LIGHT. INOP. INSPECTION TYPE-N/A, REPEAT WRITE UP WITH EMERGENCY EXIT SWITCH IN THE ARMED POSITION, THE EMERGENCY EXIT LIGHT IN THE COCKPIT IS ON. EMERGENCY EXIT LIGHT BY FW - [SDR UPS98228204](https://openairdocs.org/sdr/UPS98228204), Nov 9, 1998: SKIN. CORRODED. INSPECTION TYPE:C SURFACE CORROSION ON LOWER RUDDER SKIN PANEL LEFT SIDE BETWEEN FRONT SPAR AND REAR SPAR BY PCU ATTACH POINT. RUDDER REPLACED IAW MM 27-20-1. - [SDR UPS98228169](https://openairdocs.org/sdr/UPS98228169), Nov 4, 1998: FRAME. CRACKED. INSPECTION TYPE-C DURING NDT INSPECTION, CRACK FOUND EMANATING FROM FOURTH FASTENER HOLE ABOVE FLOOR LINE AT BS 825.95 RT. REPAIRED IAW APPENDIX C OF EO B727-53 - [SDR UPS98228205](https://openairdocs.org/sdr/UPS98228205), Nov 3, 1998: SKIN. CORRODED. INSPECTION TYPE:C CORROSION ON LOWER RUDDER SKIN PANEL RT SIDE FRONT SPAR AREA BY PCU ATTACH POIN. RUDDER REMOVED IAW MM 27-20-11. - [SDR UPS98228166](https://openairdocs.org/sdr/UPS98228166), Nov 3, 1998: FRAME. CORRODED. INSPECTION TYPE-C, FUSELAGE SLIDING FAIRING NR 3601 HAS CORRODED FRAME AT LOWER FWD CORNER. REPAIRED IAW SRM 53-10-4 AND TYPICAL WEB REPAIRS IAW SRM 51-40-3. - [SDR UPS98228161](https://openairdocs.org/sdr/UPS98228161), Nov 3, 1998: BULKHEAD BEAM. CRACKED. INSPECTION TYPE-C, CRACK FOUND ON VERTICAL BEAM AT RIGHT BUTTOCK LINE 26.83 AT BS 1183 BULKHEAD CRACK ON VERTICAL BEAM AT RBL 26.85, BS 1183 BULKHEAD REPAIRED I - [SDR UPS98228162](https://openairdocs.org/sdr/UPS98228162), Nov 2, 1998: SUPPORT. CORRODED. INSPECTION TYPE-C, CORROSION ON ANGLE SUPPORT FOR FRONT NET TIE DOWN BS 780 LBL 60.00. ANGLE SUPPORT REPLACED IAW SRM 51-30-2. - [SDR UPS98228136](https://openairdocs.org/sdr/UPS98228136), Nov 2, 1998: INTERCOSTAL. DAMAGED. INSPECTION TYPE-C, INTERCOSTAL DAMAGED BS 760 LBL 45 LBL 62. REPAIR CARRIED OUT IAW SRM 51-20-1. - [SDR UPS98228131](https://openairdocs.org/sdr/UPS98228131), Nov 2, 1998: BULKHEAD. DAMAGED. INSPECTION TYPE-C, FWD PRESSURE BULKHEAD AND STIFFENERS FOUND DAMAGED BS 178 WL 200 RBL 5. REPAIRED IAW UPS EO B727-5310-4290 USING REPAIR KIT 65C36289-1. - [SDR UPS98227428](https://openairdocs.org/sdr/UPS98227428), Aug 14, 1998: OVERHEAT LOOP. LOOSE. ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING FLT. ENGINE WAS SHUTDOWN FOR REMAINDER OF FLIGHT. FOUND BACKSHELL LOOSE ON OVERHEAT LOOP AT STATION NR 48. RAN EN - [SDR UPS97224299](https://openairdocs.org/sdr/UPS97224299), Aug 28, 1997: LIGHT. MALFUNCTIONED. INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR ILLUMINATED AT START OF DESCENT. RESEATED AND TESTED EMERGENCY EXIT LIGHT PER M/M 33-50-101, OPS CK - [SDR UPS97224288](https://openairdocs.org/sdr/UPS97224288), Aug 28, 1997: LIGHT. MALFUNCTIONED. EMERGENCY LIGHT ABOVE COCKPIT DOOR ILLUMINATES WITH EMERGENCY LIGHT SWITCH IN THE ARM POSITION. RESEATED EMERGENCY EXIT LIGHT. OPS CK OK. - [SDR UPS97222812](https://openairdocs.org/sdr/UPS97222812), Mar 24, 1997: BULKHEAD FTG. CRACKED. INSPECTION TYPE-D, CRACK FOUND IN RT BS 870 FTG. REPAIRED IAW B727-5310-3057 APP 8.3. - [SDR UPS97222813](https://openairdocs.org/sdr/UPS97222813), Mar 21, 1997: FLAP CARRIAGE. CORRODED. INSPECTION TYPE-D, LT O/B FLAP I/B CARRIAGE HAS PITTING CORROSION. REPLACED IAW 57-58-01. - [SDR UPS97222083](https://openairdocs.org/sdr/UPS97222083), Feb 19, 1997: BUNGEE ASSY. FAILED. WHEN PARKED AT FWA, AFT AIRSTAIR WAS ALL THE WAY DOWN. REMOVED AND REPLACED AFT AIRSTAIR TORQUE TUBE BUNGEE ASSY PER MM 52-60-01, OPS CHK GOOD PER MM 52-62-01. - [SDR UPS205368](https://openairdocs.org/sdr/UPS205368), Jan 30, 1996: STRINGER. CORRODED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, F.S. 740 STRINGER SKIN HAS CORROSION. REPAIRED I.A.W. DHC SK 912-788. - [SDR UPS204931](https://openairdocs.org/sdr/UPS204931), Nov 1, 1995: OVERHEAT MODULE. MALFUNCTION. CREW REPORTED NR 1 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. APPROPRIATE CHECKLIST WAS PERFORMED AND ENGINE WAS SHUTDOWN. ACT NOTIFIED, EMERGENCY DECLARED AN - [SDR UPS204516](https://openairdocs.org/sdr/UPS204516), Sep 23, 1995: SKIN. DELAMINATED. WHILE ON GROUND, MAINTENANCE FOUND LEFT INBOARD MIDFLAP TRAILING EDGE DELAMINATED IN SEVERAL PLACES. REPAIRED DELAMINATION IAW B-727 SRM 51-40-6 PAGE 20. - [SDR UPS202246](https://openairdocs.org/sdr/UPS202246), Feb 9, 1995: EEL. INOP. (SUPPLEMENTAL MRR) FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMER. EXIT LIGHT ASSY AS PER MM 33-50-01. OPS CHECKED GOOD. - [SDR UPS202202](https://openairdocs.org/sdr/UPS202202), Feb 2, 1995: EEL BATTERIES. DISCHARGED. DURING PREDEPARTURE CHECK, EMERGENCY EXIT SIGN DIM AT FORWARD ENTRY DOOR. REPALCED BATTERIES, CHECKS OK. MFG P/N 5106. ## FAA accident and incident reports (1) 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 19850418020169I](https://openairdocs.org/incident/19850418020169I), Apr 18, 1985: Boeing 72762C (N912UP), Louisville, KY. Buzzing noise while retracting flaps and a hydraulic system failing on climb. Manually extended gear and landed. ## Other aircraft with N912UP - [Registered now](https://openairdocs.org/aircraft/N912UP): Boeing 767-300F, S/N 67981, built 2025 --- 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.