# N915UP: 1967 Boeing 727-27C, registration cancelled 2006-08-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 23, 2006
- Status when cancelled: Sale reported
- Airframe: [Boeing 727-27C](https://openairdocs.org/model/boeing-727-27c) (registry code 138400J)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 19533
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 20, 1967
- Last registry action: April 29, 2005
- Mode S code: ACAB0E
- 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/N915UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=915UP
- Page: https://openairdocs.org/deregistered/N915UP-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 727-27C: https://openairdocs.org/model/boeing-727-27c.md

## Service difficulty reports (114, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UPS01236444](https://openairdocs.org/sdr/UPS01236444), Jul 30, 2001: FITTING. CORRODED. INSPECTION TYPE:IN FRAME FOOT ANGLE AT FS 351 BETWEEN STRINGERS 24R AND 25R IS SEVERELY CORRODED. THIS IS UNDER FLOOR PANEL ON RT SIDE OF NLG WW ENCLOSURE ON TH
- [SDR UPS01236434](https://openairdocs.org/sdr/UPS01236434), Jul 27, 2001: ANGLE. CRACKED. INSPECTION TYPE:N/A FRAME ANGLE CRACKED STA 351 JUST AFT OF O/B AFT CORNER OF ACCESS PANEL BEHIND NLG RT SIDE CUTOUT DAMAGED ANGLE PER SRM 51-10-01 PERFORMED HF
- [SDR UPS01236400](https://openairdocs.org/sdr/UPS01236400), Jul 20, 2001: SKIN. CORRODED. INSPECTION TYPE:N/A CORROSION AFT OF NLG WW, BELLY SKIN. REMOVED CORROSION AT BS 340 TO BS 360 BETWEEN STR 26 AND 27 RT PER SRM 51-10-01. INSTALLED LT AND RT IN
- [SDR UPS01235828](https://openairdocs.org/sdr/UPS01235828), May 8, 2001: ACTUATOR. MALFUNCTIONED. INSPECTION TYPE:N/A LT MLG WOULD NOT RETRACT AFTER LANDING GEAR RETRACTION THE RED DOORS WARNING LIGHT AND LEFT GEAR UNLOCKED RED LIGHT REMAINED ILLUMINATED WHE
- [SDR UPS00234540](https://openairdocs.org/sdr/UPS00234540), Nov 21, 2000: WEB. CRACKED. INSPECTION TYPE:N/A 1 INCH CRACK AT BOLT HOLE, WEB AREA 24 INCHES AFT OF BULKHEAD NOSE W/W 3 INCHES UP FROM DOOR OPENING LT SIDE REPAIR CRACKED WEB PER B727 SRM
- [SDR UPS00234445](https://openairdocs.org/sdr/UPS00234445), Nov 12, 2000: BATTERY. DISCHARGED. INSPECTION TYPE:C, FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERIES WEAK. REPLACED BATTERIES, OPS CKS OK.
- [SDR UPS00234444](https://openairdocs.org/sdr/UPS00234444), Nov 12, 2000: BATTERY. DISCHARGED. INSPECTION TYPE:C, COCKPIT EMERGENCY EXIT LIGHT BATTERIES WEAK. REPLACED BATTERIES, OPS CKS OK.
- [SDR UPS00233798](https://openairdocs.org/sdr/UPS00233798), Sep 16, 2000: SKIN. DAMAGED. INSPECTION TYPE:C, LEFT WING LEADING EDGE AT WS 171.5 ABOVE NR 3 LEADING EDGE FLAP DAMAGED. INSTALLED SKIN REPAIR FROM WS 171.5 TO 160.0, DOUBLER MATERIAL USED,
- [SDR UPS00233797](https://openairdocs.org/sdr/UPS00233797), Sep 16, 2000: SKIN. DAMAGED. INSPECTION TYPE:C, LEFT WING LEADING EDGE AT WS 251 ABOVE NR 2 LEADING EDGE FLAP IS DAMAGED. INSTALLED DOUBLER REPAIR, MATERIAL 2024-T3,0. 080, 9 X 7 INCHES, FI
- [SDR UPS00231267](https://openairdocs.org/sdr/UPS00231267), Jan 11, 2000: SKIN. CORRODED. CORROSION FOUND ON FUSELAGE COMPLY WITH D185003 CORROSION AT STA 118 3 LEFT SIDE. CUT OUT DAMAGED SECTION AT STR 9 LT BS1181 TO 1175 PER SRM 51-10-1. PERFORMED 
- [SDR UPS99229224](https://openairdocs.org/sdr/UPS99229224), Apr 2, 1999: FITTING. CORRODED. INSPECTION TYPE:C, LEFT WING OUTBOARD AILERON CENTER OUTBOARD HINGE FITTING CORROED (AILERON SIDE). REPLACED PER SRM 51-30-2.
- [SDR UPS99229210](https://openairdocs.org/sdr/UPS99229210), Apr 2, 1999: FITTING. CORRODED. INSPECTION TYPE:C LEFT WING OUTBOARD AILERON CENTER INBOARD HINGE FITTING CORRODED AILERON SIDE. REPLACED HINGE FITTING PER SRM 51-30-2.
- [SDR UPS99229209](https://openairdocs.org/sdr/UPS99229209), Apr 2, 1999: RIB. CRACKED. INSPECTION TYPE:C, NR 3 SLAT OUTBOARD ACTUATOR RIB IS CRACKED. REMOVED 2 EA RIBS O/B ACTUATOR RIB AND NEXT ONE O/B FOR ACCESS, DRILLED NEW RIB AND INSTALLED, IN
- [SDR UPS99229213](https://openairdocs.org/sdr/UPS99229213), Mar 24, 1999: SKIN. CORRODED. INSPECTION TYPE:C WHILE WORKING NRC 923405, FOUND CENTER FUEL CELL UPPER SKIN CORRODED UNDER SEAL RETAINER RBL 50-65. REPAIRED PER ER 99-5206.
- [SDR UPS99229215](https://openairdocs.org/sdr/UPS99229215), Mar 21, 1999: CHORD. CORRODED. INSPECTION TYPE:C, CORROSION ON WING CENTER SECTION AFT LOWER CHORD RBL 42-48 AND AFT UPPER CHORD RBL 38-42. REPLACED UPPER AND LOWER CHORD PER SRM 51-30-2 AND 
- [SDR UPS99229212](https://openairdocs.org/sdr/UPS99229212), Mar 19, 1999: FITTING. CORRODED. INSPECTION TYPE:C, LEFT HORIZONTAL STAB RUB PAD BULGING FROM CORROSION ON ATTACH FITTING. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-02.
- [SDR UPS99229211](https://openairdocs.org/sdr/UPS99229211), Mar 19, 1999: FITTING. CORRODED. INSPECTION TYPE:C, RT HORIZONTAL STAB RUB PAD BULGING FROM CORROSION ON ATTACH FITTING. REMOVED AND REPLACED FITTING PER SRM 51-30-02.
- [SDR UPS99229214](https://openairdocs.org/sdr/UPS99229214), Mar 5, 1999: LINK. CORRODED. INSPECTION TYPE:C CORROSION EMANATING FROM AROUND AFT BUSHING LBL 24 EXPANSION LINK BS 868 WL 205. REMOVED EXPANSION LINK FROM AIRCRAFT, REMOVED CORROSION FROM 
- [SDR UPS97224560](https://openairdocs.org/sdr/UPS97224560), Sep 29, 1997: SPOILER. DELAMINATED. INSPECTION TYPE-C, NR 12 SPOILER HAS A 3 X 3 AREA OF DELAMINATION ON UPPER SURFACE 8 FROM FWD EDGE ON O/B END. REPAIRED NR 12 SPOLER UPPER SURFACE IAW SRM 57-50
- [SDR UPS97224559](https://openairdocs.org/sdr/UPS97224559), Sep 29, 1997: SEAT TRACK. CORRODED. INSPECTION TYPE-C, CORROSION ON SEAT TRACK AND AROUND FASTENERS STA 850 TO 870 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. ALSO, FOUND ATTACH
- [SDR UPS97224564](https://openairdocs.org/sdr/UPS97224564), Sep 22, 1997: STIFFENER. CORRODED. INSPECTION TYPE-C, CORROSION (C53-111-03.00-01) ON NOSE WHEEL WELL UPPER SKIN BS 313 RBL 11 WL 181. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-11-1. REPLACE
- [SDR UPS97224563](https://openairdocs.org/sdr/UPS97224563), Sep 22, 1997: FLOORBEAM. CORRODED. INSPECTION TYPE-C, WHILE ACCESSING FOR INTERIOR 81 CUSTOMER NR 740183 DISCOVERED FLOORBEAM UPPER CHORD TO BE CORRODED LBL 16 RBL 16 WL 208 BS 344. REMOVED CORRO
- [SDR UPS97224562](https://openairdocs.org/sdr/UPS97224562), Sep 22, 1997: SKIN. CORRODED. INSPECTION TYPE-C, CORROSION (C53-100-01.00-4) EXTERNAL SKIN PILLOWED WITH DISHED RIVET HEADS AND LIGHTNING STRIKE STR 19R STA 664 TO 682 WL 199. REMOVED CORROS
- [SDR UPS97224561](https://openairdocs.org/sdr/UPS97224561), Sep 22, 1997: SEAT TRACK. CORRODED. INSPECTION TYPE-C, CORROSION ON SEAT TRACK AND AROUND FASTENERS BS 850 TO 870 LBL 25 WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLAC
- [SDR UPS97224468](https://openairdocs.org/sdr/UPS97224468), Sep 17, 1997: BEAM. CRACKED. INSPECTION TYPE-C, FWD ENTRY DOOR UPPER GATE BEAM CRACKED IN RADIUS OF OUTER ANGLE. REMOVED AND REPLACED FWD ENTRY DOOR UPPER GATE BEAM IAW SRM 51-30-2, 51-20-4
- [SDR UPS97224474](https://openairdocs.org/sdr/UPS97224474), Sep 16, 1997: SKIN. CRACKED. INSPECTION TYPE-C, POSSIBLE CRACK STA 219 UPPER AFT CORNER OF B2 WINDOW. REPAIRED PER UPS EO B727-5310-0012K.
- [SDR UPS97224473](https://openairdocs.org/sdr/UPS97224473), Sep 16, 1997: SKIN. CORRODED. INSPECTION TYPE-C, CORROSION NOTED ON RT ELEVATOR 2ND O/B STATIC WICK BASE. CORROSION OUT OF LIMITS IAW SRM 55-20-1. REPAIRED ELEVATOR (RT) IAW 55-20-3 SRM 51-8
- [SDR UPS97224472](https://openairdocs.org/sdr/UPS97224472), Sep 16, 1997: SKIN. CORRODED. INSPECTION TYPE-C, CORROSION (C53-111-03.00-01) FOUND ON UPPER SKIN OF NLG DOGHOUSE BS 304 RBL 6 TO 13 WL 181. REWORK UPPER SKIN OF DOGHOUSE BS 304 OUT OF LIMIT
- [SDR UPS97224471](https://openairdocs.org/sdr/UPS97224471), Sep 16, 1997: SPOILER. DELAMINATED. INSPECTION TYPE-C, NR 12 SPOILER HAS DELAMINATION AROUND ACTUATOR FITTING ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED NR 12 SPOILER IAW MM 27-61-01.
- [SDR UPS97224470](https://openairdocs.org/sdr/UPS97224470), Sep 16, 1997: SPOILER. DELAMINATED. INSPECTION TYPE-C, NR 14 SPOILER HAS DELAMINATION AROUND ACTUATOR FITTING ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED NR 14 SPOILER IAW MM 27-61-01.
- [SDR UPS97224469](https://openairdocs.org/sdr/UPS97224469), Sep 16, 1997: SPOILER. DELAMINATED. INSPECTION TYPE-C, NR 13 SPOILER HAS DELAMINATION AROUND ACTUATOR FITTING ON UPPER AND LOWER SURFACE. REMOVED NR 13 SPOILER AND REPLACED IAW MM 27-61-01.
- [SDR UPS97224467](https://openairdocs.org/sdr/UPS97224467), Sep 16, 1997: CHORD. CORRODED. INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 736862 FOUND CORROSION ON RT UPPER NLG CHORD BS 294 TO 315 RBL 11 WL 181. CORROSION REWORK OUT OF LIMITS IAW SRM 
- [SDR UPS97224477](https://openairdocs.org/sdr/UPS97224477), Sep 15, 1997: RIB. CORRODED. INSPECTION TYPE-C, CORROSION AT THE O/B LOWER BONDING JUMPER ON THE NR 3 K-FLAP RIB. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER EO 5740-3980. REPAIRED PER
- [SDR UPS97224476](https://openairdocs.org/sdr/UPS97224476), Sep 15, 1997: RIB. CORRODED. INSPECTION TYPE-C, CORROSION AT THE I/B LOWER BONDING JUMPER ON NR 3 K-FLAP RIB. REMOVED CORROSION PER EO B727-5740-3980, FOUND TO BE OUT OF LIMITS PER EO B727-
- [SDR UPS97224475](https://openairdocs.org/sdr/UPS97224475), Sep 15, 1997: SKIN. CRACKED. INSPECTION TYPE-C, POSSIBLE CRACK STA 219 UPPER AFT CORNER OF R2 WINDOW. REPAIRED PER UPS EO B727-5310-0012K.
- [SDR UPS96206006](https://openairdocs.org/sdr/UPS96206006), Apr 16, 1996: FRAME. MISDRILLED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 760 HAS HOLE DRILLED STR 16R. FAB AND INSTALLED DOUBLER REPAIR IAW SRM 51-30-2.
- [SDR UPS96206005](https://openairdocs.org/sdr/UPS96206005), Apr 16, 1996: FRAME. MISDRILLED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 783 HAS HOLE DRILLED STR 16R. FAB AND INSTALLED DOUBLER REPAIR IAW SRM 51-30-2.
- [SDR UPS96206004](https://openairdocs.org/sdr/UPS96206004), Apr 16, 1996: FRAME. MISDRILLED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 783 HAS HOLE DRILLED STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36281 SHEET 1.
- [SDR UPS96206003](https://openairdocs.org/sdr/UPS96206003), Apr 16, 1996: FRAME. MISDRILLED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 760 HAS HOLE DRILLED STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36279 AND SRM 51-30-2.
- [SDR UPS96206002](https://openairdocs.org/sdr/UPS96206002), Apr 16, 1996: FRAME. MISDRILLED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME 825.95 HAS HOLE DRILLED IN FASTENER STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36281 SHT 1.
- [SDR UPS96206007](https://openairdocs.org/sdr/UPS96206007), Apr 12, 1996: FITTING. CORRODED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 870 RT TERMINAL SEVERLY CORRODED ON VAPOR SEAL ATTACH FLANGE WL 190 RBL 65 TO 71. CUT OUT AND BLENDED CORROSION PE
- [SDR UPS96205999](https://openairdocs.org/sdr/UPS96205999), Apr 11, 1996: SEAT TRACK. WORN. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 500 BL 0 SEAT TRACK IS WORN BEYOND LIMITS. FAB AND INSTALLED SEAT TRACK PER SRM 51-10-2.
- [SDR UPS96205998](https://openairdocs.org/sdr/UPS96205998), Apr 10, 1996: FLOOR BEAM. UNPLUGGED HOLE. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FASTENER HOLE UNPLUGGED FS 1166 RBL 45 FLOOR BEAM SUPPORT CHANNEL. INSTALLED FREEZE PLUG, FAB AND INSTALLED REPAIR PA
- [SDR UPS96205996](https://openairdocs.org/sdr/UPS96205996), Apr 10, 1996: FLOOR BEAM. CORROSION. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 360 WL 208, FLOOR BEAM UPPER FLANGE AFTER NUTPLATE AND CORROSION REMOVAL, FLOOR BEAM WAS FOUND TO BE BEYOND LIMITS
- [SDR UPS96205993](https://openairdocs.org/sdr/UPS96205993), Apr 8, 1996: FLOOR BEAM. CORRODED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FLOOR BEAM UPPER FLANGE CORROSION WAS FOUND TO BE BEYOND LIMITS PER SRM 53-10-1, AT STA 560 WL 208 FROM LBL 50 TO LBL
- [SDR UPS96205995](https://openairdocs.org/sdr/UPS96205995), Apr 4, 1996: BRACKET. CRACKED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CABIN FLOOR BEAM SUPPORT BRACKET IS CRACKED AT THE UPPER EDGE TWO PLACES, BS 1130 AND RBL 44. REMOVED AND FABRIC
- [SDR UPS96206001](https://openairdocs.org/sdr/UPS96206001), Apr 3, 1996: STRINGER. CORROSION. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT EXTERNAL FUEL TANK AT WS 224 TO 230 STR 1 REQUIRES REPAIR DUE TO CORROSION BEYOND LIMITS. SPLICED STR 1 AT STA 209
- [SDR UPS96205951](https://openairdocs.org/sdr/UPS96205951), Apr 3, 1996: ANGLE. CRACKED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING AT ACCESS PANEL JUST I/B OF NR 4 K-FLAP I/B END BULKHEAD ANGLE AT LOWER END HAS NUMEROUS CRACKS AT FASTENERS.
- [SDR UPS96205949](https://openairdocs.org/sdr/UPS96205949), Apr 2, 1996: ANGLE. CRACKED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FAIRING SUPPORT ANGLE HAS CRACK AT GROUND. REMOVED FASTENER AND TERMINATED CRACK AT RIVET HOLE. INSTALLED DOUBLER PER
- [SDR UPS96206000](https://openairdocs.org/sdr/UPS96206000), Mar 30, 1996: FLOOR BEAM. CORROSION. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FLOOR BEAM UPPER FLANGE AFTER CORROSION REMOVAL, FLOOR BEAM WAS FOUND TO BE BEYOND LIMITS. REMOVED DAMAGED SECTION OF

All 114: https://openairdocs.org/deregistered/N915UP-2006-08-23/reports.md

## Other aircraft with N915UP

- [Registered now](https://openairdocs.org/aircraft/N915UP): Boeing 767-300F, S/N 67984, built 2026

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