# N926UP: 1967 Boeing 727-31C, registration cancelled 2007-09-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 19, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-31C](https://openairdocs.org/model/boeing-727-31c) (registry code 1384011)
- Engine: [Rolls-Royce TAY-651-54](https://openairdocs.org/engine/rolls-royce-tay-651-54) (registry code 54564)
- Data sheets: [TCDS E25NE](https://openairdocs.org/tcds/E25NE) (OpenAirDocs)
- Serial number: 19233
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 3, 2004
- Certificate issued: April 29, 2004
- Last registry action: April 17, 2007
- Mode S code: ACD644
- Owner when cancelled: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N926UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=926UP
- Page: https://openairdocs.org/deregistered/N926UP-2007-09-19

From the FAA registry file of October 31, 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 727-31C: https://openairdocs.org/model/boeing-727-31c.md

## Service difficulty reports (254, newest 50)

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

- [SDR UPS06248770](https://openairdocs.org/sdr/UPS06248770), Dec 15, 2006: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES AND OPS CK IAW MM 33-50-01-5.
- [SDR UPS06248392](https://openairdocs.org/sdr/UPS06248392), Nov 1, 2006: LIGHT. INOPERATIVE. FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AND OPERATIONAL CHECK PER MM 33-50-01-5 CKS NORMAL.
- [SDR UPS06247166](https://openairdocs.org/sdr/UPS06247166), Jun 21, 2006: BATTERY PACK. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP AT CABIN DOOR. REPLACED BATTERY PACK PER MM 33-50-90-2.
- [SDR UPS06247165](https://openairdocs.org/sdr/UPS06247165), Jun 21, 2006: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A EMERGENCY LIGHT INOP AT COCKPIT DOOR. REMOVED AND REPLACED LIGHT ASSY, OPS CHECK NORMAL.
- [SDR UPS05245892](https://openairdocs.org/sdr/UPS05245892), Dec 23, 2005: HYDRAULIC SYSTEM. LEAKING. INSPECTION TYPE:N/A ATB - HYD QTY AFTER TAKEOFF WENT TO 2.0 GALS AFTER FLAP RETRACTION QTY HELD STEADY AT 2.3 GALS. FOUND ASYS QTY LOW, SERVICED TO PROPER LEVEL
- [SDR UPS05245846](https://openairdocs.org/sdr/UPS05245846), Nov 26, 2005: LIGHT. INOPERATIVE. ONE LAMP INOP IN EMERGENCY EXIT LIGHT AT L1 DOOR. RELAMPED OK FOR SERVICE.
- [SDR UPS05245464](https://openairdocs.org/sdr/UPS05245464), Sep 18, 2005: SLIDE. INOPERATIVE. INSPECTION TYPE:N/A L-1 DOOR SLIDE INOP. REMOVED AND REPLACED SLIDE ASSY PER 25-60-14, THIS CLEARS M310071.
- [SDR UPS05244731](https://openairdocs.org/sdr/UPS05244731), Jun 15, 2005: SKIN. CORRODED. C NDI HAS MATERIAL LOSS INDICATION AT S19 RT BS 441, SKIN CUT OUT AND REPAIR IN CONJUNCTION WITH NRC 792106 LAP REPAIR.
- [SDR UPS05244729](https://openairdocs.org/sdr/UPS05244729), Jun 14, 2005: BUSHING. DAMAGED. ENGINE NR 3 FWD MOUNT AFT O/B HOLE REPAIR BUSHING DAMAGED. BUSHING REPLACED IAW UPS EO B727-5440-11592-A.
- [SDR UPS05244728](https://openairdocs.org/sdr/UPS05244728), Jun 14, 2005: STRUCTURE. CORRODED. ENG NR 1 FWD MOUNT BOTH O/B HOLES HAVE PITTING CORROSION ON REPAIR BUSHINGS. BUSHINGS REPLACED IAW UPS EO B727-5440-11592-A.
- [SDR UPS05244725](https://openairdocs.org/sdr/UPS05244725), Jun 13, 2005: SKIN. CRACKED. CRACK IN FUSELAGE SKIN BS 355 BETWEEN S26L AND 27L. REPAIR CARRIED OUT IAW SRM 53-30-3 AND 51-10-2.
- [SDR UPS05244732](https://openairdocs.org/sdr/UPS05244732), Jun 12, 2005: FITTING. CRACKED. CLEAT CRACKED O/B OF S26R AT BS 600 LWR SECTION OF CLEAT ADJACENT TO S 26. REMOVED DAMAGED CLEAT IAW SRM 51-30-2. FABRICATED CLEAT IAW SRM 51-20-1. INSTALLED CL
- [SDR UPS05244727](https://openairdocs.org/sdr/UPS05244727), Jun 11, 2005: SUPPORT BRACKET. CRACKED. ENG NR 3 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2.
- [SDR UPS05244726](https://openairdocs.org/sdr/UPS05244726), Jun 11, 2005: SUPPORT BRACKET. CRACKED. ENG NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2.
- [SDR UPS05244733](https://openairdocs.org/sdr/UPS05244733), Jun 10, 2005: SKIN. CRACKED. CRACK ON SKIN AT FWD ENTRY DOOR UPPER FWD AREA (BETWEEN S6 AND S 7L) OF CUT OUT. REPAIR CARRIED OUT IAW EO B727-5330-1460 OPTION 1.
- [SDR UPS05244730](https://openairdocs.org/sdr/UPS05244730), Jun 10, 2005: SUPPORT BRACKET. CRACKED. NR 2 LE FLAP ACTUATOR O/B SUPPORT BRACKET CRACKED AT UPPER FWD CORNER. BRACKET FABRICATED AND REPLACED IAW SRM 51-20-1, 51-30-02 AND DRAWING 65 -16269.
- [SDR UPS05244738](https://openairdocs.org/sdr/UPS05244738), Jun 7, 2005: HINGE. CRACKED. INSPECTION TYPE:C SUSPECT CRACK ON LEFT O/B AILERON I/B TAB HINGE ASSY LWR HALF. HFEC CARRIED OUT ON SUSPECT AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIR
- [SDR UPS05244737](https://openairdocs.org/sdr/UPS05244737), Jun 7, 2005: SKIN. DEBONDED. INSPECTION TYPE:C RT ELEVATOR TAB DISBONDED AT LOWER SURFACE 24 INCHES O/B OF INNER EDGE, AT LOWER SURFACE 3 INCHES FROM O/B EDGE 2 SUSPECT AREA RT UPPER OUTER 
- [SDR UPS05244736](https://openairdocs.org/sdr/UPS05244736), Jun 7, 2005: SKIN. CORRODED. INSPECTION TYPE:C LT ELEVATOR TAB UPPER SKIN CORRODED 5 INCHES FROM O/B END. REMOVED CORROSION IAW SRM 51-10-01, BLENDOUT FOUND TO BE OUT OF LIMITS IAW SRM 55-2
- [SDR UPS05244735](https://openairdocs.org/sdr/UPS05244735), Jun 7, 2005: LAP JOINT. CORRODED. INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT S19R BETWEEN BS 390 AND 441 AREA BETWEEN BS 390 AND 441 PAINT STRIPPED IAW MM 51-20-01. AREA REINSPECTED, COROS
- [SDR UPS04243150](https://openairdocs.org/sdr/UPS04243150), Sep 22, 2004: ACTUATOR. BROKEN. INSPECTION TYPE:N/A ON APPROACH RIGHT MAIN UPLOCKED LIGHT GEAR DOOR LIGHT REMAINED ON. RECYCLED ONCE, LIGHTS STILL ON, MANUALLY CRANKED RIGHT GEAR DOWN. REPLACE
- [SDR UPS04243022](https://openairdocs.org/sdr/UPS04243022), Aug 25, 2004: LIGHT. MALFUNCTIONED. FLT STA EMERGENCY LIGHT WAS COMING ON IN FLT IN ARM POST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW 33-50-00. OPS CHECK GOOD.
- [SDR UPS04242900](https://openairdocs.org/sdr/UPS04242900), Aug 13, 2004: SWITCH. INOPERATIVE. EMERGENCY EXIT LIGHTS INOPERATIVE, COCKPIT DOOR. TURNED BATTERY SWITCH ON PLACED EMERGENCY LIGHT SWITCH TO ARMED, LIGHT CHECKS GOOD.
- [SDR UPS04242550](https://openairdocs.org/sdr/UPS04242550), Jun 9, 2004: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTS NOT OPERATING. RESEATED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL.
- [SDR UPS04242205](https://openairdocs.org/sdr/UPS04242205), Apr 7, 2004: FLAP TRACK. CRACKED. INSPECTION TYPE: C, NR 6 FLAP TRACK FAIRING I/B TRACK IS CRACKED. FAIRING TRACK REPLACED IAW SRM 51-30-02.
- [SDR UPS04242181](https://openairdocs.org/sdr/UPS04242181), Apr 7, 2004: CASTING. CRACKED. INSPECTION TYPE: C, RIGHT O/B FLAP I/B FLAP TRACK FAIRING HAS CRACKED CASTING/BRACKET. CRACKED BRACKET REMOVED IAW SRM 51-30-02 & STOP DRILLED IAW SRM 51-10-1. 
- [SDR UPS04242260](https://openairdocs.org/sdr/UPS04242260), Apr 6, 2004: ANGLE. CORRODED. INSPECTION TYPE:C LT 950 FITTING LWR SPLICE ANGLE HAS SUSPECT CORROSION UNDER THE ANGLE. ANGLE WAS ALSO FOUND CORRODED AFTER REMOVAL. ANGLE REPLACED AND BS 950 
- [SDR UPS04242241](https://openairdocs.org/sdr/UPS04242241), Apr 6, 2004: DOOR FRAME. CRACKED. INSPECTION TYPE:C LWR FWD CARGO DOOR CUTOUT FRAME, CRACK INDICATION IN AREA NR 4 FWD DOOR STOP. REPAIR CARRIED OUT IAW SMRO EO 2004-027-01 UPS ENGINEERING FILE 
- [SDR UPS04242206](https://openairdocs.org/sdr/UPS04242206), Apr 6, 2004: FRAME. CORRODED. INSPECTION TYPE: C, FUSELAGE FAIRING 3430 HAS EXTENSIVE CORROSION TO THE FORMED FRAME HOLDING THE ANCHOR NUTS (FWD SIDE OF FAIRING). REPAIR CARRIED OUT IAW SRM 
- [SDR UPS04242204](https://openairdocs.org/sdr/UPS04242204), Apr 6, 2004: BEAM. CORRODED. INSPECTION TYPE: C, RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM HAS CORROSION AFT OF BALANCE PANEL BAYS. BEAM REPLACED IAW SRM 51-30-2 AND DRG NR 65-22987
- [SDR UPS04242180](https://openairdocs.org/sdr/UPS04242180), Apr 6, 2004: FLOORBEAM. CRACKED. INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328, RBL 44. REPAIR CARRIED OUT IAW SRM 53-10-8.
- [SDR UPS04242219](https://openairdocs.org/sdr/UPS04242219), Apr 5, 2004: DRUM. CORRODED. INSPECTION TYPE:C LEFT I/B MIDFLAP O/B AFT FLAP ACTUATING DRUM CORRODED. DRUM REPLACED IAW MM 27-51-01.
- [SDR UPS04242179](https://openairdocs.org/sdr/UPS04242179), Apr 5, 2004: FLOORBEAM. CRACKED. INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 344 LBL 24. REPAIR CARRIED OUT IAW SRM 51-20-1 FIG 7.
- [SDR UPS04242178](https://openairdocs.org/sdr/UPS04242178), Apr 5, 2004: FLOORBEAM. CRACKED. INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328 RBL 24. REPAIR CARRIED OUT IAW SRM 53-10-8.
- [SDR UPS04242223](https://openairdocs.org/sdr/UPS04242223), Apr 3, 2004: RIB. CRACKED. INSPECTION TYPE:C NR 3 L/E SLAT, CRACK AT ACTUATOR ATTACH RIB (O/B RIB). REPAIR CARRIED OUT IAW SRM 51-30-02, 51-30-03, 57-50-03 & MM 28-81-11 & 27-00-00.
- [SDR UPS04242220](https://openairdocs.org/sdr/UPS04242220), Apr 3, 2004: RIB. CRACKED. INSPECTION TYPE:C NR 2 L/E SLAT CLOSURE RIB AT INBOARD END OF SLAT CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-20-1 & MM 20-10-05.
- [SDR UPS04242177](https://openairdocs.org/sdr/UPS04242177), Apr 3, 2004: SKIN. CRACKED. INSPECTION TYPE:C NR 4 K-FLAP HAS CRACK ON INNER ANTI-ICE SKIN AROUND RIVET HOLE I/B OF O/B ACTUATION LINKAGE FOR BULLNOSE. REPAIR CARRIED OUT IAW SRM 51-30-2, 
- [SDR UPS02239194](https://openairdocs.org/sdr/UPS02239194), Aug 17, 2002: STIFFENER. CORRODED. INSPECTION TYPE:C LOWER END OF STIFFENER AT WS 210, R/H WING REAR SPAR, IS CORRODED STIFFENER REPLACED IAW SMRO EO 2002-044-006, REF. UPS ENGINEERING FI LE NO. 
- [SDR UPS02239191](https://openairdocs.org/sdr/UPS02239191), Aug 15, 2002: WEB. CRACKED. INSPECTION TYPE:C CRACK FOUND IN NLG FWD L/H PRESSURE WEB AT BS 235 APPROX. CRACK REMOVED IAW SRM 51-40-2. HFEC INSPECTION CONFIRMED CRACK REMOV AL. REPAIR PART
- [SDR UPS02239120](https://openairdocs.org/sdr/UPS02239120), Aug 15, 2002: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C SUSPECT CRACK IN NLG FWD LT PRESS WEB AT BS 243.7. CRACKED AREA REMOVED IAW SRM 51-40-2 FIG 1. HFEC C/O ON THE ABOVE AREA INSP CARRIED OUT IAW
- [SDR UPS02239168](https://openairdocs.org/sdr/UPS02239168), Aug 14, 2002: SKIN. CRACKED. INSPECTION TYPE:C CRACK IN ANTI-ICE SKIN AT 5TH BAY O/B ON NO.4 KRUEGER FLAP. ANTI-ICE SKIN FOUND TO BE OUT OF LIMITS IAW SRM ADDENDIUM EO NO. B72 7-5750-3082-D
- [SDR UPS02239166](https://openairdocs.org/sdr/UPS02239166), Aug 14, 2002: SKIN. CRACKED. INSPECTION TYPE:C #3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B RIVET 3RD BAY FROM O/ B REPAIR CARRIED OUT IAW SRM ADDENDUM EO # B727-5750-3082
- [SDR UPS02239165](https://openairdocs.org/sdr/UPS02239165), Aug 14, 2002: SKIN. CRACKED. INSPECTION TYPE:C RIVET PULLED THROUGH ANTI-ICE SKIN AT #4 KRUEGER FLAP AT 8TH BAY O/B SKIN REPAIRED IAW SRM ADDENDUM EO # B727-5750-3082
- [SDR UPS02239199](https://openairdocs.org/sdr/UPS02239199), Aug 14, 2002: SPAR. CORRODED. INSPECTION TYPE:C SUSPECT CRACK ON RT WING REAR SPAR UPPER CHORD AT APPROX WS 198 AND WS 194. UPPER CHORD HORIZONTAL FLANGE BLENDED TO REMOVE DAMAGE AT WS 196, 
- [SDR UPS02239119](https://openairdocs.org/sdr/UPS02239119), Aug 14, 2002: WEB. CRACKED. INSPECTION TYPE:C LIGHTENING HOLE IN AFT AIRSTAIR TORQUE BOX AT BS 1243 RHS IS CRACKED WEB REPAIR CARRIED OUT IAW SRM 51-10-4
- [SDR UPS02239167](https://openairdocs.org/sdr/UPS02239167), Aug 13, 2002: DOUBLER. CRACKED. INSPECTION TYPE:C SUSPECT CRACK AT FASTNER BESIDE REPAIR AT NLG WHEEL WELL LEFT FWD PR ESS WEB AT BS 269.5 REPAIR DOUBLER REMOVED IAW SRM 51-30-2 NDT CARRIED OU
- [SDR UPS02239197](https://openairdocs.org/sdr/UPS02239197), Aug 13, 2002: WEB. CRACKED. INSPECTION TYPE:C CRACKS FOUND IN NLG W/WELL PRESSURE WEB AT BS 269.5, 4" BELOW THE CE ILING ON THE R/H PRESSURE WEB AREA. NEW WEB AND DOUBLERS FABRICATED AND I
- [SDR UPS02239190](https://openairdocs.org/sdr/UPS02239190), Aug 13, 2002: SKIN. CORRODED. INSPECTION TYPE:C CORROSION FOUND AT LAP JOINT S4L. LFEC INSPECTION CARRIED OUT FROM B S 360 TO BS 440. MATERIAL LOSS INDICATION FROM BS 440 TO BS 411 APPR OX. 
- [SDR UPS02239187](https://openairdocs.org/sdr/UPS02239187), Aug 13, 2002: STIFFENER. CRACKED. INSPECTION TYPE:C SUSPECT CRACK ON AFT PRESSURE BULKHEAD VERTICAL BEAM LT AT W/L 264 APPROX LBL 26.83. HFEC INSPECTION CONFIRMED CRACK. CRACK STOP DRILLED IAW E
- [SDR UPS02239115](https://openairdocs.org/sdr/UPS02239115), Aug 13, 2002: STIFFENER. CRACKED. INSPECTION TYPE:C WING TO BODY FAIRING 3409 HAS A CRACKED FWD FRAME STIFFENER ANGLE. FABRICATED AND INSTALLED NEW STIFFENER IAW SRM 53-50-1 FIG 4 AND SRM 51-2 0

All 254: https://openairdocs.org/deregistered/N926UP-2007-09-19/reports.md

## 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 19900409012739I](https://openairdocs.org/incident/19900409012739I), Apr 9, 1990: Boeing 72731C (N926UP), Des Moines, IA, Minor damage. NR2 engine fire warning. Secured and returned. Found bleed air leak at manifold flange. Bolts not safety wired.

## Other aircraft with N926UP

- [Registered now](https://openairdocs.org/aircraft/N926UP): Boeing 767-300F, S/N 70802

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