# N924UP: 1967 Boeing 727-31C, registration cancelled 2007-08-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 24, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-31C](https://openairdocs.org/model/boeing-727-31c) (registry code 1384011)
- 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: 19234
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard
- Certificate issued: July 22, 1982
- Last registry action: September 19, 2006
- Mode S code: ACCED6
- Owner when cancelled: [United Parcel Service](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE)
- 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/N924UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=924UP
- Page: https://openairdocs.org/deregistered/N924UP-2007-08-24

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 727-31C: https://openairdocs.org/model/boeing-727-31c.md

## Service difficulty reports (108, newest 50)

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

- [SDR UPS02237711](https://openairdocs.org/sdr/UPS02237711), Feb 6, 2002: CASTING. CORRODED. INSPECTION TYPE:C #5 FLAP TRACK ATTACH POINT ON LWR SURFACE OF WING, CORROSION EXIDENT IN AFT PAD, O/B HOLE. CORROSION SEEMS TO BE CONFINED TO BARREL NUT CASTIN
- [SDR UPS02237694](https://openairdocs.org/sdr/UPS02237694), Feb 6, 2002: FRAME. CRACKED. INSPECTION TYPE:C RH AFT FRAME ON E & E DOOR CRACKED FRAME REPLACED IAW DRAWING # 65-02163
- [SDR UPS02237712](https://openairdocs.org/sdr/UPS02237712), Feb 4, 2002: SUPPORT. CRACKED. INSPECTION TYPE:C, AFT AIRSTAIRS ACTUATOR FITTING SUPPORT ANGLE CRACKED IN AFT RT TORQUE BOX AT STA 1273. REPAIRED IAW EO B727-5310-1239.
- [SDR UPS01237262](https://openairdocs.org/sdr/UPS01237262), Nov 6, 2001: ROD. BROKEN. INSPECTION TYPE:PRD INBOARD SPOILER CASTING SUPPORT ROD BROKEN LT WING. INBOARD SPOILER LT WING CASTING SUPPORT ROD REPLACED.
- [SDR UPS00233591](https://openairdocs.org/sdr/UPS00233591), Aug 18, 2000: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT CAME ON IN FLIGHT INTERMITTENTLY. EMERGENCY LIGHT REPLACED PER MM 33-50, CHECKED OK.
- [SDR UPS00233505](https://openairdocs.org/sdr/UPS00233505), Jul 25, 2000: STRINGER. CORRODED. INSPECTION TYPE:C&SI, FOLLOWING REWORK AT BS 1183 STR 15R TO 5R HOLES AT 10R HAVE EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIR CARRIED OUT IAW SMRO EO 2000-0
- [SDR UPS00233498](https://openairdocs.org/sdr/UPS00233498), Jul 25, 2000: STRUCTURE. CRACKED. INSPECTION TYPE:C&SI, SEVERAL CRACKS IN FWD CARGO DOOR. FWD CARGO DOOR REPLACED IAW MM 2-31-01.
- [SDR UPS00233455](https://openairdocs.org/sdr/UPS00233455), Jul 24, 2000: FITTING. CORRODED. INSPECTION TYPE:C+SI, AFTER REWORK OF BS 360 ON SMRO EO2000-026-001, TWO HOLES AT STR END FITTING 3L ARE REAMED UP TO MAX LIMITS AND STILL SHOW EVIDENCE OF CORR
- [SDR UPS00233486](https://openairdocs.org/sdr/UPS00233486), Jul 20, 2000: ANGLE. CRACKED. INSPECTION TYPE:C&SI, G-NET ATTACH POINT AT BS 365 BETWEEN STR 15L AND 16L HAS CRACKED ANGLE. INSTALLED NEW ANGLE AND CLIPS IAW SRM 51-30-02.
- [SDR UPS00233485](https://openairdocs.org/sdr/UPS00233485), Jul 20, 2000: FRAME. CRACKED. INSPECTION TYPE:C&SI, AFT CARGO DOOR HAS SUSPECT CRACKED FRAME AT STA 1072 BETWEEN NR 5 ST OPS. REMOVED AND REPLACED FRAME IAW SRM 53-30-2.
- [SDR UPS00233417](https://openairdocs.org/sdr/UPS00233417), Jul 20, 2000: ANGLE. CRACKED. INSPECTION TYPE:C&SI, FWD CARGO DOOR BS 577 AFT ANGLE CRACKED AT HINGE ATTACHMENT FWD CARGO DOOR REPLACED REF NRC 175922 FOR REPLACEMENT.
- [SDR UPS00233482](https://openairdocs.org/sdr/UPS00233482), Jul 19, 2000: BRACKET. CRACKED. INSPECTION TYPE:C&SI, FIRE WIRE BRACKET CRACKED AT BS 1010 LBL 45.5 LWR SURFACE OF FLOOR I T CARGO BAY. REPAIRED IAW SRM 51-40-3 FIG 1.
- [SDR UPS00233481](https://openairdocs.org/sdr/UPS00233481), Jul 19, 2000: BRACKET. CRACKED. INSPECTION TYPE:C&SI, SUSPECT CRACK TO HORIZ STIFFENER SUPPORT BRACKET AT BS 1183 RT AFT ENTRY UPPER DOOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-30-2.
- [SDR UPS00233416](https://openairdocs.org/sdr/UPS00233416), Jul 19, 2000: BOLT. CRACKED. INSPECTION TYPE:C&SI, ENGINE NR 2 CROSS STRUT AFT ATTACH BOLT FOUND CRACKED DURING NDI CHECK. BOLT REPLACED IAW MM 71-21-12.
- [SDR UPS00233470](https://openairdocs.org/sdr/UPS00233470), Jul 18, 2000: ANGLE. CORRODED. INSPECTION TYPE:C+SI, CORROSION ON LATERIAL SUPPORT ANGLE BS 850 LBL 6 AT DELTA BEAM. CORROSION ON SUPPORT ANGLE OUT OF LIMITS. NEW ANGLE FABRICATED IAW SRM 51-
- [SDR UPS00233502](https://openairdocs.org/sdr/UPS00233502), Jul 17, 2000: STRINGER. CRACKED. INSPECTION TYPE:C&SI, STR 10R AT BS 1105 HAS CRACK DUE TO CORROSION. REPAIR CARRIED OUT IAW SRM 51-40-4 FIG 1.
- [SDR UPS00233487](https://openairdocs.org/sdr/UPS00233487), Jul 17, 2000: HINGE. CORRODED. INSPECTION TYPE:C&SI, NR 5 BALANCE BAY HINGE HALF RT SIDE CORRODED BEYOND LIMITS (AFT HINGE HALF). REPLACED HINGE HALF AND HARDWARE IAW MM 27-30-21.
- [SDR UPS00233483](https://openairdocs.org/sdr/UPS00233483), Jul 17, 2000: FRAME. CRACKED. INSPECTION TYPE:C&SI, 2 SUSPECT CRACKS ON FRAME BS 277 ON RT SIDE OF CONTROL CABIN AT STR 15 AND 16. FRAME REPAIRED IAW SRM 51-40-2 FIG 1.
- [SDR UPS00233477](https://openairdocs.org/sdr/UPS00233477), Jul 17, 2000: BEAM. CORRODED. INSPECTION TYPE:C&SI, FWD CARGO BAY CORROSION ON I BEAM LWR CHORD LWR SURFACE AT BS 500 BL 0. REPAIR CARRIED OUT IAW SMRO EO 2000-026-008 UPS ENGINEERING FILE 7
- [SDR UPS00233454](https://openairdocs.org/sdr/UPS00233454), Jul 17, 2000: LINK ROD. CRACKED. INSPECTION TYPE:C+SI, CRACKED LINK AT LT MLG LINKAGE TO AIR GROUND SENSE. AIR GROUND SENSER LINK REPLACED IAW MM 20-80-01. FUNCTION CHECKED IAW MM 32-31-11 PG 5
- [SDR UPS00233427](https://openairdocs.org/sdr/UPS00233427), Jul 17, 2000: SKIN. CRACKED. INSPECTION TYPE:C&S,I ENGINE NR 1 THRUST REVERSER UPPER DOOR INNER RAMP SKIN CRACKED. NOTE: CRACK COMING OUT FROM UNDER PREVIOUS PATCH REPAIR. REPAIR CARRIED OU
- [SDR UPS00233412](https://openairdocs.org/sdr/UPS00233412), Jul 17, 2000: STIFFENER. CORRODED. INSPECTION TYPE:C&SI, CONTROL CABIN, HORIZ STIFFENER ON BS 251.6 IS CORRODED ON LT SIDE AT WL 220 APPROX. BRACKET REPLACED IAW SRM 51-20-01 & SRM 51-30-02.
- [SDR UPS00233406](https://openairdocs.org/sdr/UPS00233406), Jul 17, 2000: BRACKET. CRACKED. INSPECTION TYPE:C&SI, ENGINE NR 3 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-00.
- [SDR UPS00233405](https://openairdocs.org/sdr/UPS00233405), Jul 17, 2000: BRACKET. CRACKED. INSPECTION TYPE:C&SI, ENGINE NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-00.
- [SDR UPS00233459](https://openairdocs.org/sdr/UPS00233459), Jul 16, 2000: MOUNT. CORRODED. INSPECTION TYPE:C+SI, CORROSION ON LWR ANTENNA SUPPORT BS 820 AT CENTER LINE. CORROSION REMOVED IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS. CORRODED ANGLE SUPPO
- [SDR UPS00233468](https://openairdocs.org/sdr/UPS00233468), Jul 15, 2000: FLOORBEAM. CORRODED. INSPECTION TYPE:C+SI, BS 328 FLOORBEAM HAS SURFACE CORROSION AROUND FASTENERS ON TOP CAP, LBL30. CORROSION REMOVED IAW MM SRM 51-10-06. AREA FOUND TO BE OUT OF 
- [SDR UPS00233414](https://openairdocs.org/sdr/UPS00233414), Jul 15, 2000: STRINGER. CORRODED. INSPECTION TYPE:C&SI, CORROSION ON STR 24R AT BS 460. REPAIR CARRIED OUT IAW SRM 53-10-1 AND SRM 53-10-3.
- [SDR UPS00233504](https://openairdocs.org/sdr/UPS00233504), Jul 14, 2000: FLANGE. CORRODED. INSPECTION TYPE:C&SI, NR 3 FLAP TRACK FWD ATTACH FLANGE UPPER SURFACE CENTRE HOLE AND O/B HOLE CORRODED. REPAIR CARRIED OUT IAW SMRO EO 2000-026-004 UPS ENGINEE
- [SDR UPS00233503](https://openairdocs.org/sdr/UPS00233503), Jul 14, 2000: FLANGE. CORRODED. INSPECTION TYPE:C&SI, NR 3 FLAP TRACK AFT ATTACH FLANGE AND HOLES CORRODED. REPAIR CARRIED OUT IAW SMRO EO 2000-02-004 UPS ENGINEERING FILE NR 727-57-2172.
- [SDR UPS00233479](https://openairdocs.org/sdr/UPS00233479), Jul 14, 2000: CARRIAGE. CORRODED. INSPECTION TYPE:C&SI, NR 2 FLAP CARRIAGE SPINDLE THREADS CORRODED I/B DEADWEIGHT ROLLER HOLE CORRODED. REPLACED IAW OHM 57-58-01.
- [SDR UPS00233478](https://openairdocs.org/sdr/UPS00233478), Jul 14, 2000: BEAM. CRACKED. INSPECTION TYPE:C&SI, CRACK FOUND AT NR 8 SPOILER SUPPORT BEAM I/B OF I/B HINGE. REPAIR CARRIED OUT IAW SMRO EO 2000-026-002 UPS ENGINEERING FILE NR 727-57-2169
- [SDR UPS00233457](https://openairdocs.org/sdr/UPS00233457), Jul 14, 2000: BOLT. CORRODED. INSPECTION TYPE:C+SI, BS1183 TENSION BOLTS CORRODED ABOVE STR 8R. REMOVED SUFFICIENT BOLTS TO VERIFY CONDITION OF SPLICE. BOLTS REMOVED FROM STR 5R - 15R BOLTS 
- [SDR UPS00233426](https://openairdocs.org/sdr/UPS00233426), Jul 14, 2000: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C&SI, SUSPECT CRACK AT NOSE WHEEL WELL SIDEWALL AT RBL 23 AND STA 267 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1.
- [SDR UPS00233424](https://openairdocs.org/sdr/UPS00233424), Jul 14, 2000: MOUNT. CORRODED. INSPECTION TYPE:C&SI, ENGINE NR 1 FWD MOUNT HOLES CORROSION IN BOTH I/B HOLES AND AFT O/B HOLE. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A.
- [SDR UPS00233501](https://openairdocs.org/sdr/UPS00233501), Jul 13, 2000: BRACKET. CRACKED. INSPECTION TYPE:C&SI, LT WING T/E SUPPORT BRACKET CRACKED DIRECTLY AFT OF NR 4 SPOILER PANEL I/B HINGE. BRACKET REPLACED IAW SRM 51-30-02.
- [SDR UPS00233456](https://openairdocs.org/sdr/UPS00233456), Jul 13, 2000: FRAME. CRACKED. INSPECTION TYPE:C+SI, SUSPECT CRACK ON VERTICAL CHORD AT BS 178 BULKHEAD TO SKIN ATTACH POINT, WL 200 APPROX, LT SIDE. NDT REQUIRED TO CONFIRM. CRACK CONFIRMED.
- [SDR UPS00233404](https://openairdocs.org/sdr/UPS00233404), Jul 13, 2000: BRACKET. CRACKED. INSPECTION TYPE:C&SI, LT WING, T/E SUPPORT BRACKET CRACKED 6 INCHES O/B OF NR 5 SPOILER PANEL I/B HINGE. BRACKET REPLACED IAW SRM 51-20-01 & SRM 51-30-02.
- [SDR UPS00233484](https://openairdocs.org/sdr/UPS00233484), Jul 12, 2000: SKIN. CORRODED. INSPECTION TYPE:C&SI, SUSPECT COROSSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER BS 1090 ABOVE STR 14 RT. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3.
- [SDR UPS00233480](https://openairdocs.org/sdr/UPS00233480), Jul 12, 2000: SPLICE PLATE. CRACKED. INSPECTION TYPE:C&SI, ON REMOVAL OF BS 930 SPLICE PLATE AT STR 14 CRACK FOUND IN LWR END OF FUSELAGE UPPER FRAME. REPAIR CARRIED OUT ON FRAME IAW SRM 53-10-4 FI
- [SDR UPS00233453](https://openairdocs.org/sdr/UPS00233453), Jul 12, 2000: SKIN. CORRODED. INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON SKIN BS 1140 BETWEEN S3R & 4R. REPAIRED AREA IAW SRM 53-30-3 & UPS EO B727-5330-0509 APPEX 8.3 WEIGHT OF REPAIR
- [SDR UPS00233408](https://openairdocs.org/sdr/UPS00233408), Jul 12, 2000: CARRIAGE. CORRODED. INSPECTION TYPE:C&SI, NR 8 FLAP CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE IAW MM 27-51-13.
- [SDR UPS00233407](https://openairdocs.org/sdr/UPS00233407), Jul 12, 2000: CARRIAGE. CORRODED. INSPECTION TYPE:C&SI, NR 1 FLAP CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE IAW MM 27-51-13.
- [SDR UPS00233423](https://openairdocs.org/sdr/UPS00233423), Jul 11, 2000: BUTT JOINT. CORRODED. INSPECTION TYPE:C&SI, EVIDENCE OF CORROSION BS 1080 BUTT JOINT AFT EDGE BETWEEN S4L AND 2L. REPAIR CARRIED OUT IAW EO B727-5330-1177.
- [SDR UPS00233422](https://openairdocs.org/sdr/UPS00233422), Jul 11, 2000: BUTT JOINT. CORRODED. INSPECTION TYPE:C&SI, EVIDENCE OF CORROSION AT BS 1080 BUTT JOINT AFT EDGE (VIEWED INTERNALLY) BETWEEN S5R AND 2R. REPAIR CARRIED OUT IAW EO B727-5330-1177.
- [SDR UPS00231624](https://openairdocs.org/sdr/UPS00231624), Feb 15, 2000: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT OVER COCKPIT DOOR AND ENTRANCE DOOR, GOT NO LIGHT WHEN TESTED BY CREW PRIOR TO DEPARTURE. REMOVED AND REPLACED BATTERY PACK. BATTERY REQUIR
- [SDR UPS99230750](https://openairdocs.org/sdr/UPS99230750), Sep 23, 1999: FRAME. CRACKED. INSPECTION TYPE:C, BS 930 FRAME CRACK ON HORIZONTAL LEG OF FRAME AT FLOOR LEVEL. REPAIR TO FRAME CARRIED OUT IAW SMRO EO 99-30-003 UPS ENGINEERING FILE NR 727-5
- [SDR UPS99230723](https://openairdocs.org/sdr/UPS99230723), Sep 20, 1999: BRACKET. CRACKED. INSPECTION TYPE:C, FLOOR SUPPORT BRACKET CRACKED AT BS 440 RT IN E & E BAY. BRACKET REPAIRED IAW SRM 51-40-3 FIG 1 AND REPROTECTED IAW SRM 51-10 -2.
- [SDR UPS99230722](https://openairdocs.org/sdr/UPS99230722), Sep 20, 1999: BEAM. CRACKED. INSPECTION TYPE:C, DURING REMOVAL TO FACILITATE REPLACEMENT OF BS 940 FITTING, FLAP ROLLER TRACK SUPPORT FOUND CRACKED IN THREE PLACES. BEAM ASSY REPLACED IAW S
- [SDR UPS99230724](https://openairdocs.org/sdr/UPS99230724), Sep 18, 1999: ANGLE. CRACKED. INSPECTION TYPE:C, ANGLE CRACKED ON AFT SIDE OF FRAME BS 560 STR 17 L. ANGLE REPLACED IAW SRM 51-40-03 FIG 1 & SRM 53-10-02.
- [SDR UPS99230749](https://openairdocs.org/sdr/UPS99230749), Sep 17, 1999: T-EDGE. LIGHTNING STRIKE. INSPECTION TYPE:C, LIGHTNING DISCHARGE DAMAGE RT ELEVATOR TIP T-EDGE AT BASE LWR SURFACE & STRUCTURE AT PREVIOUS REPAIR. REPAIR CARRIED OUT IAW SRM 55-20-3 FIG 

All 108: https://openairdocs.org/deregistered/N924UP-2007-08-24/reports.md

## Other aircraft with N924UP

- [Registered now](https://openairdocs.org/aircraft/N924UP): Boeing 767-300F, S/N 68370

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