# N933UP: 1968 Boeing 727-25C, 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 727-25C](https://openairdocs.org/model/boeing-727-25c) (registry code 138400H) - 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: 19857 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 14, 1968 - Certificate issued: May 20, 1985 - Last registry action: September 19, 2006 - Mode S code: ACF29E - 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/N933UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=933UP - Page: https://openairdocs.org/deregistered/N933UP-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 727-25C: https://openairdocs.org/model/boeing-727-25c.md ## Service difficulty reports (157, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS02238717](https://openairdocs.org/sdr/UPS02238717), Jul 1, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:N/A EXIT LIGHT ABOVE COCKPIT ENTRANCE DOOR DOES NOT TEST. CABIN DOOR ENTRANCE LIGHT CHECKS OK BUT CHARGE STAT US IS IN-DOUBT. R/R EMERGENCY EXIT - [SDR UPS02238567](https://openairdocs.org/sdr/UPS02238567), Jun 7, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BATTERY, OPS CHECKS GOOD. - [SDR UPS02237797](https://openairdocs.org/sdr/UPS02237797), Feb 7, 2002: ANGLE. BULGED. INSPECTION TYPE:C LT AFT NOSE W/W DOOR CUTOUT HAS BULGE FASTENERS PULLING OFF BS 320 TO BS 350. REPLACED LEFT LOWER CHORD ANGLE AT NWW AREA IAW B727 SRM 51-30-2 - [SDR UPS02237796](https://openairdocs.org/sdr/UPS02237796), Feb 7, 2002: SKIN. CRACKED. INSPECTION TYPE:C LT FUSELAGE SKIN HAS CRACK STARTING AT FASTENER CUT OUT BS 254 STR 10L CRACK DOES NOT NEED STOP DRILL IT RUNS FROM FASTENER HOLE TO EDGE OF SK - [SDR UPS02237795](https://openairdocs.org/sdr/UPS02237795), Feb 7, 2002: SKIN. BULGED. INSPECTION TYPE:C UPPER FUSELAGE SKIN HAS BULGE AT BUTT JOINT BS 521 STR 3L - 4R. - [SDR UPS02237794](https://openairdocs.org/sdr/UPS02237794), Feb 7, 2002: SKIN. CANNING. INSPECTION TYPE:C RT FWD FUSELAGE SKIN HAS OIL CAN, PREVIOUSLY REWORKED BS 340 STR 19R. - [SDR UPS02237493](https://openairdocs.org/sdr/UPS02237493), Jan 22, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS OVER MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES, OPS CHECKS NORMAL. - [SDR UPS01237360](https://openairdocs.org/sdr/UPS01237360), Dec 10, 2001: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A BOTH EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN COCKPIT EMERGENCY LIGHTS. REPLACED EMERGENCY LIGHT ASSY OVER EXIT DOOR P/N ON AND OFF 10-0 - [SDR UPS01235463](https://openairdocs.org/sdr/UPS01235463), Mar 28, 2001: WINDSHIELD. FAILED. FIRST OFFICERS WINDSHIELD SHATTERED. OLD WINDOW REMOVED NEW WINDOW PARTIALLY INSTALLED / R&R R1 WINDOW PER M/M 56-11-1 WINDOW HEAT OPS CHECK GOOD - [SDR UPS01234968](https://openairdocs.org/sdr/UPS01234968), Feb 13, 2001: FIRE LOOP. INOPERATIVE. INSPECTION TYPE:IN ENG NR 3 A-LOOP WILL NOT TEST. *S/D* FOUND CONNECTOR D354J CONTAMINATED WITH DIRT AND MOISTURE. CLEANED SAME THOROUGHLY. TESTED NORMAL. M2091 - [SDR UPS00234506](https://openairdocs.org/sdr/UPS00234506), Nov 22, 2000: STRUCTURE. CRACKED. INSPECTION TYPE:PRE NR 4 LEADING EDGE SLAT CRACKED. AWAITING LOG PAGE ENTRY. - [SDR UPS00233587](https://openairdocs.org/sdr/UPS00233587), Aug 16, 2000: FLAP TRACK. CORRODED. INSPECTION TYPE:SI, NR 1 FLAP TRACK FWD ATTACH LUG FACES I/B AND O/B HAVE LIGHT SURFACE RUST (CORROSION C57-581-06.00-03). REMOVED CORROSION FROM NR 1 FLAP TRAC - [SDR UPS00233586](https://openairdocs.org/sdr/UPS00233586), Aug 16, 2000: FLAP TRACK. CORRODED. INSPECTION TYPE:SI, CORROSION (SDN C57-581-06.00-04) ON NR 7 FLAP TRACK AFT CENTER MOUNT HOLE. REMOVED CORROSION ON NR 7 FLAP TRACK AFT CENTER MOUNT HOLE AND RE - [SDR UPS00233585](https://openairdocs.org/sdr/UPS00233585), Aug 16, 2000: FLAP TRACK. CORRODED. INSPECTION TYPE:SI, CORROSION (SDN C57-581-06.00-04) ON NR 7 FLAP TRACK FWD ATTACH POINT I/B FLANGE AROUND BUSHING HOLE. REMOVED CORROSION ON NR 7 FLAP TRACK FW - [SDR UPS00233609](https://openairdocs.org/sdr/UPS00233609), Jul 31, 2000: WEB. CORRODED. INSPECTION TYPE:SI, CORROSION ON UPPER SURFACE OF SHEAR WEB AT BS 640, WL 208 LBL 63. SHEAR WEB REPLACED AT STA 630 - 660, LBL 45-LBL 62, WL 208 PER ER NR 00-09 - [SDR UPS00233568](https://openairdocs.org/sdr/UPS00233568), Jul 29, 2000: FITTING. CRACKED. INSPECTION TYPE:SI, STRINGER FITTING IS CRACKED AT BS 365 STR 26L. REMOVED AND REPLACED STRINGER FITTING. - [SDR UPS00233588](https://openairdocs.org/sdr/UPS00233588), Jul 27, 2000: FITTING. CRACKED. INSPECTION TYPE:SI, NR 1 K-FLAP O/B ATTACH LUG FITTING ON K-FLAP UPPER O/B SIDE IS CRACKED. REMOVED AND INSTALLED NEW K-FLAP ASSY PER MM 27-81-01. - [SDR UPS00233540](https://openairdocs.org/sdr/UPS00233540), Jul 27, 2000: SKIN. CORRODED. INSPECTION TYPE:C, CORROSION ON LWR RUDDER RT SKIN AT STA 120.6 IN BELOW FRONT SPAR. REPAIRED PER SRM 55-20-3 PG 1 STEP 3 & 4 AND SRM 51-40-5 PG 20 & 22 STEP 13 - [SDR UPS00233612](https://openairdocs.org/sdr/UPS00233612), Jul 26, 2000: STRINGER. CRACKED. INSPECTION TYPE:SI, RIGHT WING UPPER STR 17 OUTSIDE OF RIB AT WS 304 IS CRACKED. REMOVED CRACK STRINGER SECTION. FABRICATED AND INSTALLED NEW SECTION, ALL WORK - [SDR UPS00233611](https://openairdocs.org/sdr/UPS00233611), Jul 26, 2000: FLAP TRACK. CORRODED. INSPECTION TYPE:SI, NR 5 FLAP TRACK IS RUSTED AT MAIN LANDING GEAR DOOR FWD FITTING ATTACH BOLTS. REMOVED AND REPLACED FLAP TRACK PER TC 57-581-04-4D. - [SDR UPS00233558](https://openairdocs.org/sdr/UPS00233558), Jul 26, 2000: CARRIAGE. CORRODED. INSPECTION TYPE:SI, CORROSION (SDN C57-581-04.00-04) IN BORE OF SPINDLE FOR NR 6 FLAP CARRIAGE. REMOVED AND REPLACED NR 6 FLAP CARRIAGE PER MM 25-51-03. - [SDR UPS00233513](https://openairdocs.org/sdr/UPS00233513), Jul 26, 2000: MOUNT. CORRODED. INSPECTION TYPE:SI, CORROSION ON NR 6 FLAP TRACK AFT ATTACH MOUNT BLOCK OUT OF LIMITS IAW SRM 51-30-2. REMOVED AND REPLACED MOUNT BLOCK IAW SRM 51-30-5. - [SDR UPS00233512](https://openairdocs.org/sdr/UPS00233512), Jul 26, 2000: FITTING. CORRODED. INSPECTION TYPE:SI, NR 6 FLAP TRACK SPOILER BEAM MOUNT FITTINGS CORRODED OUT OF LIMITS IAW SRM 51-30-2 ON RT WING. FOUND WHILE WORKING NRC 178771. REMOVED CORRO - [SDR UPS00233557](https://openairdocs.org/sdr/UPS00233557), Jul 25, 2000: FITTING. CORRODED. INSPECTION TYPE:SI, MAIN DECK FLOOR WEB FITTING CORRODED (C53-224-01.00-03) BETWEEN LEFT CREASE BEAM AND DITCHING PAN, FWD OF BS 1183 BULKHEAD BS 1180 LBL 65, W - [SDR UPS00233556](https://openairdocs.org/sdr/UPS00233556), Jul 25, 2000: FLOORBEAM. CORRODED. INSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) FWD CARGO BAY BS 660 FLOORBEAM FWD SIDE UPPER FLANGE LOWER SURFACE AT LBL 45 TO LBL 50. REMOVED CORROSION IN DE - [SDR UPS00233555](https://openairdocs.org/sdr/UPS00233555), Jul 25, 2000: FLOORBEAM. CORRODED. INSPECTION TYPE:SI, CORROSION (C53-111-01.00-02) FWD CARGO BAY STA 540 FLOORBEAM FWD SIDE, UPPER FLANGE, LWR SURFACE AT LBL 45. REMOVED CORROSION ON UPPER CHORD - [SDR UPS00233610](https://openairdocs.org/sdr/UPS00233610), Jul 23, 2000: DRUM. CORRODED. INSPECTION TYPE:SI, RT MLG MANUAL EXTENSION CABLE DRUM IS CORRODED. REMOVED AND REPLACED PER MM 32-34-01. - [SDR UPS99228760](https://openairdocs.org/sdr/UPS99228760), Feb 17, 1999: SPAR CHORD. CORRODED. INSPECTION TYPE-C,CORROSION (C57-581-03.00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIRED IAW ERO 99-5030. - [SDR UPS99228742](https://openairdocs.org/sdr/UPS99228742), Feb 17, 1999: CHORD. CORROSION. INSPECTION TYPE:C CORROSION (C57-581-03-00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIRED IAW ERO 99-5030. - [SDR UPS99228633](https://openairdocs.org/sdr/UPS99228633), Feb 2, 1999: SEAT TRACK. CRACKED. INSPECTION TYPE:C WHILE ACCESSING OVERWING FRAMES FOUND SEAT TRACK AT STA 760 RBL 65 WL 208 CRACKED AT O/B FLANGE. REPLACED SEAT TRACK FROM BS 760 TO BS 848 PER - [SDR UPS99228558](https://openairdocs.org/sdr/UPS99228558), Jan 27, 1999: SKIN. CORRODED. INSPECTION TYPE-C, NR 4 K-FLAP AND BULLNOSE ARE CORRODED AT INBD LOWER BONDING JUMPER ATTACHMENT POINTS. REPLACED K-FLAP PER MM 27-81-01 AND ADJUST/TEST PER 727 - [SDR UPS99228530](https://openairdocs.org/sdr/UPS99228530), Jan 25, 1999: SKIN. CORRODED. INSPECTION TYPE-C ,CORROSION RT ELEVATOR AROUND BASE OF O/B STATIC WICK. REPLACED SKIN PER SRM 51-30-2 AND SRM 55-20-3. - [SDR UPS99228559](https://openairdocs.org/sdr/UPS99228559), Jan 15, 1999: FOREFLAP. CORRODED. INSPECTION TYPE-C, LEFT WING O/B FOREFLAP HAS .25 X 3.5 AREA OF DELAMINATION. TAP TESTED, FOUND ADDITIONAL DELAMINATION. FOUND CORRSION ON SPAR. REPLACED O/B FO - [SDR UPS99228674](https://openairdocs.org/sdr/UPS99228674), Jan 14, 1999: S DUCT. CRACKED. INSPECTION TYPE:C NR 2 ENGINE S DUCT HAS 5 INCH CRACK IN THE CENTER SECTION 4 RIBS FWD OF THE PRODUCTION BREAK, LT SIDE APPRX 8:00 POSITION. REMOVED DAMAGED ARE - [SDR UPS99228538](https://openairdocs.org/sdr/UPS99228538), Jan 13, 1999: SKIN. CORRODED. INSPECTION TYPE-C, CORROSION (C55-300-10.00-01) ON LT ELEVATOR AROUND I/B STATIC WICK BASE. REMOVED CORROSION OUT OF LIMITS, REPLACED SKIN PANEL. ALL WORK DONE - [SDR UPS98226858](https://openairdocs.org/sdr/UPS98226858), Jun 10, 1998: CONTROL VALVE. FAILED. INSPECTION TYPE N/A, LEFT PACK TRIPPED OFF LIGHT ON LANDING ROLLOUT. LEFT PACK SWITCH DID NOT TURN OFF, WHITE SMOKE ENTERED COCKPIT. LOST CONTROL OF PACK EVEN W - [SDR UPS98226177](https://openairdocs.org/sdr/UPS98226177), Mar 25, 1998: BATTERY PACK. DISCHARGED. INSPECTION TYPE-N/A, COCKPIT EMERGENCY EXIT LIGHT INOP. FOUND BOTH BATTERIES TO BE DEAD AND OUT OF DATE. REMOVED AND REPLACED TWO BATTERIES PER MM33-50-10. SYST - [SDR UPS98226176](https://openairdocs.org/sdr/UPS98226176), Mar 25, 1998: LIGHT. INOPERATIVE. INSPECTION TYPE-N/A, FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. - [SDR UPS97225318](https://openairdocs.org/sdr/UPS97225318), Dec 1, 1997: LIGHT. INOPERATIVE. INSPECTION TYPE-N/A, EMERGENCY LIGHT WOULD NOT TEST, BATTERIES OK. REPLACED LIGHT ASSY. - [SDR UPS97225089](https://openairdocs.org/sdr/UPS97225089), Nov 14, 1997: LINE. CRACKED. INSPECTION TYPE-N/A, ON GEAR RETRACTION RIGHT MAIN GEAR DID NOT RETRACT, A HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. A PRESSURE WAS ZERO AND QUANTITY WA - [SDR UPS97224364](https://openairdocs.org/sdr/UPS97224364), Sep 4, 1997: SKIN. DELAMINATED. INSPECTION TYPE-C, NR 7 SPOILER HAS A 4 BY 5 AREA OF DELAMINATION ON LOWER SURFACE O/B FWD CORNER. REPAIRED DELAMINATION IAW SRM 57-50-06 FIG 5. - [SDR UPS97224403](https://openairdocs.org/sdr/UPS97224403), Sep 3, 1997: SEAT TRACK. CRACKED. INSPECTION TYPE:C SEAT TRACK CRACKED AT BS 660 LBL 65. REMOVED AND REPLACED SEAT TRACK AT BS 660 LBL 65. - [SDR UPS97224365](https://openairdocs.org/sdr/UPS97224365), Sep 3, 1997: SKIN. CORRODED. INSPECTION TYPE-C, NR 4 K-FLAP O/B BONDING JUMPER HOLE HAS CORROSION AROUND OLD BONDING JUMPER LOCATION. CORROSION REWORK OUT OF LIMITS IAW UPS EO B727-5740-398 - [SDR UPS97224367](https://openairdocs.org/sdr/UPS97224367), Sep 2, 1997: FRAME. CRACKED. INSPECTION TYPE-C, WHILE WORKING EO B727-5310-5596A (940 FRAME INSP) FOUND LT 930 FRAME CRACKED AT WL 228. REPAIRED FRAME IAW EO B727-5310-2580 AND BOEING DRAWI - [SDR UPS97224366](https://openairdocs.org/sdr/UPS97224366), Sep 2, 1997: RIB. CRACKED. INSPECTION TYPE-C, NR 5 K-FLAP I/B LOWER BONDING JUMPER ON K-FLAP HAS CRACK EMANATING FROM HOLE. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS ON NR 5 K- - [SDR UPS97224368](https://openairdocs.org/sdr/UPS97224368), Sep 1, 1997: FRAME. CRACKED. INSPECTION TYPE-C, WHILE WORKING EO B727-5310-5596A (940 FRAME INSP) FOUND RT 930 FRAME CRACKED AT WL 228. REPAIRED CRACKED FRAME IAW EO B727-5310-2580 AND BOEI - [SDR UPS97224405](https://openairdocs.org/sdr/UPS97224405), Aug 29, 1997: FITTING. CORRODED. INSPECTION TYPE:C CORROSION ON UNDERSIDE OF HORIZONTAL FLANGE OF BS 740 BODY FITTING LBL 65 WL 207. BODY FITTING REPAIRED IN ACCORDANCE WITH BFG ER 97-2479 AND - [SDR UPS97222567](https://openairdocs.org/sdr/UPS97222567), Apr 11, 1997: BATTERY. DISCHARGED. INSPECTION TYPE P/F, EMERGENCY LIGHTS DID NOT COME ON WHEN TESTED AT COCKPIT DOOR. REPLACED BATTERIES ON EMERGENCY BAT PACK LIGHT (S/N 39810). - [SDR UPS96205974](https://openairdocs.org/sdr/UPS96205974), Apr 12, 1996: SUPPORT FITTING. MISDRILLED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOUBLE HOLE IN HOR FLANGE OF RT MLG SUPPORT FITTING BS 940 RBL 66 WL 208. REMOVED DAMAGED AREA AND REPAIRED PER EO 72 - [SDR UPS96205973](https://openairdocs.org/sdr/UPS96205973), Apr 11, 1996: BULLNOSE. CORRODED. WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 BULLNOSE I/B LUG CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IAW MM 27-81-0 AND OHM 57-51-01. All 157: https://openairdocs.org/deregistered/N933UP-2007-08-24/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 19900228013459I](https://openairdocs.org/incident/19900228013459I), Feb 28, 1990: Boeing 72725C (N933UP), Billings, MT. Slat warning light on climb. Returned. NR7 slat had not retracted. Had a defective actuator. ## Other aircraft with N933UP - [Registered now](https://openairdocs.org/aircraft/N933UP): Boeing 767-300F, S/N 70808 --- 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.