# N905UP: 1966 Boeing 727-51C, registration cancelled 2007-05-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 10, 2007 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-51C](https://openairdocs.org/model/boeing-727-51c) (registry code 1384015) - 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: 18947 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 12, 1966 - Certificate issued: May 11, 1992 - Last registry action: April 19, 2005 - Mode S code: AC838F - 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/N905UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=905UP - Page: https://openairdocs.org/deregistered/N905UP-2007-05-10 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 727-51C: https://openairdocs.org/model/boeing-727-51c.md ## Service difficulty reports (111, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS03241647](https://openairdocs.org/sdr/UPS03241647), Dec 9, 2003: WARNING LIGHT. ILLUMINATED. NR 3 ENG FUEL FILTER WARNING LIGHT ILLUMINATED. - [SDR UPS02239943](https://openairdocs.org/sdr/UPS02239943), Nov 25, 2002: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C SEVERAL CRACKS ON NLG WHEEL WELL PRESSURE WEB RHS FROM BS 260 DOWN 1 1" FROM CEILING AND 1" FWD OF THE AFT PRESSURE PANEL TP BS 279 6" BE LOW - [SDR UPS02239946](https://openairdocs.org/sdr/UPS02239946), Nov 21, 2002: PRESSURE PANEL. CRACKED. INSPECTION TYPE: C, NLG WHEEL WELL PRESSURE PANEL CRACKED AT BS 268, 3 INCHES DOWN FROM W/W CEILING. DAMAGED AREA CUTOUT IAW SRM 51-40-2 FIG 1 HFEC CONFIRMS A D - [SDR UPS02239949](https://openairdocs.org/sdr/UPS02239949), Nov 19, 2002: BOLT. CRACKED. INSPECTION TYPE: C, DURING REMOVAL OF LT HAND TRUNNION LINK, THE LT MAIN GEAR AFT TRUNNION BOLT AND TRUNNION HOUSING FOUND SHEARED. ON REMOVAL OF LT MLG, AFT BE - [SDR UPS02239945](https://openairdocs.org/sdr/UPS02239945), Nov 19, 2002: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C SUSPECT CRACK ON NLG CEILING AT BS 273 LBL14. HFEC CONFIRMS CRACK, DAMAGED ARE CUTOUT IAW SRM 51-40-02 FIG, HFEC CONFIRMS NDF. REPAIR CARRIED - [SDR UPS02239944](https://openairdocs.org/sdr/UPS02239944), Nov 19, 2002: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C CRACK ON NLG WHEEL WELL PRESSURE WEB @ BS 243.6 LHS 4" AFT FROM FWD PRESSURE PANEL. DAMAGED AREA CUT OUT IAW SRM 51-40-02 FIG1, HFEC AROUND CU - [SDR UPS02239940](https://openairdocs.org/sdr/UPS02239940), Nov 18, 2002: FITTING. CRACKED. INSPECTION TYPE:C SUSPECT CRACK ON L/H BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B - [SDR UPS02239937](https://openairdocs.org/sdr/UPS02239937), Nov 18, 2002: FITTING. CRACKED. INSPECTION TYPE:C SUSPECT CRACK ON RH BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B - [SDR UPS02239938](https://openairdocs.org/sdr/UPS02239938), Nov 16, 2002: PIN. CORRODED. INSPECTION TYPE:C PITTING FOUND ON RT STAB INNER PINS. RT STAB INNER PIN REPLACED IAW MM 55-10-01. - [SDR UPS02239950](https://openairdocs.org/sdr/UPS02239950), Nov 15, 2002: SPAR. CRACKED. INSPECTION TYPE: C, DURING LFEC INSPECTION OR RT INBOARD MID FLAP REAR SPAR UPPER CHORD, A CRACK WAS FOUND AROUND A FASTENER HOLE. REPAIRED PER EO.B727-5750-358 - [SDR UPS02239948](https://openairdocs.org/sdr/UPS02239948), Nov 15, 2002: BEAM. CRACKED. INSPECTION TYPE: C, DURING INSPECTION OF VERTICAL BEAM 17.8 RT, A CRACK WAS FOUND ON THE BEAM FLANGE. STOP CUT-OUT AT WL 273, BS 1183 REPAIR PARTS DRILLED OFF I - [SDR UPS02239942](https://openairdocs.org/sdr/UPS02239942), Nov 15, 2002: INTERCOSTAL. CRACKED. INSPECTION TYPE:C HORIZONTAL INTERCOSTAL CRACKED ON VERTICAL BEAM 17.8 L/H AT WL 283 1 183 BULKHEAD NEW INTERCOSTAL FABRICATED & INSTALLED PER BOEING DRAWING 65 - [SDR UPS02239941](https://openairdocs.org/sdr/UPS02239941), Nov 14, 2002: FLOORBEAM. CRACKED. INSPECTION TYPE:C BEAM TIE CRACKED ON FLOORBEAM LWR FLANGE BS 328 RBL 40. REPAIR PLATE FABRICATED AND FITTED AS PER ARM 53-10-8. - [SDR UPS02239947](https://openairdocs.org/sdr/UPS02239947), Nov 13, 2002: FITTING. CRACKED. INSPECTION TYPE: C&SI, WHILE CARRY OUT HFEC INSPECTION ON LT BS 950 FITTING. CRACK FOUND IN ROW 1 UP PER FASTENER HOLE, COMMON TO STR 9. DISCREPANT HOLE REPAIRE - [SDR UPS02238710](https://openairdocs.org/sdr/UPS02238710), Jun 28, 2002: RELAY. FAILED. INSPECTION TYPE:N/A EMERGENCY LIGHTS ABOVE COCKPIT DOOR ILLUMINATED IN FLIGHT WITH ARM SWITCH IN THE ARMED POSITION. REMOVED R70 RELAY. OPS CHECKS GOOD. - [SDR UPS01236733](https://openairdocs.org/sdr/UPS01236733), Aug 30, 2001: STIFFENER. CRACKED. INSPECTION TYPE:N/A RT MLG ACT BEAM SUPPORT PANEL. FWD STIFFENER CRACKED AT INBD HINGE. REPAIRED CRACKED STIFFENER RT MLG ACT BEAM SUPPORT PANEL PER B727 SRM 51 - [SDR UPS01236532](https://openairdocs.org/sdr/UPS01236532), Aug 5, 2001: SLIDE. INOPERATIVE. INSPECTION TYPE:IN MAIN CABIN SLIDE INOP REF DEF M220206 FWD ENTRY SLIDE DEPLOYED. REPLACED SLIDE AND LATCH ASSY REF 25-60-14. - [SDR UPS01236026](https://openairdocs.org/sdr/UPS01236026), May 31, 2001: PANEL. CRACKED. INSPECTION TYPE:C, 1 INCH CRACK ON PANEL, UPPER SURFACE OF WING, JUST FWD OF I/B AILERON ON RIGHT WING, I/B EDGE OF PANEL. REPAIRED PER SRM 51-40-2. - [SDR UPS01236033](https://openairdocs.org/sdr/UPS01236033), May 30, 2001: SKIN. CRACKED. INSPECTION TYPE:C, CRACK FOUND IN TRAILING EDGE SKIN ADJACENT NR 3 SPOILER PANEL HINGE INBOARD HINGE. CRACK REPAIRED IAW SRM. - [SDR UPS01235942](https://openairdocs.org/sdr/UPS01235942), May 21, 2001: LIGHT. INOPERATIVE. INSPECTION TYPE:IN EMERGENCY LIGHTS UNARMED LIGHT INOP WHEN UNARMED AND PRESS TO TEST. RELAMPED AND FUNCTIONALLY CK GOOD AS PER 33-50. - [SDR UPS00234515](https://openairdocs.org/sdr/UPS00234515), Nov 26, 2000: SKIN. CRACKED. INSPECTION TYPE:C FOUND R/H OUTBRD FOREFLAP WITH A 3/8 INCH CRACK AT HINGE CUTOUT. REPLACED R/H OUTBRD FOREFLAP IAW M/M 27-51-11. OK PER SAME - [SDR UPS98227681](https://openairdocs.org/sdr/UPS98227681), Sep 15, 1998: DOUBLER. CRACKED. INSPECTION TYPE-N/A, RIGHT WING AFT SPAR LOWER EDGE CORRIGATED DOUBLER CRACKED APROX 2 INCHES AT APROX WS 340 WBL 220. STOP DRILLED CRACK PER SRM 51-10-1 PG 6B. - [SDR UPS98227517](https://openairdocs.org/sdr/UPS98227517), Aug 14, 1998: RIB. CRACKED. INSPECTION TYPE-D, ON REMOVAL OF NR 4 SLAT ACTUATOR EYE END BOLT FROM SLAT BOTH RIBS EITHER SIDE OF MOUNT POINT FOUND CRACKED. REPLACED RIBS IAW SRM AND DRAWING - [SDR UPS98227488](https://openairdocs.org/sdr/UPS98227488), Aug 13, 1998: BOTTLE PIN. CORRODED. INSPECTION TYPE:D LT BS 750 BOTTLE PIN FOUND WITH LIGHT PITTING CORROSION. PIN REPLACED IAW MM 57-41-00. - [SDR UPS98227574](https://openairdocs.org/sdr/UPS98227574), Aug 12, 1998: STRINGER. CORRODED. INSPECTION TYPE:D STRINGER ON TOP OF NOSE WHEEEL WELL AT BL 0, BS 260 TO 277 IS CORRODED. STRINGER SECTION REPAIRED IAW SRM 53-10-3. - [SDR UPS98227572](https://openairdocs.org/sdr/UPS98227572), Aug 12, 1998: STRINGER. CRACKED. INSPECTION TYPE:D SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2. - [SDR UPS98227566](https://openairdocs.org/sdr/UPS98227566), Aug 12, 1998: STRINGER. CRACKED. INSPECTION TYPE-D, STRINGER 23L AT STATION 400 CRACKED AT FASTENER HOLE. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1. - [SDR UPS98227565](https://openairdocs.org/sdr/UPS98227565), Aug 12, 1998: STRINGER. CRACKED. INSPECTION TYPE-D, S21L HAS CRACK AT FASTENER HOLE AT STATION 380. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1. - [SDR UPS98227564](https://openairdocs.org/sdr/UPS98227564), Aug 12, 1998: RIB. CRACKED. INSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 13 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS B727-5710-0314. - [SDR UPS98227561](https://openairdocs.org/sdr/UPS98227561), Aug 12, 1998: RIB. CRACKED. INSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 10 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS EO B727-5710-0314 FIG 13. - [SDR UPS98227551](https://openairdocs.org/sdr/UPS98227551), Aug 12, 1998: STRINGER. CRACKED. INSPECTION TYPE-D, CRACK IN FASTENER HOLE AND FASTENER MISSING ON S21R AT BS 400. REPAIRED CRACK IAW SRM 51-10-3, FIG 2. - [SDR UPS98227550](https://openairdocs.org/sdr/UPS98227550), Aug 12, 1998: STRINGER. CRACKED. INSPECTION TYPE-D, SUSPECT CRACK ON S22R FASTENER HOLE ST STA 380. REPAIRED CRACK IAW SRM 51-10-3 FIG 2. - [SDR UPS98227549](https://openairdocs.org/sdr/UPS98227549), Aug 12, 1998: STRINGER. CRACKED. INSPECTION TYPE-D, CRACK AT FASTENER HOLE OF STRINGER 21R AT STATION 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1, DETAIL 2. - [SDR UPS98227548](https://openairdocs.org/sdr/UPS98227548), Aug 12, 1998: STRINGER. BROKEN. INSPECTION TYPE-D, STRINGER 23R BROKEN AT STA 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1 DETAIL 2. - [SDR UPS98227496](https://openairdocs.org/sdr/UPS98227496), Aug 12, 1998: STRINGER. CRACKED. INSPECTION TYPE:D, SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2. - [SDR UPS98227573](https://openairdocs.org/sdr/UPS98227573), Aug 11, 1998: FRAME. CRACKED. INSPECTION TYPE:D CRACK ON UPPER FLANGE OF FRAME AT BS 420, BL 0. REPAIR CARRIED OUT ON UPPER FLANGE IAW SRM 51-40-3, FIG 1. - [SDR UPS98227518](https://openairdocs.org/sdr/UPS98227518), Aug 10, 1998: FRAME. CRACKED. INSPECTION TYPE-D, SLIDING FAIRING 2ND AFT FRAME HAS A CRACK AT THE UPPER SLIDING TRACK ATTACH POINT. CRACK STOP DRILLED PER SRM 51-10-1, REPAIRED FRAME IAW SRM - [SDR UPS98227571](https://openairdocs.org/sdr/UPS98227571), Aug 8, 1998: STRAP. CRACKED. INSPECTION TYPE:D ON ACCOMPLISHMENT OF EDDY CURRENT INSPECTION OF RT E-F WINDOW POST PER EO B727-5310-0012, CRACKS FOUND ON 3 HOLES COMMON TO REPAIR STRAP. REPA - [SDR UPS98227560](https://openairdocs.org/sdr/UPS98227560), Aug 7, 1998: TRACK. CRACKED. INSPECTION TYPE-D, CARGO TRACK SECTION BS 1010 RT SIDE HAS SIZEABLE CRACK. RT FWD TRACK REPLACED IAW SRM 51-30-2. - [SDR UPS98227529](https://openairdocs.org/sdr/UPS98227529), Aug 7, 1998: WEB. CRACKED. INSPECTION TYPE-D, CRACK ON VERTICAL WEB ABOVE KEEL BEAM RBL BS 885 APPROX. VERTICAL WEB ABOVE KEEL BEAM REPAIRED IAW SRM 51-40-02. - [SDR UPS98227528](https://openairdocs.org/sdr/UPS98227528), Aug 7, 1998: CLIP. CRACKED. INSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT RBL 25. REPLACED SHEAR TIE CLIP IAW DRW 64-08333. - [SDR UPS98227527](https://openairdocs.org/sdr/UPS98227527), Aug 7, 1998: CLIP. CRACKED. INSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT LBL 25. REPLACED SHEAR TIE CLIP IAW DRAWING 64-08333. - [SDR UPS98227519](https://openairdocs.org/sdr/UPS98227519), Aug 7, 1998: SKIN. CORRODED. INSPECTION TYPE-D, SUSPECT CORROSION BETWEEN SKIN AND CUSP ANGLE BS 1180 STR 17R. CORRODED SKIN AT BS 1180 STR 17R REPAIRED PER SRS EO 98-24-006 REF UPS ENGINEE - [SDR UPS98227499](https://openairdocs.org/sdr/UPS98227499), Aug 7, 1998: FITTING. CORRODED. INSPECTION TYPE:D, 9G BARRIER NET ATTACH FITTING ON FLOOR LBL 20 BETWEEN BS 360-380 HAS SEVERE CORROSION. 9G FITTING AT LBL 20 REPLACED IAW SRM 51-30-02. - [SDR UPS98227495](https://openairdocs.org/sdr/UPS98227495), Aug 7, 1998: WEB. CORRODED. INSPECTION TYPE:D, COROSION ON WEB RBL 10 BS 830 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2. - [SDR UPS98227533](https://openairdocs.org/sdr/UPS98227533), Aug 6, 1998: SPINDLE. CORROSION. INSPECTION TYPE-D, SURFACE CORROSION IN BORE OF SPINDLE OF NR 3 FLAP TRACK CARRIAGE. FLAP TRACK CARRIAGE REPLACED REF OHM 57-58-11. - [SDR UPS98227492](https://openairdocs.org/sdr/UPS98227492), Aug 6, 1998: WEB. CRACKED. INSPECTION TYPE:D, ENGINE NR 1 THRUST REV AFT VERTICAL WEB SUSPECT CRACK AT 12 O'CLOCK POSITION AT HYD PIPE BRACKET ATTACH. REPAIR CARRIED OUT IAW SRM 51-40-2. - [SDR UPS98227563](https://openairdocs.org/sdr/UPS98227563), Aug 5, 1998: ANGLE. CORRODED. INSPECTION TYPE-D, CHORD ANGLE AT BS 740 LT (P/N 65-15940-24) HAS CORROSION ON O/B SECTION. CHORD REPAIRED IAW DRAWING 65C13724 AND SRS ENGINEERING ORDER 98-24- - [SDR UPS98227544](https://openairdocs.org/sdr/UPS98227544), Aug 5, 1998: BOLT. CORRODED. INSPECTION TYPE-D, NR 5 FLAP TRACK ATTACH BOLT CORRODED. BOLT CHANGED IAW MM 27-51-31. - [SDR UPS98227576](https://openairdocs.org/sdr/UPS98227576), Aug 4, 1998: PANEL. CORRODED. INSPECTION TYPE:D LT WING TANK FROMT SPAR ACCESS PANEL NR 1 CORRODED. PANEL REPLACED IAW MM 28-11-21. All 111: https://openairdocs.org/deregistered/N905UP-2007-05-10/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 19950906044029I](https://openairdocs.org/incident/19950906044029I), Sep 6, 1995: Boeing 72751C (N905UP), Portland, OR. Narrative: takeoff rejected when crew was unable to get takeoff thrust on #2 engine. Max epr attained was 1.6. Other #2 engine gauges also read lower than #1… ## Other aircraft with N905UP - [Registered now](https://openairdocs.org/aircraft/N905UP): Cessna 750, S/N 750-0133, built 2000 --- 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.