# N917UP: 1967 Boeing 727-30C, registration cancelled 2006-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2006 - Status when cancelled: Sale reported - Airframe: [Boeing 727-30C](https://openairdocs.org/model/boeing-727-30c) (registry code 1384009) - Serial number: 19310 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: January 15, 1979 - Last registry action: June 9, 2005 - Mode S code: ACB27C - 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/N917UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=917UP - Page: https://openairdocs.org/deregistered/N917UP-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 727-30C: https://openairdocs.org/model/boeing-727-30c.md ## Service difficulty reports (59, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS02238231](https://openairdocs.org/sdr/UPS02238231), May 14, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:AS-E BATTERIES IN THE COCKPIT EMERGENCY EXIT LIGHT ASSY ARE WEAK. UPON REPLACEMENT OF BATTERIES, THE BATTERY TRAY END TAB BROKE. REMOVED AND REP - [SDR UPS02237610](https://openairdocs.org/sdr/UPS02237610), Feb 12, 2002: SWITCH. OUT OF ADJUST. INSPECTION TYPE:N/A UPON LEVELING AT FLT LEVEL 280 AMBER MAIN CARGO DOOR LIGHT ILLUMINATED, FOLLOWED APPROPRIATE EMERGENCY PROCEDURES. DESCENDED TO AIRCRAFT ALT - [SDR UPS01237190](https://openairdocs.org/sdr/UPS01237190), Oct 26, 2001: SUPPORT. CRACKED. INSPECTION TYPE:IN RT WING INBOARD GROUND SPOILER ACTUATOR FITTING ASSY LT AND RT PANEL SUPPORT BRACKETS CRACKED. REMOVED AND REPLACED INBOARD AND OUTBOARD GROU - [SDR UPS01235327](https://openairdocs.org/sdr/UPS01235327), Mar 21, 2001: OXYGEN MASK. FAILED. D-SECOND OBSEVERS. O2 MASK INOP M-211583. R & R 02 MASK & CLEANED AUDIO JACK. CHECKS GOOD THIS CLEARS DFRL. - [SDR UPS00233393](https://openairdocs.org/sdr/UPS00233393), Jul 20, 2000: UNKNOWN. ODOR. INSPECTION TYPE:N/A, BRIEF ACRID SMELL DURING CLIMB. RAN ALL ENGS AND OPERATED PACKS. LOADED ELECTRICAL SYSTEM INCLUDING INTERIOR LIGHTING. COULD NOT FIND ANY A - [SDR UPS00233384](https://openairdocs.org/sdr/UPS00233384), Jun 17, 2000: STRINGER. CRACKED. INSPECTION TYPE:C, IN FORWARD LWR CARGO COMPARTMENT STA 670, STR 22R, THE STRINGER HAS A CORROSION CRACK. CUT OUT DAMAGED STRINGER SECTION AND INSTALLED REPAIR - [SDR UPS00233388](https://openairdocs.org/sdr/UPS00233388), Jun 12, 2000: FITTING. CORRODED. INSPECTION TYPE:C, EVIDENCE OF CORROSION IN PREVIOUS BLEND OUTS AT RIGHT SIDE BOTTLE PIN FITTING REAR LUG IN BUSHING BORE (FOUND AFTER BUSHING REMOVED). ACCOMPL - [SDR UPS00233383](https://openairdocs.org/sdr/UPS00233383), Jun 12, 2000: STRINGER. CRACKED. INSPECTION TYPE:C, STRINGER 16 RIGHT CRACKED AT BS 480 AND BS 500. INSTALLED REPAIR AT STR 16R, BS 480 & BS 500 IAW SRM 53-10-3 FIG 1. MATERIAL USED (P/N BAC149 - [SDR UPS00233387](https://openairdocs.org/sdr/UPS00233387), Jun 10, 2000: ANGLE. MISSING. INSPECTION TYPE:N/A, VIEW FROM LEFT WHEEL WELL INSIDE KEEL BEAM, THE CENTER CHORD ANGLE HAS TWO AREAS OF MATERIAL MISSING. INSTALLED NEW CHORD ANGLE IAW BOEING - [SDR UPS00233385](https://openairdocs.org/sdr/UPS00233385), Jun 10, 2000: PIN. CORRODED. INSPECTION TYPE:C, RIGHT WING FRONT SPAR WING-TO-BODY FITTING BOTTLE PIN CORRODED. RIGHT WING FRONT SPAR WING-TO-BODY FITTING BOTTLE PIN REPLACED IAW B727 MM 57 - [SDR UPS00233382](https://openairdocs.org/sdr/UPS00233382), Jun 10, 2000: SEAT TRACK. WORN. INSPECTION TYPE:C, SEAT TRACK WORN BETWEEN BS 500 AND BS 520 AT RBL 24.75. REPLACED SECTION OF SEAT TRACK FROM STA 500 TO STA 520 AT RBL 24.75 IAW SRM 53-10-5 F - [SDR UPS00233381](https://openairdocs.org/sdr/UPS00233381), Jun 10, 2000: SEAT TRACK. DAMAGED. INSPECTION TYPE:C, SEAT TRACK DAMAGED AT FRAME STA 500 AND BL RIGHT 0.5. REPLACED SEAT TRACK FROM BS 500 TO BS 550, RBL 0.5 IAW SRM 53-10-5 FIG 7. MATERIAL USED - [SDR UPS00233380](https://openairdocs.org/sdr/UPS00233380), Jun 10, 2000: SEAT TRACK. WORN. INSPECTION TYPE:C, SEAT TRACK WORN AT BS 1130 AND LBL 45.5. REPLACED SEAT TRACK FROM BS 1110 - 1130, LBL 45.5. MATERIAL USED (P/N BAC1520251) IAW B727 SRM 53-10 - [SDR UPS00233386](https://openairdocs.org/sdr/UPS00233386), Jun 7, 2000: SKIN. CORRODED. INSPECTION TYPE:C AT FS 680, STR 19L HAS BULGE AREA ON SKIN. PERFORMED LFEC, SKIN LOSS 30 PERCENT. INSTALLED REPAIR DOUBLER IAW SRM 53-3 0-3 & DRAWING 69-61590 - [SDR UPS99228689](https://openairdocs.org/sdr/UPS99228689), Jan 30, 1999: STRINGER. CRACKED. INSPECTION TYPE:C RT WING STA 629 STR 13 FWD LUG CRACKED. REPAIR CARRIED OUT IAW UPS EO B727-5710-0314. - [SDR UPS99228622](https://openairdocs.org/sdr/UPS99228622), Jan 29, 1999: FITTING. CORRODED. INSPECTION TYPE:C SEAT TRACK ATTACH FITTING CORRODED AT BS 740 RBL 45. FITTING AT BS 740 RBL 45 REPLACED PER DWR NR 65C13724. - [SDR UPS99228621](https://openairdocs.org/sdr/UPS99228621), Jan 29, 1999: CAP ASSY. CRACKED. INSPECTION TYPE:C APU COMBUSTION UNIT HAS CRACK ON CAP ASSY. COMBUSTION UNIT LINER ASSY REPLACED IAW MM CHP 49-30-22. - [SDR UPS99228686](https://openairdocs.org/sdr/UPS99228686), Jan 27, 1999: SKIN. DAMAGED. INSPECTION TYPE:C, RT BS 740 SKIN (STRINGERS 17 TO 22 INCLUSIVE AREA) HOLES ARE 2ND OVERSIZE. REPAIR CARRIED OUT IAW EO 99-03-001, UPS ENGINEERING FILE NR 5310- - [SDR UPS99228808](https://openairdocs.org/sdr/UPS99228808), Jan 26, 1999: SKIN. CORRODED. INSPECTION TYPE-C, ON CORROSION REMOVAL, PER NRC 811973 & 812094 & EO B727-5330-0509Q, FROM LAP STR 4L AND STR 4R, BS 1120, CORROSION AND DISBOND FOUND ON CROWN - [SDR UPS99228636](https://openairdocs.org/sdr/UPS99228636), Jan 26, 1999: SEAT TRACK. CORRODED. INSPECTION TYPE-C, TO FACILITATE REPAIR OF FRAME 848.95 SEAT TRACK BETWEEN BS 760-870 L BL 62.5 HAD TO BE REMOVED ON REMOVAL OF THIS SEAT TRACK SECTION IT WAS F - [SDR UPS99228809](https://openairdocs.org/sdr/UPS99228809), Jan 25, 1999: SPACER. CRACKED. INSPECTION TYPE-C, NR 1 FLAP TRACK FWD ATTACH FITTING OUTBD AFT SPACER CRACKED. BOLT REMOVED AND NEW SPACER, BOLT, WASHER AND LOCKNUT INSTALLED IAW SRM 51-30-2 - [SDR UPS99228688](https://openairdocs.org/sdr/UPS99228688), Jan 25, 1999: MOUNT. CORRODED. INSPECTION TYPE:C ENGINE NR 1 PITTING CORROSION ON BIG MOUNT HOLES, SMALL HOLES OK. CORROSION ON MOUNT HOLES REMOVED IAW SMRO EO 99-03-002 REV 1 UPS ENGINEERING - [SDR UPS99228687](https://openairdocs.org/sdr/UPS99228687), Jan 25, 1999: MOUNT. CORRODED. INSPECTION TYPE:C ENGINE NR 3 PITTING CORROSION ON MOUNT HOLES, FWD O/B, AFT I/B. CORROSION IN MOUNT HOLES REMOVED IAW SMRO EO 99-03-003 UPS ENGINEERING FILE NR - [SDR UPS99228654](https://openairdocs.org/sdr/UPS99228654), Jan 25, 1999: SKIN. CORRODED. INSPECTION TYPE-C, CORROSION ON UPPER SKIN OF RT HORIZONTAL STABILIZER STAB STA 68. REMOVED CORROSION IAW SRM 51-10-6. REPAIRED AREA IAW SMRO EO 99-03-008 UPS E - [SDR UPS99228637](https://openairdocs.org/sdr/UPS99228637), Jan 25, 1999: HINGE. CRACKED. INSPECTION TYPE-C, CRACK (5MM) FOUND IN MID GALLEY DOOR HINGE FWD LOWER CUTOUT. REPAIR CARRIED OUT IAW EO B727-5330-1063 APPENDIX B. - [SDR UPS99228624](https://openairdocs.org/sdr/UPS99228624), Jan 25, 1999: BRACKET. CRACKED. INSPECTION TYPE:C ENGINE NR 1 THRUST REV OUTER FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 78-30-00. - [SDR UPS99228623](https://openairdocs.org/sdr/UPS99228623), Jan 25, 1999: BRACKET. CRACKED. INSPECTION TYPE:C ENGINE NR 3 THRUST REV OUTER FAIRING MID AND AFT SUPPORT BRACKETS CRACKED. REPLACED BRACKETS IAW MM 78-30-00. - [SDR UPS99228655](https://openairdocs.org/sdr/UPS99228655), Jan 23, 1999: FRAME. CRACKED. INSPECTION TYPE-C, CRACK AT FRAME STA 848.95 LT EMINATING FROM 4TH FASTENER HOLE ABOVE FLOOR. REPAIR CARRIED OUT TO FRAME AT STA 848.95 LT IAW SMRO EO 99-03-010 - [SDR UPS99228740](https://openairdocs.org/sdr/UPS99228740), Jan 22, 1999: SKIN. CORRODED. INSPECTION TYPE-C, CORROSION BETWEEN SKIN AND STIFFENER BS 1323 TO 1342, STRINGER 9L AND STRINGER 8L. REPAIRED IAW SMRO ENGINEERING ORDER 99-03-009, REF UPS ENG - [SDR UPS99228639](https://openairdocs.org/sdr/UPS99228639), Jan 22, 1999: RIB. CRACKED. INSPECTION TYPE-C, NR 6 L/E SLAT CRACK IN RIB 6 O/B OF FLAP ACTUATOR. AREA REPAIRED IAW SRM 57-50-03 FIG 9. - [SDR UPS99228638](https://openairdocs.org/sdr/UPS99228638), Jan 22, 1999: WEB. CRACKED. INSPECTION TYPE-C, DURING INSPECTION OF AFT CARGO DOOR STOP FITTINGS SUSPECT CRACK FOUND IN WEB, FWD OF AFT DOOR HINGE INSIDE DOOR WEB. REPLACED IAW SRM 51-30-0 - [SDR UPS99228625](https://openairdocs.org/sdr/UPS99228625), Jan 22, 1999: SKIN. CRACKED. INSPECTION TYPE:C NR 3 LE KRUEGER FLAP HAS CRACK ON ANTI-ICE SKIN. CRACK STOP DRILLED IAW SRM 51-10-1. - [SDR UPS99228429](https://openairdocs.org/sdr/UPS99228429), Jan 11, 1999: FRAME. CRACKED. INSPECTION TYPE-C, CRACK AT BS 930 LT FRAME. CRACK REPAIRED IAW DRAWING 65-80107 AND EO B727-5310-2611. - [SDR UPS99228431](https://openairdocs.org/sdr/UPS99228431), Jan 8, 1999: WEB. CRACKED. INSPECTION TYPE-C, LT WING NR 4 LE SLAT AND O/B ACTUATOR WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIRED IAW SRM 57-50-3. - [SDR UPS99228640](https://openairdocs.org/sdr/UPS99228640), Jan 7, 1999: BULKHEAD FITTING. CRACKED. INSPECTION TYPE-C, BS 740 FITTING CRACKED RIGHT HAND SIDE BS 740 RT BULKHEAD FORGING. REPLACED PER EO B727-5310-7477-D. - [SDR UPS99228436](https://openairdocs.org/sdr/UPS99228436), Jan 7, 1999: FITTING. CRACKED. INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 LT FITTING AT FWD OUTBOARD FLANGE ABOVE STRINGER 9. REPAIR CARRIED OUT IAW APPENDIX C OF B727-53 - [SDR UPS99228435](https://openairdocs.org/sdr/UPS99228435), Jan 7, 1999: FITTING. CRACKED. INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 RT FITTING AT AFT O/B FLANGE ABOVE STRINGER 9. REPAIR CARRIED OUT IAW B727-5310-3057 AND DRAWING - [SDR UPS99228434](https://openairdocs.org/sdr/UPS99228434), Jan 6, 1999: WEB. CRACKED. INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE SUSPECT CRACK ON WEB AT BS 1376 RT APPROX. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555. - [SDR UPS99228433](https://openairdocs.org/sdr/UPS99228433), Jan 6, 1999: WEB. CRACKED. INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE SUSPECT CRACK ON WEB AT BS 1376 LT APPROX. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555. - [SDR UPS99228432](https://openairdocs.org/sdr/UPS99228432), Jan 5, 1999: SKIN. DELAMINATED. INSPECTION TYPE-C, NR 9 SPOILER PANEL LOWER SKIN DELAMINATED. REPAIRED IAW SRM 57-50-6 FIG 5. - [SDR UPS97225364](https://openairdocs.org/sdr/UPS97225364), Dec 26, 1997: LIGHT. LOOSE. INSPECTION TYPE-N/A, UPON LANDING EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR FLICKERED NUMEROUS TIMES. FOUND EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY, O - [SDR UPS97223766](https://openairdocs.org/sdr/UPS97223766), Jul 3, 1997: SKIN. CRACKED. INSPECTION TYPE:C, RT WING L/E SKIN CRACKED ABOVE REFUELING PANEL SLAT STN 128 APROX. REPAIR CARRIED OUT I.A.W. SRM 57-30-4 FIG 4. - [SDR UPS97223773](https://openairdocs.org/sdr/UPS97223773), Jun 27, 1997: SKIN. DELAMINATED. INSPECTION TYPE:C, NR 7 SPOILER PANEL LWR SKIN IS DELAMINATED AT I/B AND IN AREA OF SMALL DOUBLER. NR 7 SPOILER REPAIRED I.A.W. EO C-5100-7322. - [SDR UPS97223771](https://openairdocs.org/sdr/UPS97223771), Jun 27, 1997: SKIN. DELAMINATED. INSPECTION TYPE:C, LT O/B MIDFLAP T/E IS DELAMINATED IN 3 AREAS ON UPPER AFT SKIN WEDGE. 3 AREAS OF THE LT O/B MIDFLAP T/E WERE REPAIRED I.A.W. EO C-5100-7 322. - [SDR UPS97223769](https://openairdocs.org/sdr/UPS97223769), Jun 27, 1997: WEB. CRACKED. INSPECTION TYPE:C, CRACK AT FWD WALL OF LT WHEELWELL AT BS 870 LBL 56 AT RIVET. REPAIRED I.A.W. SRM 53-10-9 FIG 4. - [SDR UPS97223768](https://openairdocs.org/sdr/UPS97223768), Jun 27, 1997: STRINGER. DAMAGED. INSPECTION TYPE:C TO AID IN REMOVAL OF STR 8 R END FITTING AT BS 1183. CUT STRINGER BETWEEN BS 1148 AND 1166. STRINGER REPAIRED I.A.W. SRM 53-10-3 FIG 3. - [SDR UPS97223794](https://openairdocs.org/sdr/UPS97223794), Jun 26, 1997: SEAT TRACK. CORRODED. INSPECTION TYPE:C, EVIDENCE OF CORROSION BETWEEN TRACK AND HORIZONTAL MEMBER BS 680 RBL 14. CORRODED BEYOND LIMITS I.A.W. SRM 53-10-1. TRACK REPAIRED IAW SRM 53 - [SDR UPS97223779](https://openairdocs.org/sdr/UPS97223779), Jun 26, 1997: RAMP SKIN. WORN. INSPECTION TYPE:C, NR 3 ENG THRUST REV LOWER DOOR RAMP SKIN WORN DUE TO CHAFFING OF SEAL REPAIRED I.A.W. EFIS AND RE ENGINE SUPP SRM 54-10-03 FIG 203. - [SDR UPS97223776](https://openairdocs.org/sdr/UPS97223776), Jun 26, 1997: RAMP SKIN. WORN. INSPECTION TYPE:C, NR 1 ENG T.REV LOWER DOOR INNER RAMP SKIN WORN DUE TO CHAFFING OF SEAL. REPAIR CARRIED OUT I.A.W. EFIS AND RE ENGINE SUPPLEMENT SRM 54-10-0 3 - [SDR UPS97223775](https://openairdocs.org/sdr/UPS97223775), Jun 26, 1997: SKIN. DELAMINATED. INSPECTION TYPE:C, NR 5 SPOILER PANEL HAS TWO SMALL AREAS OF DELAMINATION ON LWR SKIN AT O/B FWD END AND I/B MIDLE AT EDGE. NR 5 SPOILER PANEL REPAIRED I.A.W. E All 59: https://openairdocs.org/deregistered/N917UP-2006-08-23/reports.md ## Other aircraft with N917UP - [Registered now](https://openairdocs.org/aircraft/N917UP): Boeing 767-300F, S/N 68363, built 2026 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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