# N909UP: 1966 Boeing 727-27C, registration cancelled 2006-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2006 - Status when cancelled: Sale reported - Airframe: [Boeing 727-27C](https://openairdocs.org/model/boeing-727-27c) (registry code 138400J) - 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: 19115 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 29, 1966 - Last registry action: February 15, 2005 - Mode S code: AC926B - 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/N909UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=909UP - Page: https://openairdocs.org/deregistered/N909UP-2006-08-23 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 727-27C: https://openairdocs.org/model/boeing-727-27c.md ## Service difficulty reports (126, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS03240006](https://openairdocs.org/sdr/UPS03240006), Jan 9, 2003: BATTERY. DISCHARGED. INSPECTION TYPE: PFLT. EMERGENCY EXIT LIGHT ASSEMBLIES AT CABIN ENTRY AND CREW ENTRY DOOR BATTERIES DEAD. RECHARGED BATTERIES, OPS CHECKS OKAY. - [SDR UPS02237399](https://openairdocs.org/sdr/UPS02237399), Jan 7, 2002: LIGHT. INOPERATIVE. INSPECTION TYPE:PFLT L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-01, OPS CHECK NORMAL. - [SDR UPS01237194](https://openairdocs.org/sdr/UPS01237194), Oct 29, 2001: BATTERY. DISCHARGED. INSPECTION TYPE:IN CREW ENTRANCE DOOR EMERGENCY EXIT LIGHT WENT DIM SHORTLY AFTER TESTING LIGHTS. REPLACED BATTERIES WITH CHARGED UNITS. OPS CHECKED GOOD IAW MM - [SDR UPS01237094](https://openairdocs.org/sdr/UPS01237094), Oct 18, 2001: BATTERY. DISCHARGED. INSPECTION TYPE:N/A, OVERHEAD LIGHTS ABOVE CREW ENTRY DOOR INOP. REPLACED BATTERIES IAW 33-50-00. OPS CHECKS GOOD. - [SDR UPS01236437](https://openairdocs.org/sdr/UPS01236437), Jul 31, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C CRACK IN MLG WEB BS 938 O/B AFT CORNER ADJACENT TO STR 18A LWR FASTENER ROW IN RT MLG WW CRACK DRESSED OUT AND NDT CONFIRMED REMOVAL SRM51-10- - [SDR UPS01236476](https://openairdocs.org/sdr/UPS01236476), Jul 22, 2001: FITTING. CRACKED. INSPECTION TYPE:C TAIL SKID LT LWR TENSION TIE REAR TERMINAL FITTING CRACKED. LT LWR TENSION TIE AFT FITTING REMOVED AND NEW ONE INSTALLED IAW DRAWING 65-25992. - [SDR UPS01236438](https://openairdocs.org/sdr/UPS01236438), Jul 20, 2001: FRAME. DAMAGED. INSPECTION TYPE:C FRAME DAMAGED AT BS 320 STR22R STR27R (HOLES DAMAGED) FRAME REPLACED IAW SRM 51-30-02 AND DRWG 65-18420 - [SDR UPS01236439](https://openairdocs.org/sdr/UPS01236439), Jul 18, 2001: BRACKET. CRACKED. INSPECTION TYPE:C CRACK ON EDGE OF FLOOR PANEL SUPPORT BRACKET AT STA 755 LBL 50. NEW BRACKET FITTED IAW SRM 51-30-02. - [SDR UPS01236440](https://openairdocs.org/sdr/UPS01236440), Jul 17, 2001: SKIN. CORRODED. INSPECTION TYPE:C CORROSION ON LAP S24R BS 295 CPCP NEAR REPAIR REQUIRED SKIN REPLACEMENT WHICH ENCOMPASSED THIS DAMAGE , SKIN REPLACED. - [SDR UPS01236436](https://openairdocs.org/sdr/UPS01236436), Jul 17, 2001: FITTING. CRACKED. INSPECTION TYPE:C SUSPECT CRACK AT TAIL SKID COMPT, RT UPPER TENSION TIE END FITTING CRACK CONFIRMED BY NDT, FITTING REPLACED IAW DRAWING. - [SDR UPS01236460](https://openairdocs.org/sdr/UPS01236460), Jul 16, 2001: HINGE. CRACKED. INSPECTION TYPE:C MAIN CARGO DOOR FWD AND AFT HINGES CRACKED. ON INVESTIGATION HINGES FOUND CORRODED BEYOND LIMITS, HINGES REPLACED IAW OHM 20-50-01 - [SDR UPS01236314](https://openairdocs.org/sdr/UPS01236314), Jul 9, 2001: STRINGER. CRACKED. INSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3 - [SDR UPS01236302](https://openairdocs.org/sdr/UPS01236302), Jul 6, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C, CRACKS FOUND AT 2 FASTENER HOLES AT PRESSURE DECK UPPER SURFACE AT BS 880 - 890 RBL 23. REPAIR CARRIED OUT IAW DRAWING 65-89360 & SRM 53-10-9 - [SDR UPS01236287](https://openairdocs.org/sdr/UPS01236287), Jul 5, 2001: FRAME. CRACKED. INSPECTION TYPE: C, LT MLG WING DOOR (OUTER HALF) O/B DOOR FRAME AFT CORNER CRACKED. REPAIR CARRIED OUT IAW SRM 51-10-2 & SRM 51-40-3 - [SDR UPS01236286](https://openairdocs.org/sdr/UPS01236286), Jul 4, 2001: STRAP. CORRODED. INSPECTION TYPE:C, DURING RECTIFICATION OF CORROSION BETWEEN TEAR STRAP SKIN AT BS 680 S6L, INDICATIONS OF SUSPECT CORROSION ALSO FOUND AT BS 660 S4L TO S3L AT - [SDR UPS01236301](https://openairdocs.org/sdr/UPS01236301), Jul 3, 2001: INTERCOSTAL. CRACKED. INSPECTION TYPE:C CRACK ON INTERCOSTAL AT STR 17R AT BS 830 INTERCOSTAL REPLACED IAW SRM 51-30-1 - [SDR UPS01236312](https://openairdocs.org/sdr/UPS01236312), Jul 2, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C, DURING NDT INSP OF RT MLG WHEEL WELL PRESSURE WEB CRACK WAS FOUND ON WEB AT BS 940 RBL 33 APPROX. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-30- - [SDR UPS01236309](https://openairdocs.org/sdr/UPS01236309), Jul 2, 2001: RIB. CRACKED. INSPECTION TYPE:C SUSPECT CRACK IN #6 SLAT RIB, O/B OF SLAT ACTUATOR DAMAGED RIB REPAIRED IAW SRM 57-30-3 - [SDR UPS01236304](https://openairdocs.org/sdr/UPS01236304), Jul 2, 2001: WEB. CORRODED. INSPECTION TYPE:C, CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK AT BBL 15L. REPAIR CARRIED OUT IAW SRM 51-40-2. - [SDR UPS01236300](https://openairdocs.org/sdr/UPS01236300), Jul 2, 2001: SKIN. CORRODED. INSPECTION TYPE:C CORROSION OF RH STAB SKIN UPPER SURFACE & RIVET PULLED @ STAB STA 80 APPROX FWD OF REAR SPAR ***CPCP*** REPAIR CARRIED OUT IAW SRM 55-10-3 - [SDR UPS01236298](https://openairdocs.org/sdr/UPS01236298), Jul 2, 2001: WEB. CORRODED. INSPECTION TYPE:C CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK OF BBL 12R ***CPCP*** WEB REPLACED IAW SRM 51-10-01 - [SDR UPS01236289](https://openairdocs.org/sdr/UPS01236289), Jul 2, 2001: STRAP. CORRODED. INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 580 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-10-6, SRM 53-30-3. - [SDR UPS01236313](https://openairdocs.org/sdr/UPS01236313), Jul 1, 2001: SUPPORT BRACKET. CRACKED. INSPECTION TYPE:C BS 910 FRAME FWD FLANGE LWR CORNER SUPPORT BRACKET CRACKED REPAIR CARRIED OUT IAW SRM 51-20-01, 51-30-2 - [SDR UPS01236284](https://openairdocs.org/sdr/UPS01236284), Jul 1, 2001: ANGLE. CORRODED. INSPECTION TYPE:C, RT MLG SUPPORT ANGLE CORRODED AT PRESSURE DECK SURFACE 2 AREAS, RBL 23 BS 880 TO 882. RT MLG SUPPORT ANGLE REPLACED IAW SRM 51-40-4. - [SDR UPS01236299](https://openairdocs.org/sdr/UPS01236299), Jun 29, 2001: STRAP. CORRODED. INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 560 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-30-2 & SRM 53-30-3. - [SDR UPS01235829](https://openairdocs.org/sdr/UPS01235829), May 8, 2001: BATTERY. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT AT A/C ENTRANCE WILL NOT TEST. REPLACED BATTERIES. - [SDR UPS00233150](https://openairdocs.org/sdr/UPS00233150), Jun 29, 2000: BATTERY. DISCHARGED. EMERGENCY LIGHT BATTERY DEAD R&R EMERGENCY LIGHT BATTERIES OPERATION CHECKS NORMAL - [SDR UPS00231767](https://openairdocs.org/sdr/UPS00231767), Feb 9, 2000: FRAME. CORRODED. INSPECTION TYPE:C, RIGHT MID CHORD IS CORRODED BS 300-306 WL 170 RBL 18, ACCESS RT MID CHORD. INSTALLED NEW MID CHORD REPLACED ACCESSED STRUCTURE PER SRM.* - [SDR UPS00231625](https://openairdocs.org/sdr/UPS00231625), Feb 9, 2000: SHEAR TIE. CORRODED. INSPECTION TYPE:C WHILE WORKING CUST ID NR 113675 FOUND CORROSION ON SHEAR TIE AT BS 312 BELOW STR RT SHEAR TIE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. R - [SDR UPS00231598](https://openairdocs.org/sdr/UPS00231598), Feb 9, 2000: SEAT TRACK. CORRODED. INSPECTION TYPE:C CORROSION IN FWD CARGO BAY ON SEAT TRACK IN 3 AREAS AT RBL 14 BS 577, BS 585, AND BS 591 ON UPPER AND LOWER SURFACE. REMOVED CORROSION FROM OU - [SDR UPS00231511](https://openairdocs.org/sdr/UPS00231511), Feb 5, 2000: CONDUIT. DAMAGED. INSPECTION TYPE:MOD, NR 2 ENGINE FUEL SOV CONDUIT WAS DAMAGED AT FWD END AND WIRING INSULATOR WAS PEELED OFF. INSTALLED NEW CONDUIT PER EO 00-0148. INSTALLED NE - [SDR UPS00231600](https://openairdocs.org/sdr/UPS00231600), Jan 31, 2000: ANGLE. CORRODED. INSPECTION TYPE:C CORROSION (C53-100-01.00-02) ON L/GANGLE AT BS 949, WL 198, LBL 39. REMOVED, FABRICATED AND INSTALLED NEW L ANGLE. WORK DONE IAW SRM'S 51-30-2 - [SDR UPS00231599](https://openairdocs.org/sdr/UPS00231599), Jan 31, 2000: ANGLE. CORRODED. INSPECTION TYPE:C CORROSION (C53-100-01.00-02) ON L/ANGLE AT BS 949, WL 198, LBL 29.5. REMOVED, FABRICATED AND INSTALLED NEW L ANGLE. WORK DONE IAW SRM'S 53-10- - [SDR UPS99231118](https://openairdocs.org/sdr/UPS99231118), Nov 15, 1999: LIGHT. INOP. INSPECTION TYPE: N/A, EMERGENCY EXIT LIGHT FWD ENTRY DOOR INTERMIT (REPEAT ITEM). ACCOMPLISHED VOLTAGE CHECK IAW MM 33-50-01, OPS CHECK GOOD. REPLACED LIGHT MOU - [SDR UPS99231053](https://openairdocs.org/sdr/UPS99231053), Nov 5, 1999: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT OVER FOWARD ENTRY DOOR COMES ON INTERMITTENLY WITH CORRESPONDING OVERHEAD PANEL SWITCH IN ARM POSITION. REMOVED AND REPLACED BATTERY PACK I - [SDR UPS98227266](https://openairdocs.org/sdr/UPS98227266), Aug 3, 1998: SPAR. CRACKED. INSPECTION TYPE-N/A, RT WING REAR SPAR U-CHANNEL CRACKED BETWEEN LIGHTENING HOLES DIRECTLY OVER RT MAIN LANDING GEAR STRUT, (MARKED IN RED). REPAIRED CRACKED AR - [SDR UPS98226495](https://openairdocs.org/sdr/UPS98226495), Apr 24, 1998: PITOT. CONTAMINATED. LOST CAPTAINS AIRSPEED INDICATOR ON TAKEOFF ROLL CONTINUED TAKEOFF NOTICED STBY AIRSPEED INDICATOR INOP AT 10,000 FT, WINDSHEAR/GRD PRX CAME ON THROUGH 500 FT. - [SDR UPS98226174](https://openairdocs.org/sdr/UPS98226174), Mar 25, 1998: BATTERY PACK. DISCHARGED. INSPECTION TYPE-N/A, INOP EMERGENCY EXIT LIGHT OVER CREW ENTRY DOOR. INSTALLED SERVICEABLE FWD ENTRY DOOR EMER EXIT LIGHT ASSY, BATTERIES TEST GOOD. - [SDR UPS97222643](https://openairdocs.org/sdr/UPS97222643), Apr 17, 1997: SPAR CHORD. CORRODED. INSPECTION TYPE:SI, CENTER SECTION UPPER REAR CHORD HAS EVIDENCE OF CORROSION SEPARATED FROM WEB LBL 6-36 WL 190. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED A - [SDR UPS97222638](https://openairdocs.org/sdr/UPS97222638), Apr 16, 1997: SILL. CORRODED. INSPECTION TYPE-SI, SSID (F-12) HFEC INSP OF UPPER SURFACE OF INNER SILL CHORD OF MAIN CARGO DOOR AT LBL 70 WL 208 BODY STATIONS 488, 501, 510 TO 520 525, 535, - [SDR UPS97222627](https://openairdocs.org/sdr/UPS97222627), Apr 16, 1997: SPAR. CORRODED. INSPECTION TYPE-SI, CORROSION LT FIN MID SPAR CHORD (S-7) IS CHAFED AND FRETTING AT FS 225.7. REPAIRED PER EWO NR 97-2111, UPS FILE NR 727-55-0347. - [SDR UPS97222621](https://openairdocs.org/sdr/UPS97222621), Apr 16, 1997: BEAM. DAMAGED. INSPECTION TYPE-SI, WHILE WORKING CUST ID C57-581-04-30 DISCOVERED O/B HOLE ON MLG BEAM COMMON TO NR 4 FLAP TRACK O/B HOLE TO HAVE THE UPPER SURFACE DAMAGED. RE - [SDR UPS97222623](https://openairdocs.org/sdr/UPS97222623), Apr 15, 1997: FRAME. CORRODED. INSPECTION TYPE-SI, CORROSION AROUND HANDLE HOUSING ON LT AFT EMERGENCY EXIT. REMOVED CORRODED FRAME PROCURED NEW FRAME AND INSTALLED IAW SRM 51-30-2. - [SDR UPS97222622](https://openairdocs.org/sdr/UPS97222622), Apr 15, 1997: FRAME. CORRODED. INSPECTION TYPE-SI, RT FWD EMERGENCY EXIT HAS CORROSION ON ITS HANDLE HOUSING. REMOVED CORRODED FRAME PROCURED NEW FRAME AND INSTALLED IAW SRM 51-30-2. - [SDR UPS97222620](https://openairdocs.org/sdr/UPS97222620), Apr 15, 1997: SKIN. CORRODED. INSPECTION TYPE-SI, LEFT WING LOWER SKIN CORRODED AT FLAP TRACK ATTACH POINT. REPAIRED PER EWO 97-2100 AND UPS ENG FILE NR 727-57-1803. - [SDR UPS97222618](https://openairdocs.org/sdr/UPS97222618), Apr 15, 1997: SPAR CHORD. CHAFED. INSPECTION TYPE-SI, CORROSION RT FIN MID SPAR CHORD (S-7) IS CHAFED AND FRETTING AT FS 225.7. REPAIRED PER EWO 97-2111 AND UPS ENG FILE NR 727-55-0347. - [SDR UPS97222586](https://openairdocs.org/sdr/UPS97222586), Apr 14, 1997: SKIN. CORRODED. INSPECTION TYPE-SI, WHILE WORKING CUST CARD NR 510847 FUSE 152 FOUND UPPER SIDE OF LOWER CENTER WING SKIN TO BE CORRODED AT STA 870 RBL 56. REMOVED CORROSION AN - [SDR UPS97222583](https://openairdocs.org/sdr/UPS97222583), Apr 11, 1997: FITTING. CRACKED. INSPECTION TYPE-SI, CRACK INDICATIONS ON RT 950 BODY FORGING FORWARD O/B FLANGE AFT ROW BETWEEN STR 10R AND 11R. REPAIRED RT 950 BODY FORGING PER UPS EO B727-53 - [SDR UPS97222579](https://openairdocs.org/sdr/UPS97222579), Apr 11, 1997: SUPPORT FTG. CORRODED. INSPECTION TYPE-SI, NR 11 SPOILER ACTUATOR FITTING LOWER MOUNT BOLT HOLES CORRODED. REMOVED AND REPLACED NR 11 SPOILER ACTUATOR SUPPORT FITTING IAW MM 27-51-131 - [SDR UPS97222578](https://openairdocs.org/sdr/UPS97222578), Apr 11, 1997: ACTUATOR FTG. CORRODED. INSPECTION TYPE-SI, NR 4 SPOILER SUPPORT FITTING LOWER MOUNT HOLES CORRODED. REMOVED AND REPLACED NR 4 SPOILER ACTUATOR FITTING IAW MM 27-61-01, MM 27-51-131, M All 126: https://openairdocs.org/deregistered/N909UP-2006-08-23/reports.md ## Other aircraft with N909UP - [Registered now](https://openairdocs.org/aircraft/N909UP): Cessna 750, S/N 750-0135, 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.