# N936UP: 1985 Boeing 727-108C, registration cancelled 2008-08-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 4, 2008
- Status when cancelled: Sale reported
- Airframe: [Boeing 727-108C](https://openairdocs.org/model/boeing-727-108c) (registry code 1384039)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 19503
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, normal
- Airworthiness date: February 5, 1985
- Last registry action: March 28, 2008
- Mode S code: ACFDC3
- 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/N936UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=936UP
- Page: https://openairdocs.org/deregistered/N936UP-2008-08-04

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 727-108C: https://openairdocs.org/model/boeing-727-108c.md

## Service difficulty reports (263, newest 50)

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

- [SDR UPS07248814](https://openairdocs.org/sdr/UPS07248814), Jan 1, 2007: LATCH. BROKEN. INSPECTION TYPE:N/A MAIN CABIN DOOR ENTRY EMERGENCY DOOR SLIDE LATCH ASSY BROKEN. INSTALLED NEW LATCH ON EMERGENCY SLIDE ASSY AS OUTLINED IN AMM 25-60-15-2 (IPC
- [SDR UPS06248627](https://openairdocs.org/sdr/UPS06248627), Nov 14, 2006: LIGHT. MALFUNCTIONED. INSPECTION TYPE: N/A EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT COULD NOT RESET. STAYED ON. ACCOMPLISHED EMERGENCY LIGHTING ADJUSTMENT/TEST IAW MM 33-50-01-5. S
- [SDR UPS06247727](https://openairdocs.org/sdr/UPS06247727), Aug 19, 2006: SHEAR TIE. CRACKED. INSPECTION TYPE:SV SHEAR TIE CRACKED AT STA 441 STR 26L. REMOVED CRACKED SHEAR TIE AT STA 441 STR 26L IAW SRM 51-30-02, FABRICATED AND INSTALLED SHEAR TIE AT ST
- [SDR UPS06246772](https://openairdocs.org/sdr/UPS06246772), Apr 29, 2006: CONNECTOR. INOPERATIVE. IN FLIGHT, CAPTAIN'S VOR/FLAG INDICATED RED. STATIONS SELECTED ALL ALONG FLIGHT WITH NO GOOD INDICATION ON EASI. TAE NAV 1 DENTS WERE GOOD, DME AND RMI NEEDLES 
- [SDR UPS06246100](https://openairdocs.org/sdr/UPS06246100), Jan 13, 2006: SKIN. CORRODED. INSPECTION TYPE:C EVIDENCE OF FRETTING FOUND AT BS 1080 TO 1139.5 FROM STR 24L TO STR 26 L ON THE SKIN. SKIN REPLACMENT REQUIRED AT THIS LOCATION, CARRIED OUT I
- [SDR UPS06246098](https://openairdocs.org/sdr/UPS06246098), Jan 13, 2006: MOUNT. CORRODED. INSPECTION TYPE:A ENG NR 1 PYLON FWD ENGINE MOUNT, AFT O/B HOLE PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS06246097](https://openairdocs.org/sdr/UPS06246097), Jan 13, 2006: MOUNT. CORRODED. INSPECTION TYPE:C NR 1 PYLON FWD ENGINE MOUNT FWD O/B HOLE, HAS PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS06246096](https://openairdocs.org/sdr/UPS06246096), Jan 13, 2006: MOUNT. CORRODED. INSPECTION TYPE:C NR 3 PYLON FWD ENGINE MOUNT, AFT O/B HOLE HAS PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS06246095](https://openairdocs.org/sdr/UPS06246095), Jan 13, 2006: MOUNT. CORRODED. INSPECTION TYPE:C NR 3 PYLON FWD ENGINE MOUNT, FWD O/B HOLE PITTING CORROSION IN BORE OF HOLE. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.
- [SDR UPS06246094](https://openairdocs.org/sdr/UPS06246094), Jan 13, 2006: MOUNT. CORRODED. INSPECTION TYPE:C NR 3 PYLON FWD MOUNT, FWD I/B HOLE HAS PITTING CORROSION. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS06246102](https://openairdocs.org/sdr/UPS06246102), Jan 12, 2006: BEAM. CORRODED. INSPECTION TYPE:C CORROSION FOUND ON RT FWD FACE OF HORIZONTAL BEAM ATTACH POINT TO BS 740 FITTING. REPLACED HORIZONTAL BEAM IAW SRM NR 51-30-2 AND DRW NO.65-15
- [SDR UPS06246101](https://openairdocs.org/sdr/UPS06246101), Jan 12, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE:C ON REMOVAL OF FLOORBOARD AT BS 360 EVIDENCE OF CORROSION FOUND. UPPER CHORD OF FLOORBEAM REMOVED BETWEEN RBL 12 AND LBL 67 AT BS 360. REPAIR C
- [SDR UPS06246085](https://openairdocs.org/sdr/UPS06246085), Jan 10, 2006: ANGLE. CORRODED. INSPECTION TYPE-C RT FUSE ABOVE NR 2 ENG AT THE ANGLE BETWEEN FUSE AND VERT STAB HAS LIGHT SURFACE CORROSION AT BS1428 TO 1464. DAMAGED ANGLE REMOVED AND REPLAC
- [SDR UPS06246099](https://openairdocs.org/sdr/UPS06246099), Jan 3, 2006: MOUNT. CORRODED. INSPECTION TYPE:C NR 1 PYLON FWD ENGINE MOUNT, FWD I/B HOLE, PITTING CORROSION IN THE BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS05244442](https://openairdocs.org/sdr/UPS05244442), May 12, 2005: OXYGEN MASK. INOPERATIVE. CREW PREFLIGHT - F/O O2 MASK WOULD NOT TRANSMIT. REMOVED AND REPLACED F/O'S 02 MASK ASSY. OPS CKS GOOD IAW MM 35-11-00.
- [SDR UPS04243067](https://openairdocs.org/sdr/UPS04243067), Aug 26, 2004: ATTACH ANGLE. CORRODED. INSPECTION TYPE: C, DURING INSPECTION OF SKIN REPAIR, AT 1334 LT SIDE AFT AIRSTAIRS, SKIN ATTACH ANGLE FOUND CORRODED. REPLACED ATTACH ANGLE IAW SRM 51-10-01.
- [SDR UPS04243032](https://openairdocs.org/sdr/UPS04243032), Aug 26, 2004: SUPPORT BRACKET. CRACKED. INSPECTION TYPE: C, SUPPORT BRACKET FOR NR 5 FWD FLAP TRACK FAIRING FOUND CRACKED ON O/B SIDE OF NR 5 FLAP TRACK. SUPPORT BRACKET REMOVED IAW SRM 51-30-02, NEW 
- [SDR UPS04243079](https://openairdocs.org/sdr/UPS04243079), Aug 23, 2004: CASTING. CRACKED. INSPECTION TYPE: C, CRACK ON NR 7 FLAP TRACK CASTING ON VERTICAL FLANGE SECOND FROM I/B. HFEC CARRIED OUT - CRACKS CONFIRMED AND ENDS MARKED. STOP DRILLED CRACK
- [SDR UPS04243070](https://openairdocs.org/sdr/UPS04243070), Aug 23, 2004: STIFFENER. CORRODED. INSPECTION TYPE: C, HORIZONTAL STIFFNER CORRODED AFT OF APU EXHAUST PORT ON LOWER SURFACE OF UPPER PANEL AT 2 LOCATIONS. CORROSION FOUND TO BE OUTSIDE LIMITS. S
- [SDR UPS04243068](https://openairdocs.org/sdr/UPS04243068), Aug 23, 2004: STRAP. CORRODED. INSPECTION TYPE: C ON INSP FLOOR PANEL SPLICE STRAP FOUND BADLY CORRODED AT BS 520 BETWEEN RBL 24 AND LBL 24. SPLICE STRAP REPLACED IAW SRM 51-20-01
- [SDR UPS04243066](https://openairdocs.org/sdr/UPS04243066), Aug 23, 2004: LIGHT. DEFECTIVE. INSPECTION TYPE: C-COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH SWITCH ON P5 PANEL TO ON. LIGHT ASSEMBLY FOUND DEFECTIVE IAW WDM 33-51-01. LIGHT ASSY REPLAC
- [SDR UPS04243080](https://openairdocs.org/sdr/UPS04243080), Aug 22, 2004: SKIN. CORRODED. INSPECTION TYPE:C, SUSPECT CORROSION BS 1340 BETWEEN STR 8L AND 9L DAMAGED SKIN REMOVED FROM BS 1323 TO BS 1342, FROM FIN TO STR 10L IAW SRM 51-10-6 AND REPAIRE
- [SDR UPS04243077](https://openairdocs.org/sdr/UPS04243077), Aug 22, 2004: DOUBLER. CRACKED. INSPECTION TYPE: C, CRACK ON DOUBLER RT SIDE BS 1444 APPROX. CRACK CUT OUT IAW SRM 51-40-02. HFEC CARRIED OUT IAW NDT MANUAL 51- 00-00 PT 6 FIG 4. NO DEFECTS FO
- [SDR UPS04243081](https://openairdocs.org/sdr/UPS04243081), Aug 17, 2004: SPAR. CORRODED. INSPECTION TYPE: C, CRACK INDICATION AT WS 205 ON LT UPPER CHORD REAR SPAR. REPAIR CARRIED OUT IAW AAAE EO 2004-077-005. REF UPS EO B727-5710-20995.
- [SDR UPS04243062](https://openairdocs.org/sdr/UPS04243062), Aug 17, 2004: SKIN. DEBONDED. INSPECTION TYPE:C LT OB MIDFLAP T-EDGE WEDGE UPPER SKIN DISBOND 45 INCHES IB OF OB EDGE. DAMAGE REPAIRED IAW SRM 51-40-5
- [SDR UPS04243063](https://openairdocs.org/sdr/UPS04243063), Aug 16, 2004: LAP JOINT. CORRODED. INSPECTION TYPE: C, SUSPECT CORROSION AT LAP JOINT S19L BETWEEN BS 390 AND BS 441, CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02. REPAIR CARRIED OUT IAW 
- [SDR UPS04243076](https://openairdocs.org/sdr/UPS04243076), Aug 13, 2004: SKIN. CORRODED. INSPECTION TYPE: C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 217 STR 25L. AREA PAINT STRIPPED IAW MM 51-20-15. TRIMMED CORRODED AREA IAW SRM 53-
- [SDR UPS04243064](https://openairdocs.org/sdr/UPS04243064), Aug 12, 2004: SKIN. CRACKED. C-CRACKS ON CENTER POST OF COCKPIT WINDOWS, NR 1 LT AND NR 1 RT, LOWER IB CORNERS. HFEC CARRIED OUT AND CRACKS CONFIRMED. CRACKED SKIN REPLACED IAW AAAE EO 2004
- [SDR UPS03241671](https://openairdocs.org/sdr/UPS03241671), Dec 23, 2003: LIGHT. INOPERATIVE. INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT FOR CABIN INOP. REMOVED AND REPLACED CABIN EMERGENCY LIGHTING FIXTURE PER MM 33-50. OPS CHECKS NORMAL AT THIS TIME.
- [SDR UPS03241668](https://openairdocs.org/sdr/UPS03241668), Dec 18, 2003: LIGHT. INOPERATIVE. INSPECTION TYPE:PFLT CABIN DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED CABIN DOOR, EMERGENCY EXIT LIGHT OPS CHECKS NORMAL AT THIS TIME PER MM 33-50.
- [SDR UPS03241214](https://openairdocs.org/sdr/UPS03241214), Sep 10, 2003: BATTERY. DISCHARGED. INSPECTION TYPE: ASV, EMERGENCY EXIT LIGHTS INOPERATIVE IN COCKPIT AND FORWARD ENTRY REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY. OPS CKS GOOD.
- [SDR UPS03240298](https://openairdocs.org/sdr/UPS03240298), Feb 28, 2003: FLOORBEAM. CORRODED. INSPECTION TYPE: C&SI, CORROSION ON FLOORBEAM TOP CAP BS 950 LBL 50. REPAIR CARRIED OUT IAW SRM EO 2003-008-022. UPS ENGINEERING FILE 7 27-53-20100.
- [SDR UPS03240279](https://openairdocs.org/sdr/UPS03240279), Feb 26, 2003: DOUBLER. CORRODED. INSPECTION TYPE: C&SI, ON REMOVAL OF WINDOW FRAME TO FACILITATE BS 870 FITTING REPLACEMENT CORROSION FOUND ON FLANGE OF WINDOW FRAMES, FRAME AT BS 880 AT LWR AF
- [SDR UPS03240293](https://openairdocs.org/sdr/UPS03240293), Feb 25, 2003: FITTING. CRACKED. INSPECTION TYPE: C&SI, DURING REMOVAL OF UPPER AIRSTAIR THREADS IT WAS NOTED THAT THE TAILSKID ACTUATOR FITTING (RT SIDE) WAS CRACKED (TRUNNION FITTING). TAILSK
- [SDR UPS03240292](https://openairdocs.org/sdr/UPS03240292), Feb 25, 2003: YOKE. CRACKED. INSPECTION TYPE: C&SI, DURING REMOVAL OF TAILSKID ACTUATOR FITTING, TAILSKID YOKE ASSY FOUND CRACKED. TAILSKID YOKE ASSY REPLACED IAW MM 32-71-41.
- [SDR UPS03240278](https://openairdocs.org/sdr/UPS03240278), Feb 25, 2003: STIFFENER. CRACKED. INSPECTION TYPE:C&SI #6 FLAP TRACK AFT O/B ATTACH POINT VERTICAL STIFFENER ON R/H FALSE S PAR CRACKED STIFFENER REMOVED IAW SRM 51-30-2. STIFFENER REPLACED IAW 
- [SDR UPS03240256](https://openairdocs.org/sdr/UPS03240256), Feb 25, 2003: PAD. CORRODED. INSPECTION TYPE:C&SI #6 FLAP TRACK AFT ATTACH POINT LWR PAD ON R/H FALSE SPAR HAVE EVIDEN CE OF CORROSION REMOVED PAD IAW SRM 51-30-02. ON REMOVAL OF CORROAION,
- [SDR UPS03240300](https://openairdocs.org/sdr/UPS03240300), Feb 23, 2003: SKIN. CORRODED. INSPECTION TYPE:C&SI EVIDENCE OF CORROSION BETWEEN WING CENTER SECTION UPPER SKIN & SKIN UPPER SPLICE @ BS 856 - 860 I/B OF WBL 70.5 RIGHT REPAIR CARRIED OUT IA
- [SDR UPS03240254](https://openairdocs.org/sdr/UPS03240254), Feb 23, 2003: STIFFENER. CORRODED. INSPECTION TYPE: C&SI, CORROSION ON INTERNAL SIDE OF NLG LT SIDE WALL AT BS 285 (FWD OF VERTICAL STIFFENER) LWR END CORROSION FOUND AT BS 280 & 285 BETWEEN STIF
- [SDR UPS03240290](https://openairdocs.org/sdr/UPS03240290), Feb 21, 2003: SEAT TRACK. CORRODED. INSPECTION TYPE:C&SI CABIN SEAT TRACK AT STA 650 TO 680 HAS CORROSION ON O/B FLANGE OF T RACK LBL 45.5. CORROSION REMOVED IAW SRM 53-10-1 OUT OF LIMITS. SEAT TR
- [SDR UPS03240274](https://openairdocs.org/sdr/UPS03240274), Feb 21, 2003: STIFFENER. CORRODED. INSPECTION TYPE: C+SI, VERT STIFFENER HAS INTERGRANULAR CORROSION AT BS 343 APPROX AT NLG CUTOUT LT VERT WEB. INSTALLED NEW STIFFENER IAW SRM 51-30-02.
- [SDR UPS03240255](https://openairdocs.org/sdr/UPS03240255), Feb 21, 2003: CASTING. CORRODED. INSPECTION TYPE: C&SI, LT O/B AILERON TAB FIRST & SECOND FROM O/B HINGE CASTINGS HAVE PITTING CORROSION. HINGE CASTINGS REPLACED IAW MM 27-10-19.
- [SDR UPS03240294](https://openairdocs.org/sdr/UPS03240294), Feb 20, 2003: SEAT TRACK. CORRODED. INSPECTION TYPE:C&SI CORROSION ON SEAT TRACK LBL 42.84 BETWEEN BS 344 & 480 SEAT TRACK REMOVED IAW SRM 51-30-2. NEW SEAT TRACK FABRICATED IAW S RM 51-20-1. NEW 
- [SDR UPS03240289](https://openairdocs.org/sdr/UPS03240289), Feb 19, 2003: FITTING. CRACKED. INSPECTION TYPE:C&SI L/H 870 FITTING HAS 2 CRACKS FWD OF CENT. LINE IN 1ST ROW OF FASTENE RS (HOLES 3 & 4) AND 1 CRACK IN AFT OF BUTT LINE 1ST ROW 3RD FASTENE R
- [SDR UPS03240281](https://openairdocs.org/sdr/UPS03240281), Feb 19, 2003: FRAME. CRACKED. INSPECTION TYPE: C&SI, SUB FRAME AT BS 920 RT HAS SMALL CRACK AT STR 15. SUB FRAME AT BS 920 RT REPAIRED IAW SRM 51-40-03.
- [SDR UPS03240280](https://openairdocs.org/sdr/UPS03240280), Feb 19, 2003: FLOORBEAM. CORRODED. INSPECTION TYPE: C&SI, CORROSION ON FLOORBEAM TOP CAP BS 344 RBL 24.75 TO 24.75 LBL. CORROSION REMOVED IAW SRM 51-10-6 DEPTH OF BLEND-OUTS MEASURED AND FOUND TO
- [SDR UPS03240273](https://openairdocs.org/sdr/UPS03240273), Feb 19, 2003: CARRIAGE. CORRODED. INSPECTION TYPE:C+SI NO.7 FLAP TRACK CARRIAGE HAS PITTING COROSION ON BEARING MOUNT HOLE. FLAP TRACK CARRIAGE REPLACED IAW SB 27-112.
- [SDR UPS03240309](https://openairdocs.org/sdr/UPS03240309), Feb 18, 2003: FLAP TRACK. CORRODED. INSPECTION TYPE: C&S, NR 3 FLAP TRACK HAS SURFACE CORROSION IN THE FOLLOWING AREAS, INSIDE HOLE D, INSIDE HOLE E, INSIDE HOLE F, INSIDE HOLE G & FLAP AFT PAD (B
- [SDR UPS03240308](https://openairdocs.org/sdr/UPS03240308), Feb 18, 2003: ATTACH FITTING. CORRODED. INSPECTION TYPE: C&SI, NR 7 FLAP TRACK HAS SURFACE CORROSION ON FWD MOUNT LUG FACES A & D AND IN FWD LUG BOREHOLES. REPAIR CARRIED OUT IAW SRMO EO'S 2002-008-00
- [SDR UPS03240307](https://openairdocs.org/sdr/UPS03240307), Feb 18, 2003: ATTACH FITTING. CORRODED. INSPECTION TYPE: C&SI, ON INSPECTION OF NR 2 FLAP TRACK CORROSION FOUND ON FWD MOUNT LUG FACES A, B, C & D AND IN FWD LUG BOREHOLES A & B. REPAIR CARRIED OUT IA

All 263: https://openairdocs.org/deregistered/N936UP-2008-08-04/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 20010316004949I](https://openairdocs.org/incident/20010316004949I), Mar 16, 2001: Boeing 727108C (N936UP), Cedar Rapids, IA. (-23) Ups 5526 landed at Cedar Rapids, Iowa on runway 9 at 0540 and slid off the north side runway approx. 5000 feet from the approach end. The airport was…

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