# N928UP: 1966 Boeing 727-22C, registration cancelled 2013-03-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 26, 2013
- Status when cancelled: Sale reported, canceled
- Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F)
- 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: 19091
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 28, 1966
- Last registry action: July 19, 2006
- Mode S code: ACDDB2
- 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/N928UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=928UP
- Page: https://openairdocs.org/deregistered/N928UP-2013-03-26

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 727-22C: https://openairdocs.org/model/boeing-727-22c.md

## Service difficulty reports (128, newest 50)

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

- [SDR UPS02239022](https://openairdocs.org/sdr/UPS02239022), Aug 8, 2002: STRINGER. CORRODED. INSPECTION TYPE:C MATERIAL LOSS INDICATION AT BS 259.5 AT STR.19 R/H. REMOVED FASTENERS IAW SRM 51-30-2. CORR NOT FOUND TO BE WITHIN LIMIT S IAW SRM 53-30-01. R
- [SDR UPS02238980](https://openairdocs.org/sdr/UPS02238980), Jul 31, 2002: YOKE. CORRODED. INSPECTION TYPE:C, LT BS 940 SWING LINK REMOVAL YOKE ASSY FOUND TO BE CORRODED. YOKE ASSY REPLACED IAW MM 57-15-01.
- [SDR UPS02239016](https://openairdocs.org/sdr/UPS02239016), Jul 30, 2002: FRAME. CORRODED. INSPECTION TYPE:C CORROSION ON FAIRING # 3334 ON FRAME AT L/H FAN INLET DOOR AFT AREA FRAME REPAIR CARRIED OUT IAW SRM 51-40-4 L/H FAN INLET DOOR REPLACED IAW M
- [SDR UPS02239021](https://openairdocs.org/sdr/UPS02239021), Jul 26, 2002: LINK. DAMAGED. INSPECTION TYPE:C, LEFT MLG BEAM SWING LINK BOLT HOLE HAS MECHANICAL DAMAGE. REPAIR CARRIED OUT IAW SMRO EO 2002-040-004 UPS ENGINEERING FILE 727-57-20059.
- [SDR UPS02239018](https://openairdocs.org/sdr/UPS02239018), Jul 25, 2002: PANEL. DELAMINATED. INSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED, INNER SURFACE FWD END. REPAIRED IAW SRM 51-40-5.
- [SDR UPS02239017](https://openairdocs.org/sdr/UPS02239017), Jul 25, 2002: PANEL. DELAMINATED. INSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER, SURFACE FWD END. REPAIRED IAW SRM 51-40-5.
- [SDR UPS02238984](https://openairdocs.org/sdr/UPS02238984), Jul 24, 2002: STRAP. CRACKED. INSPECTION TYPE:C, FLOORBOARD SUPPORT STRAP CRACKED BS 850 LBL 45.5. FLOORBOARD SUPPORT STRAP REPLACED BS 850 LBL 45.5 IAW SRM 53-20-2.
- [SDR UPS02239025](https://openairdocs.org/sdr/UPS02239025), Jul 23, 2002: FITTING. CRACKED. INSPECTION TYPE:C LH WHEEL WELL BS 940 FORGING HAS A SUSPECT CRACK @ BASE OF PREVIOUS BLENDOUT FITTING REPLACED IAW UPS EO B727-5310-4501
- [SDR UPS02239011](https://openairdocs.org/sdr/UPS02239011), Jul 23, 2002: CHANNEL. CRACKED. INSPECTION TYPE:C CRACK ON CHANNEL SECTION IN LWR AFT CARGO HOLD AT BS 1060 BBL 8L REPAIRED IAW SRM 53-10-5 FIG 4
- [SDR UPS02239010](https://openairdocs.org/sdr/UPS02239010), Jul 23, 2002: FRAME. CRACKED. INSPECTION TYPE:C, LEFT WHEEL WELL, BS 930 FRAME IS CRACKED ON INNER FLANGE UPPER HOLE. REPAIR CARRIED OUT IAW UPS EO B727-5310-2611-B.
- [SDR UPS02239009](https://openairdocs.org/sdr/UPS02239009), Jul 23, 2002: STIFFENER. CRACKED. INSPECTION TYPE:C, MAIN CARGO DECK COMPARTMENT BS 1183 STIFFENER TIE CRACKED AT RBL 361 UPPER TIE BETWEEN VERT BEAM AT RBL 26.83 & RBL 36.83. NEW STIFFENER INST
- [SDR UPS02239029](https://openairdocs.org/sdr/UPS02239029), Jul 22, 2002: SKIN. CORRODED. INSPECTION TYPE:C, 15 TO 20 PERCENT MATERIAL LOSS INDICATION AT BS 1080 STR 4R. REPAIR CARRIED OUT IAW UPS EO B727-5330-1177 & SMRO EO 2002-040-005 UPS ENGINEER
- [SDR UPS02239023](https://openairdocs.org/sdr/UPS02239023), Jul 22, 2002: SKIN. CORRODED. INSPECTION TYPE:C, MATERIAL LOSS INDICATIONS AT BS 521 AFT SKIN FROM STR 1 TO STR 2 OF 15 - 20 PERCENT AND FROM STR 3R TO STR 4R OF 20 PERCENT AND ON FWD SKIN A
- [SDR UPS02239020](https://openairdocs.org/sdr/UPS02239020), Jul 22, 2002: DOUBLER. CRACKED. INSPECTION TYPE:C CRACK ON R/H WINDOW POST BETWEEN R1 & R2 WINDOWS AT UPPER CORNER REPAIR DOUBLER FABRICATED IAW SRM 53-30-3 REPAIR DOUBLER INSTALLED IAW SRM 53
- [SDR UPS02239012](https://openairdocs.org/sdr/UPS02239012), Jul 22, 2002: WINDOW POST. CRACKED. INSPECTION TYPE:C CRACKS ON CENTER WINDOW POST ON LWR LHS & RHS COCKPIT CENTER WINDOW POST REPAIRED IAW UPS EO B727-5330-5128
- [SDR UPS02239013](https://openairdocs.org/sdr/UPS02239013), Jun 26, 2002: STRUCTURE. CRACKED. INSPECTION TYPE:C PLS CARRY OUT PERMANENT REPAIR TO NR 2 L/E SLAT DENT (APPROX 1.5 FT O/B OF ACTUATOR). PERMANENT REPAIR CARRIED OUT ON NR 2 L/E SLAT IAW SRM 57
- [SDR UPS01236010](https://openairdocs.org/sdr/UPS01236010), May 26, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:N/A, RT WHEEL WELL CRACKS. *S/D* REPAIRED PER SRM 51-1-9A.
- [SDR UPS01235658](https://openairdocs.org/sdr/UPS01235658), Apr 21, 2001: CONTROL ROD. LACK OF LUBE. INSPECTION TYPE:IN AILERON STIFF IN LEFT TURNS AILERON SPRING CARTRIDGE FOUND OUT OF RIG. RE-ADJUSTED I.A.W. B727 M .M.27-61-21. SPRING CARTRIDGE OPS CHECKS SER
- [SDR UPS01234776](https://openairdocs.org/sdr/UPS01234776), Jan 26, 2001: PITOT TUBE. DAMAGED. INSPECTION TYPE:IN AT FL 33.0 CAPTS ALT 33,000 FT F/OS ALT 32820 FT CAPTS A/S 296 KNOTS F/OS A/S 294.5. STANDBY ALT 33,200. TESTED CAPT AND FO ALT PER MM 34-12-
- [SDR UPS01234762](https://openairdocs.org/sdr/UPS01234762), Jan 17, 2001: HEAT EXCHANGER. LEAKING. INSPECTION TYPE:C, RT WING HYDRAULIC HEAT EXCHANGER LEAKING HYD FLUID INTO NR 3 TANK. ACCOMPLISHED RIGHT WING HYDRAULIC COOLER ANTI-ROTATION PLATE REPLACEMENT I
- [SDR UPS01234765](https://openairdocs.org/sdr/UPS01234765), Jan 11, 2001: FRAME. CRACKED. INSPECTION TYPE:C, LEFT WHEEL WELL CASTING FRAME BS 930 SHOWS CRACK TO LOWER END STR 18L. INSTALLED REPAIR AT BS 930 CASTING FRAME IAW UPS EO B727-5310-2611B.
- [SDR UPS01234770](https://openairdocs.org/sdr/UPS01234770), Jan 3, 2001: ANGLE. CRACKED. INSPECTION TYPE:C, RT WING NR 6 LE SLAT, I/B TRACK RECESS CUTOUT 2 ANGLES CRACKED, I/B AND O/B AT LWR END OF ANGLE. REMOVED AND REPLACED 2 ANGLES IAW SRM 57-10-
- [SDR UPS01234767](https://openairdocs.org/sdr/UPS01234767), Jan 3, 2001: ANGLE. CRACKED. INSPECTION TYPE:C, RT WING NR 6 LE SLAT, O/B TRACK RECESS CUTOUT, I/B VERT ANGLE CRACKED AT LWR END. REMOVED AND REPLACED I/B VERT ANGLE IAW SRM 51-30-2.
- [SDR UPS01234764](https://openairdocs.org/sdr/UPS01234764), Jan 3, 2001: SKIN. BULGED. INSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGING AT BS 610, STR 4L. INSTALLED DOUBLER REPAIR IAW 52-30-01.
- [SDR UPS01234763](https://openairdocs.org/sdr/UPS01234763), Jan 3, 2001: SKIN. BULGED. INSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGED AT BS 490, STR 4 LEFT. INSTALLED REPAIR AT MAIN CARGO DOOR SKIN IAW SRM 52-30-01.
- [SDR UPS01234772](https://openairdocs.org/sdr/UPS01234772), Jan 2, 2001: SKIN. BULGED. INSPECTION TYPE:C, SKIN BULGING AT STR 2L, STA 441. ACCOMPLISHED REPAIR IAW UPS EO B727-5310-1371E.
- [SDR UPS01234771](https://openairdocs.org/sdr/UPS01234771), Jan 2, 2001: SKIN. CRACKED. INSPECTION TYPE:C, NOSE LANDING GEAR WHEEL WELL TOP CEILING BS 272, LBL 15 SHOWS CRACK RUNNING BETWEEN RIVETS, ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR I
- [SDR UPS01234766](https://openairdocs.org/sdr/UPS01234766), Jan 2, 2001: SKIN. BULGED. INSPECTION TYPE:C, SKIN BULGING BETWEEN STR 5R AND STR 6R AT STA 481. INSTALLED REPAIR DOUBLER IAW UPS EO B727-5310-1371E.
- [SDR UPS01234759](https://openairdocs.org/sdr/UPS01234759), Jan 2, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS272 LWR OF AFT ACCESS DOOR CRACK INDICATION RUNNING BETWEEN FASTENER ROW, 1.5 INCH LONG. INSTALLED DOUBLER REPAIR
- [SDR UPS01234758](https://openairdocs.org/sdr/UPS01234758), Jan 2, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C CK, NLG W/W LT SIDEWALL BS 243 TO LWR SHOWED CRACK AROUND FASTENER, ABOU T 1 INCH LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-
- [SDR UPS01234757](https://openairdocs.org/sdr/UPS01234757), Jan 2, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C CK, NLG W/W TOP CEILING RBL 15 AND BS 272 CRACK INDICATION ALONG FASTENER ROW ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WI
- [SDR UPS01234756](https://openairdocs.org/sdr/UPS01234756), Jan 2, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS 251 AFT OF FWD ACCESS DOOR, CRACK INDICATION ALONG FASTENERS ROW, ABOUT 4.5 INCHES. INSTALLED DOUBLER REPAIR IN 
- [SDR UPS01234755](https://openairdocs.org/sdr/UPS01234755), Jan 2, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C CK, NOSE LANDING GEAR WHEEL WELL SIDEWALL RIGHT BS 290 TO LWR HAS CRACK INDICATION MIGRATING FROM PREVIOUS REPAIR ABOUT 1 INCH LONG. INSTALLED
- [SDR UPS01234761](https://openairdocs.org/sdr/UPS01234761), Dec 31, 2000: SKIN. BULGED. INSPECTION TYPE:C, BULGE IN SKIN AT STA 260 LEFT WL 270. REPAIRED PER UPS EO B727-5310-1371E.
- [SDR UPS01234753](https://openairdocs.org/sdr/UPS01234753), Dec 29, 2000: SUPPORT BRACKET. CRACKED. INSPECTION TYPE:C CK, LEFT WHEEL WELL STA 913 UPLOCK SUPPORT ASSY, CRACK AT AFT SUPPORT FRAME. CRACK VERIFIED BY NDT. REPAIRED STA 913 SUPPORT FRAME IN ACCORDAN
- [SDR UPS01234760](https://openairdocs.org/sdr/UPS01234760), Dec 26, 2000: SKIN. BULGED. INSPECTION TYPE:C CK, FUSELAGE AFT RIGHT BS 1333 STR 8R TO STR 10R, SKIN BULGE AND FASTENERS PULLING THROUGH. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 54
- [SDR UPS00232079](https://openairdocs.org/sdr/UPS00232079), Mar 22, 2000: LIGHT. INOPERATIVE. EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. CANIBALIZED EMERGENCY LIGHT ASSY FROM AIRCRAFT 907 OPS CHECKED GOOD.
- [SDR UPS99231048](https://openairdocs.org/sdr/UPS99231048), Nov 4, 1999: LIGHT. MISSING. INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERGENCY EXIT LIGHT ROBBED FOR ACFT 910. INSTALLED FWD ENTRY DOOR EMERGENCY EXIT LIGHT, OPS CHECK GOOD.
- [SDR UPS99230117](https://openairdocs.org/sdr/UPS99230117), Jul 9, 1999: DUCT. CRACKED. INSPECTION TYPE:C, ENGINE NR 3 ANTI-ICE DUCT CRACKED AT BRACKET NEAR ANTI-ICE VALVE. DUCT REPAIRED PER SMRO EO 99-17-005 (UPS ENGINEERING FILE NR 727-30- 0009).
- [SDR UPS99230116](https://openairdocs.org/sdr/UPS99230116), Jul 9, 1999: SKIN. DELAMINATED. INSPECTION TYPE:C, RUDDER LOWER TAB DELAMINATED AT UPPER T/E LEFT SIDE PREVIOUS REPAIR. REPAIRED IAW SRM 51-40-10 FIG 3.
- [SDR UPS99230107](https://openairdocs.org/sdr/UPS99230107), Jul 9, 1999: CLEVIS. CRACKED. INSPECTION TYPE:C, ENGINE NR 2 STRUTS ABOVE NR 2 HORIZONTAL FIRE WALL, CLEVIS CRACKED ON LOWER END OF LOWER STRUT. CLEVIS REPLACED IAW DWG 65-17553.
- [SDR UPS99230120](https://openairdocs.org/sdr/UPS99230120), Jul 8, 1999: BALANCE PANEL. CORRODED. INSPECTION TYPE:C, NR 5 ELEVATOR BALANCE PANEL RT HAS EVIDENCE OF CORROSION ON PANEL TO HINGE ATTACH RACK. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW S
- [SDR UPS99230106](https://openairdocs.org/sdr/UPS99230106), Jul 8, 1999: WEB. CORRODED. INSPECTION TYPE:C, CORROSION ON SHEAR WEB LBL 24.75 STA 1130-1183. WEB REPAIRED IAW SRM 51-40-2.
- [SDR UPS99230124](https://openairdocs.org/sdr/UPS99230124), Jul 7, 1999: ANGLE. CRACKED. INSPECTION TYPE:C, FLOOR SUPPORT CRACKED BS 850 LBL 45.5. FLOOR SUPPORT ANGLE REPAIRED IAW SRM 57-20-1.
- [SDR UPS99230119](https://openairdocs.org/sdr/UPS99230119), Jul 7, 1999: MOUNT. CORRODED. INSPECTION TYPE:C, CORROSION FOUND ON NR 1 ENG, FWD MOUNT HOLE AFT I/B HOLE ONLY (PITTING CORROSION). INVESTIGATED AND REPAIRED IAW SMRO EO 99-17-002 UPS ENGINE
- [SDR UPS99230118](https://openairdocs.org/sdr/UPS99230118), Jul 7, 1999: MOUNT. CORRODED. INSPECTION TYPE:C, CORROSION FOUND ON NR 3 ENG FWD MOUNT HOLES AT TRUNNION FITTING ATTACH (PITTING CORROSION). REPAIRED IAW SRMO EO 99-17-003 (UPS ENGINEERING F
- [SDR UPS99230103](https://openairdocs.org/sdr/UPS99230103), Jul 7, 1999: RIB. CRACKED. INSPECTION TYPE:C, NR 6 SLAT RIB AT IB SIDE OF ACTUATOR HAS SMALL CRACK IN FWD LOWER RADIUS. RIB REPAIRED IAW SRM 57-50-3.
- [SDR UPS99230121](https://openairdocs.org/sdr/UPS99230121), Jul 6, 1999: FIREWALL WEB. CRACKED. INSPECTION TYPE:C, STRUCTURE OVER NR 2 ENGINE HORIZ FIREWALL LEFT AND RIGHT WEBS AT BS 1376 ARE CRACKED. FABRICATED AND INSTALLED WEBS IAW DRG NR 65-17555.
- [SDR UPS99230110](https://openairdocs.org/sdr/UPS99230110), Jul 6, 1999: STIFFENER. CRACKED. INSPECTION TYPE:C, NR 4 SPOILER IB ATTACH VERTICAL LEG CRACKED VERTICAL STIFFENER. REPLACED IAW DWG 69-16201.
- [SDR UPS99230105](https://openairdocs.org/sdr/UPS99230105), Jul 6, 1999: SUPPORT. CORRODED. INSPECTION TYPE:C, CORROSION FOUND ON AFT LT LAVATORY PARTITION SUPPORT ON FLOOR STRUCTURE BS 1140 LBL 24.75-LBL60. TOP HAT SECTION REPLACED IAW SRM 51-10-1.

All 128: https://openairdocs.org/deregistered/N928UP-2013-03-26/reports.md

## FAA accident and incident reports (2)

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 19910504019109I](https://openairdocs.org/incident/19910504019109I), May 4, 1991: Boeing 72722C (N928UP), Kansas City, MO. NR4 main tire blew during landing roll. Anti-skid released only the right inboard position with brakes applied.
- [Incident 19861224076719I](https://openairdocs.org/incident/19861224076719I), Dec 24, 1986: Boeing 72722C (N928UP), Denver, CO. Ground personnel attempted to chock front wheels before aircraft came to a stop. Hand caught and injured.

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