# N929UP: 1966 Boeing 727-22C, registration cancelled 2006-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2006 - Status when cancelled: Sale reported - 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: 19092 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 29, 1966 - Last registry action: April 4, 2005 - Mode S code: ACE169 - 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/N929UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=929UP - Page: https://openairdocs.org/deregistered/N929UP-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 727-22C: https://openairdocs.org/model/boeing-727-22c.md ## Service difficulty reports (163, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS03240133](https://openairdocs.org/sdr/UPS03240133), Jan 20, 2003: SKIN. CRACKED. INSPECTION TYPE:SP CRACK FOUND ON FUSELAGE ABOVE # 1 ENGINE STATION 1183 STRINGER 4L-8L REMOVED PREVIOUS REPAIR DOUBLER AND DAMAGED AREA I.A.W. SRM.53-30-3 FIG. - [SDR UPS01236772](https://openairdocs.org/sdr/UPS01236772), Sep 5, 2001: LIGHT. WILL NOT TEST. INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT AT COCKPIT DOOR WILL NOT TEST. R&R LIGHT ASSY WITH NEW BATTERIES, OPS CHECK K PER MM 33-50-01. - [SDR UPS01236729](https://openairdocs.org/sdr/UPS01236729), Aug 29, 2001: LIGHT. DEFECTIVE. INSPECTION TYPE:IN COCKPIT EMERGENCY LIGHT ILLUMINATED DURING FLIGHT THEN FELL OUT OF ITS CONTAINER. UNABLE TO REINSTALL. REINSTALLED EMERGENCY EXIT LIGHT ASSY - [SDR UPS01235445](https://openairdocs.org/sdr/UPS01235445), Mar 21, 2001: GIRT BAR. INOPERATIVE. INSPECTION TYPE: PREFLT, ESCAPE SLIDE GIRT BAR STOW HOOKS DO NOT HOLD BAR IN PLACE WHEN SLIDE IS DISENGAGED. REMOVED MAIN ENTRY DOOR SLIDE COVER FOR REPAIR. INS - [SDR UPS01235325](https://openairdocs.org/sdr/UPS01235325), Mar 21, 2001: SLIDE. OUT OF POSITION. INSPECTION TYPE IN ESCAPE SLIDE FELL OUT. RE-PACKED EMERGENCY ESCAPE SLIDE. - [SDR UPS01234910](https://openairdocs.org/sdr/UPS01234910), Feb 7, 2001: BATTERY. DISCHARGED. INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS FOUND INOP, PRE-FLT. FOUND BATTERIES WEAK, INSTALLED NEW BATTERIES. OPS CKS NORMAL. - [SDR UPS01234820](https://openairdocs.org/sdr/UPS01234820), Jan 30, 2001: LIGHT. MALFUNCTIONED. INSPECTION TYPE:IN, COCKPIT DOOR EMERGENCY LIGHT VERY DIM. OPS CHECK COCKPIT EMERGENCY LIGHTS WITH BOTH THE SWITCH AT THE ASSY AND THE EMERGENCY LIGHT ARM/DISAR - [SDR UPS01234786](https://openairdocs.org/sdr/UPS01234786), Jan 21, 2001: LIGHT. INOPERATIVE. INSPECTION TYPE:IN, NEITHER EMERGENCY ENT LIGHT WORKING. RESET SWITCH, OPS CHECK IAW MM 33-50-01. OPS CHECK NORMAL. - [SDR UPS01234726](https://openairdocs.org/sdr/UPS01234726), Jan 2, 2001: ANGLE. CRACKED. INSPECTION TYPE:C CK FWD LAV FLOOR INTERCOSTAL ANGLE HAS 2 CRACKS AT STA 320 RIGHT SIDE 20 INCHES FROM RIGHT HAND WALL. INSTALLED DOUBLER REPAIR, ACCOMPLISHED I - [SDR UPS01234728](https://openairdocs.org/sdr/UPS01234728), Dec 31, 2000: STRUCTURE. CRACKED. INSPECTION TYPE:C CK RIGHT WING L/E CAVITY AT STA 330.6, EXISTING REPAIR ANGLE IS CRACKED. REMOVED AND REPLACED REPAIR ANGLE IN ACCORDANCE WITH SRM 51-30-2. - [SDR UPS00234108](https://openairdocs.org/sdr/UPS00234108), Oct 12, 2000: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULBS, OPS OK. A/C OK FOR SERVICE. - [SDR UPS00233409](https://openairdocs.org/sdr/UPS00233409), Jul 21, 2000: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT ABOVE CABIN ENTRANCE DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. - [SDR UPS00231344](https://openairdocs.org/sdr/UPS00231344), Jan 17, 2000: SKIN. DELAMINATED. NLG RT FIXED STRUT DOOR DELAMINATED AT LEADING EDGE. AREA OF DELAMINATION APROX .375 SQ INCH ON LEADING EDGE OF DOOR. REPAIRED PER SRM 51-40-09 PG 25 ITEM TRANS - [SDR UPS00231343](https://openairdocs.org/sdr/UPS00231343), Jan 17, 2000: FLOOR PAN. CRACKED. CRACK AT RT MLG FLOOR PAN STA 910. TRANSFERRED TO DMI D185355 AIRCRAFT TO FERRY TO MIA FOR REPAIR. - [SDR UPS00231342](https://openairdocs.org/sdr/UPS00231342), Jan 17, 2000: WEB. CRACKED. CRACK AT RT MLG WEB BS STA 910. TRANSFER TO DMI D185355 AC TO FERRY TO MIA FOR REPAIR. ALL FERRY FLIGHT PROCEDURES HAVE BEEN ACCOMPLISHED AND A/C IS IN SAFE OPE - [SDR UPS99230982](https://openairdocs.org/sdr/UPS99230982), Oct 23, 1999: FLAP TRACK. CRACKED. INSPECTION TYPE:N/A LH INBD FLAP OUTBD TRACK CRACKED ***MRR FILED AS OPEN*** - [SDR UPS99230015](https://openairdocs.org/sdr/UPS99230015), Jun 28, 1999: SUPPORT. CORRODED. INSPECTION TYPE:C CORROSION UNDER AFT AILERON LOCKOUT GEARBOX ATTACH BOLT (NUTSIDE) ON L/W O/B AILERON LOCKOUT FITTING. REPLACED AILERON LOCKOUT FITTING (SUPPOR - [SDR UPS99229986](https://openairdocs.org/sdr/UPS99229986), Jun 25, 1999: SEAT TRACK. CORRODED. INSPECTION TYPE:C, SEAT TRACK FROM BS 590 TO 605 RBL 25 WL 208 HAS CORROSION IN CHANNEL. AFTER THE CORROSION REMOVAL PROCESS, FOUND THE AREA TO GO BEYOND ALLOWA - [SDR UPS99229982](https://openairdocs.org/sdr/UPS99229982), Jun 24, 1999: SKIN. CORRODED. INSPECTION TYPE:C, CORROSION (C53-113-01.01-01) ON SKIN BS 687 TO 694 LBL 25 JUST ABOVE STR 26 LT SIDE. AFTER REMOVAL OF CORROSION, FOUND THE SKIN TO GO BEYOND - [SDR UPS99229985](https://openairdocs.org/sdr/UPS99229985), Jun 21, 1999: SKIN. CRACKED. INSPECTION TYPE:C, CRACK INDICATED NOTED AROUND 2 FASTENER HEADS AT LT BS 243.7, WL 198.5 AND WL 200. AREAS MARKED IN RED. REMOVED DAMAGED AREA, FABRICATED DOUB - [SDR UPS99230014](https://openairdocs.org/sdr/UPS99230014), Jun 19, 1999: SKIN. CRACKED. INSPECTION TYPE:C CRACK INDICATION NOTED AROUND TWO FASTENER HEADS AT RT BS 235.8 WL 228 AND 229, MARKED IN RED. CUT OUT DAMAGE FABRICATED FILLER AND DOUBLER AN - [SDR UPS99229984](https://openairdocs.org/sdr/UPS99229984), Jun 19, 1999: SKIN. CRACKED. INSPECTION TYPE:C, CRACK INDICATION NOTED AT BS 243.7 WL 229 AROUND FASTENER HEAD MARKED IN RED (RIGHT HAND SIDE. REMOVED DAMAGE, FABRICATED DOUBLER AND INSTALL - [SDR UPS99229983](https://openairdocs.org/sdr/UPS99229983), Jun 18, 1999: CHORD. CORROSION. INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON NOSE MID CHORD BS 349, LBL 15, WL 169. REMOVED CHORD, INSTALLED NEW CHORD. REPLACED WEB WITH FABRICATED WEB, - [SDR UPS00231393](https://openairdocs.org/sdr/UPS00231393), Jan 18, 1999: FRAME. CRACKED. BS 930 FRAME INBOARD AND OUTBOARD FLANGE CRACKED, FROM STRINGER 18A TO MAIN LANDING GEAR PRESSURE DECK. REPLACED BS930 FITTING, RIGHT SIDE IN ACCORDANCE WITH BO - [SDR UPS98226478](https://openairdocs.org/sdr/UPS98226478), Apr 23, 1998: BATTERY. DISCHARGED. INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS LIGHTS, COCKPIT FWD ENTRY DOOR INOP. REMOVED AND REPLACED BOTH SETS OF BATTERIES OUT OF THE EMERGENCY EXIT LIGHT UNIT - [SDR UPS98226476](https://openairdocs.org/sdr/UPS98226476), Apr 23, 1998: LIGHT. INOPERATIVE. INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT ABOVE STAIR TO COCKPIT INOP (UPPER DECK). REMOVED AND REPLACED COCKPIT STAIR EMERGENCY LIGHT, OPS CHECK GOOD (P/N 5135 - [SDR UPS96221745](https://openairdocs.org/sdr/UPS96221745), Dec 12, 1996: SLAT ACTUATOR. INOPERATIVE. INSPECTION TYPE-N/A, NR 2 SLAT WOULD NOT RETRACT AFTER T/O. COMPLETED AOM PROCEDURES, DUMPED FUEL AND RETURNED TO OAK. REPLACED NR 2 SLAT ACT AS PER MM 27-81-32 - [SDR UPS96221470](https://openairdocs.org/sdr/UPS96221470), Oct 25, 1996: BATTERIES. DISCHARGED. INSPECTION TYPE N/A, EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES. - [SDR UPS96221055](https://openairdocs.org/sdr/UPS96221055), Sep 5, 1996: BATTERIES. DISCHARGED. INSPECTION TYPE N/A EMERGENCY LIGHT INOP. REPLACED BATTERIES. - [SDR UPS96220572](https://openairdocs.org/sdr/UPS96220572), Jun 29, 1996: FRAME. CRACKED. INSPECTION TYPE SI, RT 870 FORGING SPLICE AT STR 9 HAS 5 CRACKED HOLES AND ONE 2 TO 3 INCH CRACK IN RADIUS OF AFT FLANGE. REPAIRED BS 870 FORGING BY REMOVING DA - [SDR UPS96220571](https://openairdocs.org/sdr/UPS96220571), Jun 29, 1996: FRAME. CRACKED. INSPECTION TYPE SI, LT 870 FORGING STR 9 HAS ONE CRACKED HOLE AND CRACK IN RADIUS ON FWD FLANGE. INSTALLED EXTERNAL DOUBLERS AND REPAIRED IAW EO B727-5310-3057E - [SDR UPS96220576](https://openairdocs.org/sdr/UPS96220576), Jun 28, 1996: FLOOR. CORRODED. INSPECTION TYPE SI, CORROSION ON FLOOR STA 209 TO 231 LBL 6 TO 18 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED FLOOR PANEL - [SDR UPS96220575](https://openairdocs.org/sdr/UPS96220575), Jun 28, 1996: FLOOR BEAM. CORRODED. INSPECTION TYPE SI, CORROSION ON FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE AT NUTCLIP HOLES STA 680 WL 207.5 LBL 5, 29, 33, 35 RBL 4, 37, 59, 60, AREAS MARKED. REM - [SDR UPS96220574](https://openairdocs.org/sdr/UPS96220574), Jun 28, 1996: FLOOR BEAM. CORRODED. INSPECTION TYPE SI, DOUBLE HOLES IN LOWER FLANGE OF THE 1110 FLOOR BEAM LBL 19 RBL 45 WL 201. DURING REMOVAL OF CEILING SUPPORT FOUND FLOOR BEAM TO BE CORRODED - [SDR UPS96220573](https://openairdocs.org/sdr/UPS96220573), Jun 28, 1996: FLOOR BEAM. CORRODED. INSPECTION TYPE SI, CORROSION AT NUTPLATES IN FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE STA 640 WL 207.5 LBL 38 AREAS MARKED. FOUND FLOOR BEAM AT BS 640 LBL 38 TO - [SDR UPS96220535](https://openairdocs.org/sdr/UPS96220535), Jun 27, 1996: FRAME. CORRODED. INSPECTION TYPE SI, FOUND CORROSION ON FRAME AT BS 304 WL 175 LBL 44. CLEANED AND REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER EO - [SDR UPS96220539](https://openairdocs.org/sdr/UPS96220539), Jun 26, 1996: EXPANSION LINK. CORRODED. INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 LBL 25 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED EXPANSION L - [SDR UPS96220538](https://openairdocs.org/sdr/UPS96220538), Jun 26, 1996: EXPANSON LINK. CORRODED. INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 850 TO 870 LBL 45 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPLACED EXPANSION L - [SDR UPS96220529](https://openairdocs.org/sdr/UPS96220529), Jun 21, 1996: WEB. CORRODED. INSPECTION TYPE SI, CRACK ON FLOOR WEB STA 480 WL 208 LBL 55 AREA MARKED. WHILE WORKING CRACK FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-10-1. REPAIRED PER - [SDR UPS96220527](https://openairdocs.org/sdr/UPS96220527), Jun 21, 1996: SUPPORT. CORRODED. INSPECTION TYPE SI, CORROSION ON COCKPIT ENTRY SUPPORT STA 304 WL 208 LBL 4,9 RBL 3,8 AREA MARKED. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, FARICATE - [SDR UPS96220525](https://openairdocs.org/sdr/UPS96220525), Jun 21, 1996: STIFFENER. CORRODED. INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 RBL 25 WL 208 IN CENTER CHANNEL AT FWD END. FOUND EXPANSION LINK TO BE OUT OF LIMITS PER SRM 53-1 - [SDR UPS96220547](https://openairdocs.org/sdr/UPS96220547), Jun 20, 1996: CHANNEL. CORRODED. INSPECTION TYPE SI, CORROSION ON HAT CHANNEL FROM BS 300 TO 342, RBL 12, WL 208. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-30-2, 53-10-1, 51-40-4. - [SDR UPS96220546](https://openairdocs.org/sdr/UPS96220546), Jun 20, 1996: SPAR. CORRODED. INSPECTION TYPE SI, CORROSION R/W UPPER REAR SPAR CHORD AT WBL 86 JUST ABOVE NR 3 ENGINE FUEL SHUTOFF VALVE. REPAIRED UPPER REAR SPAR CHORD IAW SB 727-57-0145, - [SDR UPS96220545](https://openairdocs.org/sdr/UPS96220545), Jun 20, 1996: FRAME. CORRODED. INSPECTION TYPE SI, CORROSION ON FRAME CHORD STA 312, RBL 43, WL 178. REMOVED AND REPLACED CHORD IAW SRM 53-10-1, 51-40-3, 51-30-2. - [SDR UPS96220544](https://openairdocs.org/sdr/UPS96220544), Jun 20, 1996: FRAME. CORRODED. INSPECTION TYPE SI, CORROSION ON BS 351 WEB AT RBL 37 AND 47, WL 168 BELOW DOGHOUSE FLOOR. REMOVED DAMAGED WEB SECTION AND INSTALLED NEW SECTION IAW SRM 51-40-2 - [SDR UPS96220543](https://openairdocs.org/sdr/UPS96220543), Jun 20, 1996: STIFFENER. CORRODED. INSPECTION TYPE SI, CORROSION ON DOGHOUSE FLOOR SUPPORT AT BS 351, RBL 20 AND RBL 30, WL 170. REMOVED AND REPLACED STIFFENER/FLOOR SUPPORT IAW SRM 51-30-2, 53-1 - [SDR UPS96220542](https://openairdocs.org/sdr/UPS96220542), Jun 20, 1996: CREASE BEAM. CORRODED. INSPECTION TYPE SI, CORRROSION ON STA 1176 CREASE BEAM FROM LBL 25 TO 55 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. REMOVED CREASE - [SDR UPS96220541](https://openairdocs.org/sdr/UPS96220541), Jun 20, 1996: RIB. CRACKED. INSPECTION TYPE SI, NR 8 SLAT I/B TRACK SUPPORT STRUCTURE O/B RIB IS CRACKED IN 2 PLACES. REMOVED AND REPLACED NR 8 SLAT I/B TRACK SUPPORT FITTINGS AND WEBS PER - [SDR UPS96220540](https://openairdocs.org/sdr/UPS96220540), Jun 20, 1996: INTERCOSTAL. CORRODED. INSPECTION TYPE SI, CORROSION ON BOTTOM OF INTERCOSTAL STA 219.8 TO STA 227 LBL 42 WL 227. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM - [SDR UPS96220534](https://openairdocs.org/sdr/UPS96220534), Jun 20, 1996: FLOOR SUPPORT. CORRODED. INSPECTION TYPE SI, CORROSION ON LAV FLOOR SUPPORT STA 315 WL 208 RBL 17, 20, 24, 27, 30, 39 AREAS MARKED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-1, 5 All 163: https://openairdocs.org/deregistered/N929UP-2006-08-23/reports.md ## Other aircraft with N929UP - [Registered now](https://openairdocs.org/aircraft/N929UP): Boeing 767-300F, S/N 70804 --- 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.