# N942UP: 1966 Boeing 727-22C, registration cancelled 2007-12-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 4, 2007 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Serial number: 19101 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 8, 1990 - Certificate issued: July 16, 1990 - Last registry action: September 19, 2006 - Mode S code: AD1666 - Owner when cancelled: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO) - Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville) - Owner type: Corporation - Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N942UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=942UP - Page: https://openairdocs.org/deregistered/N942UP-2007-12-04 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 727-22C: https://openairdocs.org/model/boeing-727-22c.md ## Service difficulty reports (172, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS07249849](https://openairdocs.org/sdr/UPS07249849), May 23, 2007: BATTERY PACK. INOPERATIVE. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER CABIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHT IAW B727 MM 33-50-67-2. OPS CHECKS N - [SDR UPS06248018](https://openairdocs.org/sdr/UPS06248018), Sep 21, 2006: ACTUATOR. WORN. LED NR 6 DOES NOT RETRACT. THE AMBER LT CAME ON DURING CLIMB TO 310. COULD NOT DUPLICATE FAULT ON GROUND. AS PRECAUTION REPLACED NR 6 L/E SLAT ACTUATOR. OPS CHE - [SDR 2007FA0000197](https://openairdocs.org/sdr/2007FA0000197), Sep 4, 2006: RING. ELONGATED. DURING ROUTINE C-CHECK INSPECTION OF FORWARD DOOR EMERGENCY ESCAPE SLIDE, THE SLIDE BUSTLE LATCH CHAIN WAS FOUND DETACHED FROM THE SPLIT RING. THE SPLIT RING HA - [SDR UPS06247858](https://openairdocs.org/sdr/UPS06247858), Aug 24, 2006: HINGE. CRACKED. INSPECTION TYPE:C CRACK FOUND AFT FASTENER HOLE OF LT O/B AILERON 2ND FROM I/B FIXED W WING HINGE CASTING UPPER O/B FLANGE. REPLACE HINGE ASSY. HINGE ASSY REPLA - [SDR UPS06247849](https://openairdocs.org/sdr/UPS06247849), Aug 18, 2006: FAIRING. CORRODED. INSPECTION TYPE:C BODY FAIRING 3430 HAS AREA OF LIGHT SURFACE CORROSION LWR DOOR CUTOUT FRAME. PLEASE REMOVE ANCHOR NUTS, REMOVE CORROSION, REINSPECT AND RECTIF - [SDR UPS06247815](https://openairdocs.org/sdr/UPS06247815), Aug 15, 2006: BUSHING. CORRODED. INSPECTION TYPE: C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON REPAIR BUSHING IN AFT OB HOLE FITTING REPAIR BUSHING REMOVED IAW SOPM 20-50-03. REPAIR - [SDR UPS06247804](https://openairdocs.org/sdr/UPS06247804), Aug 15, 2006: BRACKET. CRACKED. INSPECTION TYPE:C SUSPECT CRACK IN 870 BULKHEAD O/B OF LT 870 FITTING AT LWR CORNER, CRACK IDENTIFIED ON BRACKET REMOVED BRACKET IAW SRM 51-30-02. NEW BRACKET I - [SDR UPS06247806](https://openairdocs.org/sdr/UPS06247806), Aug 14, 2006: SKIN. SCRATCHED. INSPECTION TYPE:C SCRATCH ON FUSELAGE SKIN BETWEEN BS 1186 AND 1193 S19R. PAINTSTRIP AREA A RE-INSPECT AND RECTIFY AREA PAINT STRIPPED IAW MM 51-20-01. SCRATCH - [SDR UPS06247897](https://openairdocs.org/sdr/UPS06247897), Aug 11, 2006: RING. BROKEN. INSPECTION TYPE-C ON SLIDE LATCH CHAIN AND RING BROKEN ON FWD ENTRY DOOR ESCAPE SLIDE. REPLACE RING AND CHAIN ON FURTHER INVESTIGATION CHAIN FOUND NOT TO BE BRO - [SDR UPS06247831](https://openairdocs.org/sdr/UPS06247831), Aug 11, 2006: SKIN. CRACKED. INSPECTION TYPE-C CRACK ON RT OB FORE FLAP LE AT CUTOUT OB OF IB SEQUENCE CARRIAGE ATTACH BRACKET DAMAGE OUTSIDE LIMITS IAW SRM 57-50-1. CRACK STOP DRILLED IAW - [SDR UPS06247830](https://openairdocs.org/sdr/UPS06247830), Aug 10, 2006: SUPPORT. CRACKED. INSPECTION TYPE-C ENGINE NR 2 SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL HAS SUSPECT CRACK ON RT CHORD BETWEEN AFT CONE BOLT HOUSING AND REAR SPAR AT 2 FOOT FR - [SDR UPS06247823](https://openairdocs.org/sdr/UPS06247823), Aug 9, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE-C CORROSION AT BS 344 OUTSIDE LIMITS, PLEASE REPAIR IAW SRM FLOORBEAM TOP CHORD REMOVED IAW SRM 51-30-02. SPLICE ANGLES AND TOP CHORD FABRICATED - [SDR UPS06247745](https://openairdocs.org/sdr/UPS06247745), Aug 9, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE: C, ON REMOVAL OF FLOOR PANEL AT ENTRANCE TO COCKPIT. CORROSION FOUND ON FLOORBEAM TOP CAP BS 344 LBL 10 TO RBL 12. AREA FOUND TO BE OUTSIDE LIM - [SDR UPS06247721](https://openairdocs.org/sdr/UPS06247721), Aug 8, 2006: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C SUSPECT CRACK ON NLG SIDE WALL AT WL 184 BS 276. CRACK REPAIRED IAW SRM 51-40-02. - [SDR UPS06247746](https://openairdocs.org/sdr/UPS06247746), Jul 26, 2006: PRESSURE PANEL. CRACKED. INSPECTION TYPE: C, DURING PRESSURIZATION CHECK LEAK WAS FOUND IN NOSE WW PRESSURE DECK CE CEILING. WEB CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-02, - [SDR UPS06246886](https://openairdocs.org/sdr/UPS06246886), May 17, 2006: LIGHT. INOPERATIVE. INSPECTION TYPE:ASE FLIGHT STAT EMERGENCY LIGHT INOP. REMOVED & REPLACED EMERGENCY EXIT LIGHT ASSY IAW 33-50-01-2. OPS CHECK GOOD. - [SDR UPS06247805](https://openairdocs.org/sdr/UPS06247805), May 8, 2006: BRACKET. CRACKED. INSPECTION TYPE:C SUSPECT CRACK IN 870 BULKHEAD O/B OF RT 870 FITTING AT LWR CORNER. CRACK IDENTIFIED ON BRACKET, REMOVED BRACKET IAW SRM 51-30-02. NEW BR BRACK - [SDR UPS05244165](https://openairdocs.org/sdr/UPS05244165), Mar 15, 2005: SKIN. CORRODED. INSPECTION TYPE:C AREAS OF LITE SURFACE CORROSION FOUND ON INNER FUSELAGE SKIN SURFACE OF LWR SURFACE OF INTERNAL DOUBLER BETWEEN S3L & S2L BS 630 TO 660 AT VAR - [SDR UPS05244169](https://openairdocs.org/sdr/UPS05244169), Mar 11, 2005: FITTING. CRACKED. INSPECTION TYPE:C EXTENSIVE CRACKING SROUND BOTH I/B B & C HOLES FOR A LARGE AREA OF THE RT TRUNNION FITTING ON RT REAR SPAR. REMOVED MLG FWD TRUNNION HOUSING A - [SDR UPS05244134](https://openairdocs.org/sdr/UPS05244134), Mar 11, 2005: BRACKET. CRACKED. INSPECTION TYPE:C ENGINE NR 1 THRUST REVERSER O/B FAIRING MID AND AFT SUPPORT BRACKET ARE CRACKED. BRACKETS REPLACED IAW MM 78-30-01. - [SDR UPS05244172](https://openairdocs.org/sdr/UPS05244172), Mar 10, 2005: FITTING. CORRODED. INSPECTION TYPE:C NR 5 FLAP TRACK FWD SUPPORT FITTING P/N 65-21651 HAS PITTING CORROSION ON HOLE FOR SPECIAL STUD. REPAIR CARRIED OUT IAW AAAE EO 2005-021-003. - [SDR UPS05244166](https://openairdocs.org/sdr/UPS05244166), Mar 10, 2005: CARGO TRACK. CRACKED. INSPECTION TYPE:C CARGO TIE DOWN TRACK CRACKED AT BS 1030 RBL 14. REPAIR CARRIED OUT IAW SRM 53-10-5, 51-30-2, 51-20-1 & 53-10-5. - [SDR UPS05244146](https://openairdocs.org/sdr/UPS05244146), Mar 10, 2005: FLOOR SUPPORT. CRACKED. INSPECTION TYPE:C FLOOR SUPPORT CRACKED AT BS 1070 LBL 14. REPLACED FLOOR SUPPORT FROM 1100 - 1060 IAW SRM 53-10-5 FIG 4. - [SDR UPS05244167](https://openairdocs.org/sdr/UPS05244167), Mar 9, 2005: SKIN. CRACKED. INSPECTION TYPE: C FWD CARGO DOOR CRACKED AT AFT UPPER FRAME BETWEEN LWR ATTACH BOLT FOR BALANCE MECHANISM. REPAIR CARRIED OUT IAW AAAE EO 2005-021-002. - [SDR UPS05244154](https://openairdocs.org/sdr/UPS05244154), Mar 9, 2005: SPINDLE. CORRODED. INSPECTION TYPE:C SURFACE CORROSION ON 4 FLAP CARRIAGE SPINDLE INNER SURFACE. CORROSION REMOVED IAW SRM 51-00-06, WITHIN LIMITS OHM 57-52-01. AREA PROTECTED IAW - [SDR UPS05244151](https://openairdocs.org/sdr/UPS05244151), Mar 9, 2005: CHANNEL. CRACKED. INSPECTION TYPE:C UPPER SUPPORT CHANNEL FOR EQUIPMENT RACK CRACKED AT BS 420 AND 460 RBL 22. REPAIRED CRACKED UPPER SUPPORT CHANNEL IAW SRM 51-90-3 AT BS 420 TO - [SDR UPS05244148](https://openairdocs.org/sdr/UPS05244148), Mar 9, 2005: CHANNEL. CRACKED. INSPECTION TYPE:C UPPER SUPPORT CHANNEL FOR EQUIP RACK CRACKED AT BS 400 BS 420 AND BS 460 LBL 17. REPAIRED CRACKS ON UPPER SUPPORT CHANNEL AT BS 400, 420, 460 - [SDR UPS05244170](https://openairdocs.org/sdr/UPS05244170), Mar 8, 2005: TAB. DELAMINATED. INSPECTION TYPE:C EVIDENCE OF DELAMINATION TO RT ELEVATOR TAB UPPER INBOARD SURFACE. TAB REPLACED IAW MM 27-30-11 & 27-30-00. - [SDR UPS05244168](https://openairdocs.org/sdr/UPS05244168), Mar 8, 2005: PANEL. DELAMINATED. INSPECTION TYPE:C DELAMINATION ON NR 8 SPOILER AT I/B END. NR 8 SPOILER PANEL REPLACED IAW MM 27-62-01 AND SPOILER LINK REPLACED IAW MM 27-62-91. - [SDR UPS05244135](https://openairdocs.org/sdr/UPS05244135), Mar 8, 2005: FRAME. CRACKED. INSPECTION TYPE:C AFT CARGO DOOR, CRACKED IN 1ST FRAME FROM TOP IN O/B RADIUS BENEATH FWD HINGE. REPAIR CARRIED OUT IAW MM 52-31-01 & SRM 51-10-01, 51-40-3, 51- - [SDR UPS05243938](https://openairdocs.org/sdr/UPS05243938), Feb 22, 2005: LIFE RAFT. MALFUNCTIONED. LIFE RAFT LOCATED AFT OF LAV EXPERIENCED AN UNCOMMANDED INFLATION. NO DAMAGE TO THE A/C WAS NOTICED. A/C NOW IN HEAVY MAINTENANCE IN SNN. INSTALLED SERVICEABLE - [SDR UPS04241937](https://openairdocs.org/sdr/UPS04241937), Feb 6, 2004: SKIN. DAMAGED. INSPECTION TYPE:C PARTIAL REPLACEMENT OF SKIN LOCATED AT BS 360-390 S4L-4R. REPLACED IAW UPS AUTHORIZATION B727-5330-19967-A. - [SDR UPS04241932](https://openairdocs.org/sdr/UPS04241932), Feb 4, 2004: RIB. CRACKED. INSPECTION TYPE:C ON REMOVAL OF PANEL 8855 FOUND NR 14 O/B SPOILER DOWN STOP RIB CRACKED AT WS 620.5. CRACKED RIB REPLACED IAW SRM 51-30-2 & SPOILER OPERATION W - [SDR UPS04241875](https://openairdocs.org/sdr/UPS04241875), Feb 2, 2004: BRACKET. CRACKED. INSPECTION TYPE: C, BATTERY CHARGER FWD MOUNTING BRACKET CRACKED ON E3 RACK LOWER RT SIDE. REMOVED CRACKED BRACKET IAW SRM 51-30-02. FABRICATED NEW BRACKET IAW - [SDR UPS04241872](https://openairdocs.org/sdr/UPS04241872), Jan 30, 2004: BRACKET. DAMAGED. INSPECTION TYPE: C, LATCH FITTING ON W/BODY FAIRING BRACKET FOR AFT CARGO DOOR FAIRING LATCH IS DAMAGED. BRACKET REPLACED IAW SRM 51-20-01. - [SDR UPS04241876](https://openairdocs.org/sdr/UPS04241876), Jan 25, 2004: BRACKET. CORRODED. INSPECTION TYPE: C, SUSPECT CORROSION WHERE 259.5 RT STIFFENER AND TOP LEFT HAND CORNER OF NWW TORQUE BOX MEET BRACKET. REMOVED IAW SRM 51-30-02. BRACKET FABRIC - [SDR UPS04241898](https://openairdocs.org/sdr/UPS04241898), Jan 23, 2004: WEB. CRACKED. INSPECTION TYPE: C, AFT STAIRWELL RT TORQUE BOX VERTICAL WEB HAS CRACKING BEYOND PREVIOUS REPAIR AT BS 1273. REPAIR CARRIED OUT IAW EO B727-5310-1239-E & MM 20- - [SDR UPS04241873](https://openairdocs.org/sdr/UPS04241873), Jan 23, 2004: HINGE. CRACKED. INSPECTION TYPE: C, LEFT WING GEAR DOOR AFT HINGE, INNER HINGE HALF CRACKED. REPLACED HINGE IAW SRM 51-30-02. - [SDR UPS04241940](https://openairdocs.org/sdr/UPS04241940), Jan 22, 2004: BEAM. CORRODED. INSPECTION TYPE:C PRESENCE OF INTERGRANULAR CORROSION FOUND ON VARIOUS HOLES AND THE LOWER I-BEAM AT BS 1110 RBL 31 AS MARKED. REPAIRED IAW UPS AUTHORIZATION B7 - [SDR UPS04241933](https://openairdocs.org/sdr/UPS04241933), Jan 22, 2004: SUPPORT FITTING. DAMAGED. INSPECTION TYPE:C REPAIR PLATES ON NR 3 SPOILER PCU SUPPORT FITTING, REAR SPAR ATTACH ANGLES DO NOT CONFORM TO REQUIREMENTS OF SRM REPAIR 51-40-4 FIG 1 OR S/B 5 - [SDR UPS04241816](https://openairdocs.org/sdr/UPS04241816), Jan 22, 2004: BRACKET. CORRODED. INSPECTION TYPE: C, INTERGRANULAR CORROSION FOUND ON CEILING PANEL BRACKET AT BS 1130 AFT CARGO COMPT, AS MARKED. HFEC INSPECTION CARRIED OUT AROUND CUTOUT AT T - [SDR UPS04241939](https://openairdocs.org/sdr/UPS04241939), Jan 21, 2004: FITTING. CRACKED. INSPECTION TYPE:C RIGHT MLG WHEEL WELL, EVIDENCE OF CORROSION ON BS 870 FITTING O/B FLANGE AREA ABOVE STR 18A. FITTING REPLACED IAW DWG65C23231 AND 2BOF65-72710 - [SDR UPS04241874](https://openairdocs.org/sdr/UPS04241874), Jan 21, 2004: SOLENOID VALVE. STICKING. INSPECTION TYPE: C, ENGINE NR 1 FIRE EXTINGUISHING SOLENOID STICKS DURING OPERATION. ENGINE NR 1 FIRE SOLENOID VALVE REPLACED IAW MM 26-21-21. TEST AND FOUND SA - [SDR UPS02238739](https://openairdocs.org/sdr/UPS02238739), Jul 8, 2002: CARRIAGE. CORRODED. INSPECTION TYPE:C+SI FLAP CARRIAGE NR 1 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. REMOVAL OF HARDWARE CORROSION FOUND ON SPINDLE SMALL BEARING SEAT. CORROSION - [SDR UPS02238849](https://openairdocs.org/sdr/UPS02238849), Jul 1, 2002: FITTING. CRACKED. INSPECTION TYPE:C+SI DURING RECTIFICATION UPPER LT AFT TENSION TIE FITTING FOUND CRACKED IN TAIL SKID UNIT CAVITY. UPPER LT TENSION TIE REMOVED IAW SRM 51-30-02 - [SDR UPS02238844](https://openairdocs.org/sdr/UPS02238844), Jun 27, 2002: DOOR FRAME. CRACKED. INSPECTION TYPE:C+SI SUSPECT CRACKS ON 2 FRAMES AND FRAME ATTACH ANGLES ON OUTER FACE OF AFT CARGO DOOR. FRAMES AND ANGLES REPLACED IAW DWG 65-18625, LOWER FRAM - [SDR UPS02238804](https://openairdocs.org/sdr/UPS02238804), Jun 21, 2002: STRINGER. CRACKED. INSPECTION TYPE:C+SI STR NO8 L/H HAS EVIDENCE OF CRACKING ON ROOT OF INSIDE LOWER FLANGE AT BS 460 REPAIR CARRIED OUT IAW SRM 53-10-3 FIGURE 3. - [SDR UPS02238786](https://openairdocs.org/sdr/UPS02238786), Jun 21, 2002: HINGE. CORRODED. INSPECTION TYPE:C+SI SEVERAL MAIN HINGES CORRODED ON MAIN CARGO DOOR. HINGES REPLACED IAW OHM 20-50-01. - [SDR UPS02238851](https://openairdocs.org/sdr/UPS02238851), Jun 20, 2002: INTERCOSTAL. CRACKED. INSPECTION TYPE:C+SI BS 950 LBL 6 ANGLE CRACKED AT FLOOR BEAM INTERCOSTEL. NEW ANGLE FABRICATED IAW SRM 51-20-1 FIG.7 ANGLE INSTALLED IAW SRM 51-30-2. - [SDR UPS02238830](https://openairdocs.org/sdr/UPS02238830), Jun 20, 2002: DOUBLER. CORRODED. INSPECTION TYPE:C+SI BULGING ON EXTERNAL DOUBLER ATTACHED TO DELTA BEAM BS 747 Y/H DOUBLER REMOVED IAW SRM 51-30-2, CORROSION FOUND ON UDERSIDE OF DOUB LER, DEL All 172: https://openairdocs.org/deregistered/N942UP-2007-12-04/reports.md ## Other aircraft with N942UP - [Registered now](https://openairdocs.org/aircraft/N942UP): Bombardier BD-100-1A10, S/N 20375, built 2012 --- 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.