# N919UP: 1967 Boeing 727-30C, 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 727-30C](https://openairdocs.org/model/boeing-727-30c) (registry code 1384009) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Serial number: 19012 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: None - Airworthiness: Standard, transport - Airworthiness date: May 31, 1979 - Certificate issued: September 7, 1982 - Last registry action: September 19, 2006 - Mode S code: ACB9EA - 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/N919UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=919UP - Page: https://openairdocs.org/deregistered/N919UP-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 727-30C: https://openairdocs.org/model/boeing-727-30c.md ## Service difficulty reports (92, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS07248886](https://openairdocs.org/sdr/UPS07248886), Jan 19, 2007: SLIDE. DISLODGED. FWD ENTRY ESCAPE SLIDE IS OUT OF CONTAINER. INSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE IAW 25-60-14-2. OPS CHECK GOOD. - [SDR UPS06248684](https://openairdocs.org/sdr/UPS06248684), Nov 14, 2006: SKIN. CRACKED. 3 INCH CRACK ON FUSELAGE SKIN AT 10 O'CLOCK POSITION RUNNING FWD AND AFT AT STA 348.2, BETWEEN STRINGERS 5L & 6L. ADDITIONAL DISBONDING APPROXIMATELY 4 X 4 INCH - [SDR UPS06248513](https://openairdocs.org/sdr/UPS06248513), Nov 7, 2006: SLIDE. DISLODGED. FOUND DOOR SLIDE ON FLOOR. RE-INSTALLED ESCAPE SLIDE PER 25-60-14-2. - [SDR UPS06248330](https://openairdocs.org/sdr/UPS06248330), Oct 26, 2006: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHTS ABOVE THE MAIN ENTRY DOOR AND ABOVE THE COCKPIT ENTRY DOOR ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY ON MAIN ENTRY DOOR PER - [SDR UPS06247827](https://openairdocs.org/sdr/UPS06247827), Aug 28, 2006: SLIDE. DISLODGED. INSPECTION TYPE: NA ESCAPE SLIDE FELL OUT OF CASE ON MAIN ENTRY DOOR REPLACED ENTRY DOOR EVACUATION SLIDE IAW MM 25-60-14-2. - [SDR UPS06247717](https://openairdocs.org/sdr/UPS06247717), Aug 17, 2006: BATTERY. INOPERATIVE. INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPS CK NORMAL. - [SDR UPS06247529](https://openairdocs.org/sdr/UPS06247529), Jul 31, 2006: BATTERY. DISCHARGED. FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AS REQUIRED. - [SDR UPS06246808](https://openairdocs.org/sdr/UPS06246808), May 8, 2006: FAIRING. DELAMINATED. DELAM ON L/AFT WING TO BODY FAIRING PANEL NR 3510 JUST AFT OF HYD SYS BAY REF EO B727-5350-24306. PERFORMED INTERIM REPAIR PER EO B727-5350-24306 STEP 6. DEFERR - [SDR UPS05245266](https://openairdocs.org/sdr/UPS05245266), Aug 6, 2005: SKIN. CORRODED. INSPECTION TYPE: C, NR 2 ENG UPPER HORIZ FIREWALL SURFACE TO VERT FIN, LT, ANGLE HAS EVIDENCE OF CORROSION ON INNER SURFACE OF VERT FIN SKIN BETWEEN STA 1385 AN - [SDR UPS05245265](https://openairdocs.org/sdr/UPS05245265), Aug 5, 2005: STIFFENER. CORRODED. LT MLG W/W, EVIDENCE OF CORROSION ON BS 870 VERTICAL STIFFENER AND ATTACH CLIP AT LB 145. CEILING AREA. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-10-2, 51-10-1. - [SDR UPS05245262](https://openairdocs.org/sdr/UPS05245262), Aug 4, 2005: STIFFENER. CORRODED. RT MLG W/W, EVIDENCE OF CORROSION ON VERTICAL STIFFENER CEILING AREA BS 870 RBL 45. REPAIR CARRIED OUT IAW SRM 51-40-4. - [SDR UPS05245263](https://openairdocs.org/sdr/UPS05245263), Aug 3, 2005: FLOORBEAM. CORRODED. FLOORBEAM TOP CHORD CORROSION OUTSIDE LIMITS BS 328 RBL 12. REPAIR CARRIED OUT IAW SRM 53-10-8 & 51-10-2. - [SDR UPS05245207](https://openairdocs.org/sdr/UPS05245207), Aug 3, 2005: INTERCOSTAL. CORRODED. INSPECTION TYPE:C, CORROSION ON INTERCOSTAL BS 294.5 - BS 312 LBL 33. INTERCOSTAL REPLACED IAW BOEING DWG 65-17593 AND SRM 51-30-02. - [SDR UPS05245205](https://openairdocs.org/sdr/UPS05245205), Aug 2, 2005: SUPPORT. CORRODED. INSPECTION TYPE:C FWD LAV PARTITION SUPPORT STRUCTURAL EXTRUSION CORRODED BS 302 - 344 DOOR THRESHOLD AREA. PARTITION SUPPORT STRUCTURE EXTRUSION REPLACED IAW S - [SDR UPS05245261](https://openairdocs.org/sdr/UPS05245261), Aug 1, 2005: SKIN. CORRODED. AREA OF CORROSION ON SKIN BS 355, BETWEEN STR 8 AND 10 LT. PAINT STRIP AREA IF REQUIRED, REMOVE CORROSION AND RECTIFY. REPAIR CARRIED OUT IAW SRM 51-10-1, 53-30 - [SDR UPS05245264](https://openairdocs.org/sdr/UPS05245264), Jul 31, 2005: ATTACH ANGLE. CORRODED. RT SIDE AFT OF BS 294.5 FWD ATTACHMENT ANGLE OF NWW BOX HAS EVIDENCE OF CORROSION. WEB REPAIRED IAW SRM 51-40-2. - [SDR UPS05245206](https://openairdocs.org/sdr/UPS05245206), Jul 31, 2005: WEB. CORRODED. INSPECTION TYPE:C RT SIDE AFT OF RT 294.5 FWD ATTACHMENT ANGLE OF NWW BOX AND RT HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 & 51-40- - [SDR UPS05243629](https://openairdocs.org/sdr/UPS05243629), Jan 6, 2005: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY LIGHT INOP. RESEATED BULB, OPS CHECK GOOD. - [SDR UPS04242069](https://openairdocs.org/sdr/UPS04242069), Mar 17, 2004: FITTING. CRACKED. INSPECTION TYPE:C ON REMOVAL OF STR END FITTING AT BS 360 S17L FOUND STR END FITTING CRACKED & CORRODED. REPLACED STR END FITTING IAW SRM 51-30-02 & DRAWING 65- - [SDR UPS04242070](https://openairdocs.org/sdr/UPS04242070), Mar 12, 2004: FITTING. CRACKED. INSPECTION TYPE:C ON REMOVAL OF LOWER SKIN BETWEEN BS 259.5 - BS 360 S22 24L STRINGER END FITTING FOUND CRACKED AT BS 360 S22L. REPLACED STRINGER END FITTING IA - [SDR UPS04242058](https://openairdocs.org/sdr/UPS04242058), Mar 11, 2004: STRINGER. CORRODED. INSPECTION TYPE: C, ON REMOVAL OF FASTENER AT BS 340 APPROX S25R STRINGER FOUND TO BE CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-3. - [SDR UPS04242073](https://openairdocs.org/sdr/UPS04242073), Mar 10, 2004: SKIN. CORRODED. INSPECTION TYPE:C ON REMOVAL OF SKIN PANEL AT BS 295.5 & BS 360 S19L - 24L UPPER SKIN UNDER FWD ENTRY DOOR FOUND TO BE EXCESSIVELY CORRODED. REPAIR CARRIED OUT - [SDR UPS04242072](https://openairdocs.org/sdr/UPS04242072), Mar 9, 2004: DOOR FRAME. CORRODED. INSPECTION TYPE:C TAIL SKID DOOR RIGHT LWR FRAME IS CORRODED ON INNER SURFACE. REPLACED TAIL SKID DOOR IAW MM 32-71-61. - [SDR UPS04242060](https://openairdocs.org/sdr/UPS04242060), Mar 9, 2004: CARGO TRACK. CRACKED. INSPECTION TYPE: C, LEFT CARGO TRACK RAIL IN AFT CARGO BAY, VERY FWD SECTION TO BS 950 IS CRACKED. REF CPT 2643 FOR FABRICATION OF CARGO TRACK. REPAIRED CARGO T - [SDR UPS04242075](https://openairdocs.org/sdr/UPS04242075), Mar 8, 2004: SUPPORT. CORRODED. INSPECTION TYPE:C NR 12 SPOILER ACTUATOR SUPPORT CASTING HAS PITTING AND CORROSION UNDERNEATH THE BOLT HEADS. NR 12 SPOILER ACTUATOR SUPPORT CASTING REPLACED IA - [SDR UPS04242059](https://openairdocs.org/sdr/UPS04242059), Mar 5, 2004: MOUNT. CORRODED. INSPECTION TYPE: C, ENGINE NR 1 PYLON FWD MOUNT FITTING, BOTH FWD AFT LARGE AND AFT SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-1159 - [SDR UPS04242057](https://openairdocs.org/sdr/UPS04242057), Mar 5, 2004: MOUNT. CORRODED. INSPECTION TYPE: C, ENGINE NR 3 PYLON FWD MOUNT FITTING, BOTH FWD AND AFT LARGE AND FWD SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440- - [SDR UPS04242056](https://openairdocs.org/sdr/UPS04242056), Mar 4, 2004: SKIN. BULGED. INSPECTION TYPE:C SUSPECT CORROSION (SKIN BULGING) BETWEEN SKIN & FRAME AT BS 260 FROM STR 18L - S19L. REF N/R 740347, LOW FREQ EDDY CURRENT INSP CARRIED OUT AT - [SDR UPS03240251](https://openairdocs.org/sdr/UPS03240251), Mar 4, 2003: TORQUE TUBE. LOOSE. INSPECTION TYPE:N/A ATB-AFTER T/O, LG RAISED AND RIGHT MAIN GEAR STAYED DOWN. RED GEAR LIGHT AND DOORS LIGHT REMAINED ON. GEAR CAME DOWN NORMALLY. REPLACED 6 EA - [SDR UPS02239549](https://openairdocs.org/sdr/UPS02239549), Sep 30, 2002: BATTERY. DISCHARGED. COCKPIT EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERIES, OPS CHECKS GOOD, BATTERIES IAW MM 33-50-01. - [SDR UPS02239530](https://openairdocs.org/sdr/UPS02239530), Sep 20, 2002: CONTACTOR. DIRTY. EMERGENCY EXIT LIGHTS INOP. REMOVED LIGHT ASSY OVER CREW CABIN DOOR, CLEANED CONTACTS, OPS CK OK IAW MM 33-50-01. - [SDR UPS02238920](https://openairdocs.org/sdr/UPS02238920), Jul 29, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT L1 DOOR. REPLACED BATTERIES, OPS CHECK GOOD. - [SDR UPS02238919](https://openairdocs.org/sdr/UPS02238919), Jul 29, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT COCKPIT. REPLACED BATTERIES, OPS CHECK GOOD. - [SDR UPS02238737](https://openairdocs.org/sdr/UPS02238737), Jul 2, 2002: LIGHT. NOT SEATED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE CABIN DOOR INOP. SEATED EXIT LIGHT ASSY OPS CHECKS GOOD - [SDR UPS02238641](https://openairdocs.org/sdr/UPS02238641), Jun 17, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:PFLT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM 33-50-01. - [SDR UPS02237755](https://openairdocs.org/sdr/UPS02237755), Mar 3, 2002: LIGHT. INOPERATIVE. INSPECTION TYPE:IN FWD EXIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. OP CHECK GOOD IAW MM 33-50-01. - [SDR UPS02237516](https://openairdocs.org/sdr/UPS02237516), Jan 24, 2002: COVER. LOOSE. INSPECTION TYPE:PFLT CABIN EXIT LIGHT COVER OVER CABIN DOOR IS LOOSE. CHECK SECURITY OF EXIT LIGHT ASSY PER MAINT PRACTICES MM 33-50-01 AND INSTALLED LIGHT COVE - [SDR UPS02237439](https://openairdocs.org/sdr/UPS02237439), Jan 20, 2002: LIGHT. NOT SEATED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IS DIM, RESEATED LIGHT ASSY. OPS CHECKS GOOD PER MM 33-50-101. - [SDR UPS01236604](https://openairdocs.org/sdr/UPS01236604), Aug 5, 2001: FAIRING. CRACKED. INSPECTION TYPE:PFLT LT INBD FLAP LT OUTBD CANOE FIXED FAIRING HAS A CRACK ON AFT UPPER CORNER OF PREVIOUS REPAIR. DEFFERRED PER MMOC - [SDR UPS01236163](https://openairdocs.org/sdr/UPS01236163), Jun 22, 2001: ACTUATOR. LEAKING. INSPECTION TYPE:N/A RIGHT MAIN GEAR DOOR OPENED ENROUTE GEAR HANDLE PLACED TO "UP" POSIT ION DOOR CLOSED GEAR HANDLE RETURNED TO "OFF" POSITION OPS NORMAL ****S - [SDR UPS01235279](https://openairdocs.org/sdr/UPS01235279), Mar 5, 2001: FRAME. CRACKED. INSPECTION TYPE:C-CK, CRACK AT FUSELAGE FRAME BS 930 ABOVE STR 13L. CUT OUT DAMAGE SECTION OF FRAME BETWEEN STR 12L & 13L. INSTALLED FORMED ANGLE REPAIR, HEAT T - [SDR UPS01235278](https://openairdocs.org/sdr/UPS01235278), Feb 28, 2001: STRINGER. CORRODED. INSPECTION TYPE:C-CK, STRINGER 18 LEFT CORRODED BETWEEN BS 440 TO BS 460. REMOVED CORROSION ON STRINGER FLANGE. FOUND OUT OF UNIT. INSTALLED STRINGER REPAIR. - [SDR UPS01235402](https://openairdocs.org/sdr/UPS01235402), Feb 26, 2001: FITTING. CRACKED. INSPECTION TYPE:C CHECK LT WING FRONT SPAR INTERIOR & LBBL 70.5 TERMINAL FITTING ATTACH V SHAPE FITTING TO UPPER SHOW CRACK MIGRATING FROM OB BOLT. REMOVED FITT - [SDR UPS01235399](https://openairdocs.org/sdr/UPS01235399), Feb 19, 2001: DUCT. CRACKED. INSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS. 1 EA 4 INCH CRACK 93 INCHES FROM AFT EDGE 4 OCLOCK. CUT OUT DAMAGED AREA - [SDR UPS01235398](https://openairdocs.org/sdr/UPS01235398), Feb 19, 2001: DUCT. CRACKED. INSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS 2 EA APPX 100-104 INCH FROM AFT EDGE. 1 EA 7 INCH Y SHAPED CRACK & 1 EA 1 - [SDR UPS01235284](https://openairdocs.org/sdr/UPS01235284), Feb 19, 2001: INTAKE DUCT. CRACKED. INSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 6 INCH CIRCUMFERENTIAL CRACK AT 4 O''CLK APPROX 30 INCHES AFT OF WHERE S-DUCT ATTACHES TO INLE - [SDR UPS01235283](https://openairdocs.org/sdr/UPS01235283), Feb 19, 2001: SKIN. CRACKED. INSPECTION TYPE:C-CK, FUSELAGE SKIN HAS CORROSION BULGE AND APPROX 3 INCH LATERAL CRACK. REMOVED FASTENERS, REMOVED CORROSION. NDT INSP C/W CUT DAMAGE AREA AND - [SDR UPS01235282](https://openairdocs.org/sdr/UPS01235282), Feb 19, 2001: SKIN. CORRODED. INSPECTION TYPE:C-CK, LOW FREQ EDDY CURRENT INSP OF SKIN AT BS 441 BETWEEN STRG 18R & 19R HAS INDICATION OF CORROSION LOSS GREATER THAN 10 PERCENT. REMOVED EQUI - [SDR UPS01235221](https://openairdocs.org/sdr/UPS01235221), Feb 19, 2001: DUCT. CRACKED. INSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 3 INCH CIRCUMFERENTIAL CRACK APPROX 104 INCHES FROM AFT EDGE AT 3 O''CLOCK. CUT OUT DAMAGE ARE - [SDR UPS01235401](https://openairdocs.org/sdr/UPS01235401), Feb 18, 2001: LAP JOINT. BULGED. INSPECTION TYPE:C CK LAP JOINT 19RT HAS SKIN BULGE AT BS 620. CUT OUT DAMAGED SKIN LWR & UPPER AREA. INSTALLED REPAIR PART AT LAP JOINT STR 19 BS 620. All 92: https://openairdocs.org/deregistered/N919UP-2007-12-04/reports.md ## Other aircraft with N919UP - [Registered now](https://openairdocs.org/aircraft/N919UP): Boeing 767-300F, S/N 68365, built 2026 --- 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.