# N930UP: 1966 Boeing 727-22C, registration cancelled 2007-11-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 21, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Serial number: 19096
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Experimental, research and development
- Airworthiness date: April 7, 1993
- Certificate issued: October 27, 1982
- Last registry action: September 19, 2006
- Mode S code: ACE779
- Owner when cancelled: [United Parcel Service](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE)
- 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/N930UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=930UP
- Page: https://openairdocs.org/deregistered/N930UP-2007-11-21

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 (175, newest 50)

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

- [SDR UPS06248609](https://openairdocs.org/sdr/UPS06248609), Nov 12, 2006: BATTERY. DISCHARGED. FOUND EMERGENCY EXIT LIGHT OVER ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER MM 35-50-67. OPS CHECK GOOD.
- [SDR UPS06246477](https://openairdocs.org/sdr/UPS06246477), Mar 21, 2006: DOOR. DAMAGED. FOUND LT AC PACK DOOR CAME OFF IN FLIGHT AND DAMAGING FUSELAGE AFT OF PACK. RT DOOR IS HANGING BY AFT HINGE AND IS BEYOND REPAIR.
- [SDR UPS06246446](https://openairdocs.org/sdr/UPS06246446), Mar 15, 2006: WIRE. LOOSE. EMERGENCY EXIT LIGHTS INOP. FOUND BOTTOM C/B PANEL LIGHTING INOP ON LEFT SIDE OF COCKPIT. FOUND POWER WIRE LOOSE. TIGHTENED LOOSE POWER WIRE. OPS CK GOOD.
- [SDR UPS06246517](https://openairdocs.org/sdr/UPS06246517), Mar 14, 2006: BATTERY. INOPERATIVE. ON PREDEPARTURE CK, FOUND EMERGENCY EXIT LIGHT SWITCH IN ON POSITION. REMOVED AND REPLACED BATTERIES IAW MM 33-50-11-2. OPS CKS NORMAL.
- [SDR UPS06246393](https://openairdocs.org/sdr/UPS06246393), Feb 28, 2006: SKIN. DENTED. INSPECTION TYPE:SP REF DMI D-320435, DENT AT FS 1163 AT STR 20R INCOMING MEASUREMENT (APPROX) OF 3.0"DIA X .200 DEEP AND GOUGED 2.0" X .005"DEEP. CUT OUT DAMAGE
- [SDR UPS05245314](https://openairdocs.org/sdr/UPS05245314), Aug 30, 2005: SKIN. CRACKED. SUSPECT SKIN CRACK AT BS 364 STR 3 LT. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 53030-3 FIG 3A.
- [SDR UPS05245313](https://openairdocs.org/sdr/UPS05245313), Aug 29, 2005: CLIP. CRACKED. RT BODY FAIRING 3427 HAS SMALL CRACK AT FWD ATTACHING END CLIP. ATTACHING END CLIP REPLACED IAW SRM 51-20-04.
- [SDR UPS05245312](https://openairdocs.org/sdr/UPS05245312), Aug 29, 2005: FRAME. CORRODED. BODY FAIRING 3608 AFT FRAME AT ATTACHING ANGLE IS CORRODED AT BS 1010 ADJACENT TO STR 26R. FRAME REPLACED IAW SRM 51-20-1 FIG 7.
- [SDR UPS05245357](https://openairdocs.org/sdr/UPS05245357), Aug 25, 2005: SKIN. CRACKED. SUSPECT SKIN CRACK AT UPPER FWD ENTRY DOOR CUT OUT BETWEEN STR 5 AND 6 L. PLEASE CARRY OUT NDI AND RECIFITY. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B727-5330-14
- [SDR UPS05245372](https://openairdocs.org/sdr/UPS05245372), Aug 23, 2005: WEB. CRACKED. INSPECTION TYPE: C, NLG W/W CEILING AT BS 290 LBL 0 HAS SUSPECT CRACKS AT FASTENER HEADS. WEB REPLACED IAW SRM 51-20-1 AND DWG 65-18416.
- [SDR UPS05245356](https://openairdocs.org/sdr/UPS05245356), Aug 23, 2005: DOOR. CORRODED. NLG FWD LT DOOR HAS CORROSION UNDER SEAL AT I/B END. CORRODED SECTION REPLACED WITH FABRICATED SECTION IAW SRM 51-20-1 AND DWG 65-17563.
- [SDR UPS05245317](https://openairdocs.org/sdr/UPS05245317), Aug 22, 2005: STRINGER. CORRODED. AREA OF SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE AT BS 295 STR22R. CORROSION FOUND TO BE ON STRINGER 22R BETWEEN BS 204-316. STRINGER SECTION REPLA
- [SDR UPS05245316](https://openairdocs.org/sdr/UPS05245316), Aug 22, 2005: SKIN. SCRATCHED. LIGHT SURFACE SCRATCHES FOUND ON SKIN AT BS 1263 BETWEEN S5L AND 6L. DAMAGED AREA FOUND OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13.
- [SDR UPS04243231](https://openairdocs.org/sdr/UPS04243231), Sep 29, 2004: PANEL. DELAMINATED. INSPECTION TYPE:N/A NR 8 GROUND SPOILER CENTER HINGE BOTTOM S/M PANEL DELAMINATED. REMOVED AND REPLACED NR 8 GROUND SPOILER PER MM 27-62-01. OPS CHECK NORMAL.
- [SDR UPS04242321](https://openairdocs.org/sdr/UPS04242321), Apr 27, 2004: SUPPORT. CRACKED. INSPECTION TYPE:C CRACK ON SUPPORT STRUCTURE IN NWW RT FWD AREA. SUPPORT STRUCTURE REMOVED REF NRC NR 748078, SUPPORT STRUCTURE FABRICATE D IAW SRM 51-20-1, SUP
- [SDR UPS04242344](https://openairdocs.org/sdr/UPS04242344), Apr 26, 2004: FRAME. CRACKED. INSPECTION TYPE: C, VERT STAB JACKSCREW CUTOUT LT, FWD FRAME CRACKED AT FW STA 128 APPROX. CRACKED FRAME REMOVED IAW SRM 51-30-02. NEW FRAME INSTALLED IAW SRM 5
- [SDR UPS04242316](https://openairdocs.org/sdr/UPS04242316), Apr 26, 2004: PULLEY BRACKET. CRACKED. INSPECTION TYPE:C SUSPECT CRACKS ON RUDDER TRIM CABLE PULLEY BRACKET IN AIRSTAIRS AREA BS 1203 RT HFEC C/W, DERIVETED BRACKET, FAB BRACKET IAW SRM 51-20-01, BRA
- [SDR UPS04242343](https://openairdocs.org/sdr/UPS04242343), Apr 24, 2004: SKIN. CRACKED. INSPECTION TYPE: C, ENGINE NR 1 THRUST REV. UPPER DOOR INNER RAMP SKIN CRACKED. DYE PENETRANT INSP. CARRIED OUT ON THE ABOVE AREA IAW MIL-STD-6866. CRACKS FOUND
- [SDR UPS04242341](https://openairdocs.org/sdr/UPS04242341), Apr 16, 2004: SKIN. CHAFED. INSPECTION TYPE:C CHAFING UNDER FAIRING AT BS1050 AND BS1070 JUST BELOW STR26L. AT BS1050 DAMAGE REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-30-1. AREA REP
- [SDR UPS04242358](https://openairdocs.org/sdr/UPS04242358), Apr 15, 2004: RIB. CRACKED. INSPECTION TYPE: C, MID GALLEY DOOR UPPER GATE HINGE RIB CRACKED AT FWD CORNER. HINGE RIB REPLACED IAW DWG 65-16720 AND SRM 51-30-02
- [SDR UPS04242356](https://openairdocs.org/sdr/UPS04242356), Apr 15, 2004: RETAINER. CORRODED. INSPECTION TYPE: C, SEAL RETAINER ON NWW CUTOUT FWD LHS CORRODED SEAL RETAINER REPLACED IAW SRM 51-20-01 AND AMM 20-80-01
- [SDR UPS04242342](https://openairdocs.org/sdr/UPS04242342), Apr 15, 2004: CARGO TRACK. CORRODED. INSPECTION TYPE: C, SECTION OF TIE DOWN RAIL IS CORRODED FROM BS530 TO BS480 IN LOWER FWD CARGO COMPARTMENT. CORRODED SECTION OF TIE DOWN RAIL REMOVED IAW SRM 5
- [SDR UPS04242355](https://openairdocs.org/sdr/UPS04242355), Apr 14, 2004: RETAINER. CORRODED. INSPECTION TYPE: C, FWD RT SEAT RETAINER ON NLG WW CUTOUT CORRODED SEAL RETAINER REMOVED, SEAL RETAINER FABRICATED IAW SRM 51-20-1, SEAL RETAINER INSTALLED MM 2
- [SDR UPS04242320](https://openairdocs.org/sdr/UPS04242320), Apr 14, 2004: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C AIR LEAK FROM CRACK ON NWW WEB LHS BS 287. PAINT STRIPPED, HFEC INSPECTION C/O CRACKS CONFIRMED, CRACKED AREA CUT OUT, HFEC C/O AROUND CUT OUT
- [SDR UPS04242318](https://openairdocs.org/sdr/UPS04242318), Apr 14, 2004: DOUBLER. CORRODED. INSPECTION TYPE:C OLD REPAIR DOUBLER HAS SIGNS OF INTERGRANULAR CORROSION IN LOWER NOSE COMPT, DOUBLER LOCATED ON VERTICAL INTERNAL STRUCTURE OF NWW RBL 14.6 B 
- [SDR UPS04242357](https://openairdocs.org/sdr/UPS04242357), Apr 13, 2004: WEB. CRACKED. INSPECTION TYPE: C, 5 FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB CRACKED. K FLAP ACTUATOR REMOVED, TRUNNION SUPPORT BOX I/B WEB REMOVED. WEB FABRICATED IAW DWG 
- [SDR UPS03240913](https://openairdocs.org/sdr/UPS03240913), Jun 26, 2003: SKIN. CRACKED. INSPECTION TYPE: ASV, SKIN PANEL BELOW L1 AND R1 CENTER WINDOW POST HAS .375 INCH CRACK FROM EDGE TO RIVET. CONFIRMED BY DYE PENETRANT INSP. REPLACED SKIN PANEL
- [SDR UPS02239758](https://openairdocs.org/sdr/UPS02239758), Oct 10, 2002: HINGE. CRACKED. UPPER HINGE ARM OF AFT ENTRY DOOR CRACKED. HINGE REPLACED. FUNCTION AND OPERATION CHECK CARRIED OUT IAW MM 52-13-02 AND 52-13-00.
- [SDR UPS02239609](https://openairdocs.org/sdr/UPS02239609), Oct 4, 2002: SHEAR TIE. CRACKED. INSPECTION TYPE:C+SI STR.SHEAR TIE CRACKED AT STR.5 R/H BS1050. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACED IAW 51-20-1+51-40-3
- [SDR UPS02239769](https://openairdocs.org/sdr/UPS02239769), Oct 3, 2002: SPAR. CORRODED. DURING PREPARATION FOR CENTER SECTION REAR SPAR WEB SPLICE REPAIR, ADDITIONAL CORROSION WAS NOTED ON UPPER CHORD INBOARD OF LBL 34.20. WEB, CHORD, SPLICE AND ST
- [SDR UPS02239767](https://openairdocs.org/sdr/UPS02239767), Sep 30, 2002: BEAM. CORRODED. DURING REMOVAL OF T/E PANEL ATTACHED TO LOWER SURFACE OF RT MLG SUPPORT BEAM, CORROSION NOTED AROUND MLG SUPPORT BEAM FASTENER HOLE. CORROSION REMOVED AROUND HO
- [SDR UPS02239741](https://openairdocs.org/sdr/UPS02239741), Sep 30, 2002: FRAME. DAMAGED. INSPECTION TYPE:C&SI DURING REPAIR OF FRAME BS 560 STR. 7R DAMAGE WAS FOUND ON EXISTING R EPAIR ABOVE AT S5R - 6R REPAIR TO FRAME CARRIED OUT IAW SRM 53-10-4 FI
- [SDR UPS02239740](https://openairdocs.org/sdr/UPS02239740), Sep 30, 2002: PRESSURE PANEL. DAMAGED. PRESS WEB AT BS 740 BULKHEAD DAMAGED AT LWR END WHERE IT ATTACHS TO 740 RT FITTING. DAMAGE BLENDED OUT AND REPAIRED PER SRM 53-10-9 FIG 4.
- [SDR UPS02239774](https://openairdocs.org/sdr/UPS02239774), Sep 24, 2002: RISER. CORRODED. INSPECTION TYPE:C+SI CORROSION ON RISER #5 FOUND TO BE OUTSIDE LIMITS- REF NRC 480122.(AI RSTAIR DOOR) RISER REPLACED IAW SRM ADDENDIUM EO B727-5260-1551-A.
- [SDR UPS02239773](https://openairdocs.org/sdr/UPS02239773), Sep 24, 2002: HINGE PIN. CORRODED. HORIZONTAL STAB HINGE LEFT OUTER PIN HAS EVIDENCE OF PITTING CORROSION ADJACENT TO RELIEF RADIUS. HORIZONTAL STABILIZER HINGE PIN LEFT OUTER REPLACED IAW MM 55-
- [SDR UPS02239719](https://openairdocs.org/sdr/UPS02239719), Sep 24, 2002: RISER. CORRODED. INSPECTION TYPE:C&SI CORROSION ON RISER #6 ON AFT AIRSTAIRS FOUND TO BE OUTSIDE LIMITS RE F. NRC 480122 #6 RISER REPLACED IAW SRM ADDENDUM B727-5260-7551-A
- [SDR UPS02239718](https://openairdocs.org/sdr/UPS02239718), Sep 24, 2002: RISER. CORRODED. INSPECTION TYPE:C&SI CORROSION ON RISER #8 ON AFT AIRSTAIRS DOOR FOUND TO BE OUTSIDE LIMI TS REF. NRC 480122 RISER REPLACED IAW SRM ADDENDUM B727-5260-7551-A
- [SDR UPS02239716](https://openairdocs.org/sdr/UPS02239716), Sep 24, 2002: PANEL. CRACKED. INSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL PANEL RH SIDE ALONG ROW OF FASTNERS BELOW FW D RH PRESSURE PANEL BS 239 FASTENERS REMOVED IAW SRM 51-30-02. CRACK C
- [SDR UPS02239715](https://openairdocs.org/sdr/UPS02239715), Sep 24, 2002: PANEL. CRACKED. INSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL SIDE PANEL RH SIDE ALONG ROW OF FASTENERS AF T OF FWD RH PANEL BS 250 FASTNERS REMOVED IAW SRM 51-30-02. CRACK CUT 
- [SDR UPS02239557](https://openairdocs.org/sdr/UPS02239557), Sep 24, 2002: PIN. CORRODED. INSPECTION TYPE:C&SI HORIZ. STAB. HINGE R/H OUTER PIN HAS EVIDENCE OF PITTING CORROSION A DJACENT TO RELIEF RADIUS HORIZ. STAB HINGE R/H O/B PIN REPLACED IAW MM
- [SDR UPS02239768](https://openairdocs.org/sdr/UPS02239768), Sep 23, 2002: KEELBEAM. CRACKED. CRACKS RT KEEL BEAM VERTICAL WEB FWD OF APU CUT OUT. REPAIR IAW EO B727-5330-1995-B.
- [SDR UPS02239717](https://openairdocs.org/sdr/UPS02239717), Sep 23, 2002: FRAME. CORRODED. BS 740 BULKHEAD LWR CHORD FOUND CORRODED DURING REMOVAL TO FACILITATE FITTING REPLACEMENT. SECTION OF CHORD REPLACED IAW DRAWING 65C13724.
- [SDR UPS02239558](https://openairdocs.org/sdr/UPS02239558), Sep 23, 2002: INTERCOSTAL. CRACKED. INSPECTION TYPE:C&SI COCKPIT FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 294 & 284 LBL 5 REMOVED INTERCOSTAL IAW SRM 51-30-2 FABRICATED INTERCOSTAL IAW SRM 53-10-2 
- [SDR UPS02239607](https://openairdocs.org/sdr/UPS02239607), Sep 22, 2002: RIB. CRACKED. INSPECTION TYPE:C+SI SUSPECT CRACK AT RIB BS 519 AT LWR. STR. ATTACH POINT AFT OF ACCESS PNL. STOP DRILLED CRACK IAW 51-10-1. PAGE 12.
- [SDR UPS02239714](https://openairdocs.org/sdr/UPS02239714), Sep 20, 2002: SEAT TRACK. CORRODED. CORROSION AROUND NUT BS 380 LBL 45.5 ON SEAT TRACK. REMOVED DAMAGED SECTION IAW SRM 51-30-2, REPAIRED IAW SRM 53-10-5.
- [SDR UPS02239639](https://openairdocs.org/sdr/UPS02239639), Sep 20, 2002: FRAME. DENTED. INSPECTION TYPE:C+SI DENT IN FRAME BS 560 STR7 R/H REPAIRED IAW SRM 53-10-4 FIG 1
- [SDR UPS02239766](https://openairdocs.org/sdr/UPS02239766), Sep 19, 2002: SUPPORT FITTING. CORRODED. INSPECTION TYPE:C+SI CORROSION ON INNER FACE OF RH MLG TRUNNION SUPPORT FITTING. RH MLG TRUNNION SUPPORT FITTING REPLACED.
- [SDR UPS02239756](https://openairdocs.org/sdr/UPS02239756), Sep 19, 2002: STIFFENER. CORRODED. BULGING EVIDENT ON WING CENTER SECTION REAR SPAR WEB AT BS 870, 3RD VERTICAL STIFFENER FROM LEFT SIDE. CORROSION FOUND ON VERTICAL STIFFENER AT LBL 24.70. STIFF
- [SDR UPS02239745](https://openairdocs.org/sdr/UPS02239745), Sep 19, 2002: FRAME. CRACKED. INSPECTION TYPE:C&SI CRACK ON LWR AFT FLANGE OF FRAME BS 930 R/H AT MLG PRESS. WEB REPAIRS TO S15 & S16 CARRIED OUT IAW SRM 53-10-3. FRAME REPAIR BS 9 20 SPLICE
- [SDR UPS02239721](https://openairdocs.org/sdr/UPS02239721), Sep 19, 2002: FRAME. CRACKED. INSPECTION TYPE:C&SI LWR AFT CARGO BAY, FRAME (BS1030)TO FUSELAGE SKIN ATTACH POINT IS CR ACKED IN BEND RADIUS BETWEEN STR 25 AND STR. 26L/H FRAME REPAIRED IAW 

All 175: https://openairdocs.org/deregistered/N930UP-2007-11-21/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 19890609027589I](https://openairdocs.org/incident/19890609027589I), Jun 9, 1989: Boeing 72722C (N930UP), Louisville, KY. Unsafe nose gear light. Lowered gear manually. Landed without incident. Cleaned and lubricated gear parts.

## Other aircraft with N930UP

- [Registered now](https://openairdocs.org/aircraft/N930UP): Boeing 767-300F, S/N 70805

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