# N906UP: 1967 Boeing 727-30C, registration cancelled 2007-05-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 10, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-30C](https://openairdocs.org/model/boeing-727-30c) (registry code 1384009)
- Engine: [Rolls-Royce TAY-651-54](https://openairdocs.org/engine/rolls-royce-tay-651-54) (registry code 54564)
- Data sheets: [TCDS E25NE](https://openairdocs.org/tcds/E25NE) (OpenAirDocs)
- Serial number: 19314
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 4, 1999
- Certificate issued: May 11, 1992
- Last registry action: December 21, 2004
- Mode S code: AC8746
- 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/N906UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=906UP
- Page: https://openairdocs.org/deregistered/N906UP-2007-05-10

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 (109, newest 50)

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

- [SDR UPS03241659](https://openairdocs.org/sdr/UPS03241659), Dec 15, 2003: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT OVER FLIGHT DECK DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, SYS GROUND CHECK GOOD.
- [SDR UPS02239970](https://openairdocs.org/sdr/UPS02239970), Dec 6, 2002: ANGLE. CORRODED. INSPECTION TYPE:C SMALL AREA OF CORROSION NOTED IN R/H WING T/E STRUCTURE WS 383, ANGL E BETWEEN SUPPORT WEB & UPPER T/E SKIN REMOVED FASTNERS FROM CORRODED ARE
- [SDR UPS02239964](https://openairdocs.org/sdr/UPS02239964), Dec 3, 2002: SKIN. CRACKED. INSPECTION TYPE:C ENGINE #1 THRUST REVERSER UPPER DOOR INNER SKIN CRACKED AT UPPER I/B CORNER OF LWR SKIN REPAIRED DAMAGED AREA IAW SRM 78-30-01 FIG 201
- [SDR UPS02239973](https://openairdocs.org/sdr/UPS02239973), Dec 2, 2002: WEB. CRACKED. INSPECTION TYPE:C SUSPECT CRACKS IN NOSE WHEEL WELL R/H WEB, JUST BELOW FWD END OF AFT PRESSURE PANEL REPAIR CARRIED OUT IAW SRM 51-40-2 & 51-30-2. REPAIR PARTS
- [SDR UPS02239961](https://openairdocs.org/sdr/UPS02239961), Dec 2, 2002: LONGERON. CRACKED. INSPECTION TYPE:C ENG. #2 R/H FWD COWL CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK(DOOR SHEAR) LONGERON REMOVED IAW SRM 51-30-02. NEW LONGERON FABRICA
- [SDR UPS02239960](https://openairdocs.org/sdr/UPS02239960), Dec 2, 2002: LONGERON. CRACKED. INSPECTION TYPE: C, ENGINE NR 2, LT NACELLE. CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK (DOOR SHEAR). LONGERON REMOVED IAW SRM 51-30-02. NEW LONGERON
- [SDR UPS02239965](https://openairdocs.org/sdr/UPS02239965), Nov 29, 2002: SKIN. CRACKED. INSPECTION TYPE:C ENG. #1 THRUST REVERSER, UPPER DOOR, INNER SKIN CRACKED AT I/B OF CE NTER OF LWR SKIN REPAIRED DAMAGED AREA IAW SRM 78-30-01 FIG 201
- [SDR UPS02239956](https://openairdocs.org/sdr/UPS02239956), Nov 28, 2002: BRACKET. CRACKED. INSPECTION TYPE: C, ENGINE NR 1 & 3 THRUST REVERSER OUTBOARD FAIRING MID SUPPORT BRACKETS CRACKED. REPLACED BRACKETS IAW MM 20-80-01
- [SDR UPS02239955](https://openairdocs.org/sdr/UPS02239955), Nov 26, 2002: FITTING. CRACKED. INSPECTION TYPE:C L/H LWR TENSION TIE FITTING CRACKED AT O/B LUG IN TAILSKID COMPARTME NT INSTALLED NEW L/H LWR TENSION TIE FITTING IAW SRM 51-30-02 & DRAWING 6
- [SDR UPS02239962](https://openairdocs.org/sdr/UPS02239962), Nov 24, 2002: FITTING. CRACKED. INSPECTION TYPE:C TAILSKID BAY R/H UPPER TENSION TIE AFT FITTING CRACKED NEW R/H UPPER TENSION TIE AFT FITTING INSTALLED IAW SRM 51-30-02 AND DRAWING 65-25992
- [SDR UPS02239957](https://openairdocs.org/sdr/UPS02239957), Nov 24, 2002: BULKHEAD. CRACKED. INSPECTION TYPE: C, SUSPECT CRACKS IN NOSE WHEEL WELL BULKHEAD RT SIDE, BETWEEN FASTENER JUST UNDER CENTER OF FWD RT PRESSURE PANEL REPAIR CARRIED OUT IAW SRM 5
- [SDR UPS02239954](https://openairdocs.org/sdr/UPS02239954), Nov 24, 2002: FITTING. CRACKED. INSPECTION TYPE:C TAILSKID BAY L/H UPPER TENSION TIE AFT FITTING CRACKED L/H UPPER TENSION TIE REPLACED IAW SRM 51-30-02 & DRAWING 65-25992
- [SDR UPS02239953](https://openairdocs.org/sdr/UPS02239953), Nov 24, 2002: FITTING. CRACKED. INSPECTION TYPE:C TAILSKID BAY RH LWR TENSION TIE AFT FITTING HAS EVIDENCE OF CRACK INSTALLED NEW R/H LWR TENSION TIE FITTING IAW SRM 51-30-02 & DRAWING 65-2599
- [SDR UPS02239974](https://openairdocs.org/sdr/UPS02239974), Nov 22, 2002: STRUCTURE. DAMAGED. INSPECTION TYPE: C, RT LE, REMOVABLE SECTION, SOME SCREWS HAVE PULLED THROUGH ON UPPER SURFACE AT O/B END (INTERSECTION OF NR 6 KREUGER & NR 5 SLAT). REPAIR CAR
- [SDR UPS02239972](https://openairdocs.org/sdr/UPS02239972), Nov 22, 2002: ELEVATOR. CRACKED. INSPECTION TYPE:C X-RAY INSPECTION SHOWS A CRACK INDICATION ON THE LEFT ELEVATOR AT EL EV STA. 204, APPROX 5" FWD OF THE TRAILING EDGE REPAIR CARRIED OUT IAW SR
- [SDR UPS02239971](https://openairdocs.org/sdr/UPS02239971), Nov 22, 2002: PRESSURE PANEL. CRACKED. INSPECTION TYPE: C, SUSPECT CRACKS ON RT VERTICAL WEB OF NOSE WHEEL WELL AT UPPER FWD EN D OF AFT PRESSURE PANEL. REPAIR CARRIED OUT IAW SRM 51-40-2
- [SDR UPS02239969](https://openairdocs.org/sdr/UPS02239969), Nov 22, 2002: PRESSURE PANEL. CRACKED. INSPECTION TYPE: C. SUSPECT CRACKS ON RT VERTICAL WEB OF NOSE WHEEL WELL IN AREA ADJACENT TO AFT LOWER CORNER OF AFT PRESS PANEL REPAIR PARTS FABRICATED IAW SRM
- [SDR UPS02239963](https://openairdocs.org/sdr/UPS02239963), Nov 22, 2002: ELEVATOR. CRACKED. INSPECTION TYPE:C X-RAY INSP. SHOWS A CRACK INDICATION ON THE RIGHT ELEVATOR JUST I/B OF THE TAB AT ELEV. STA. 47, APPROX. REPAIR CARRIED OUT IAW SRM 51-30-2,51
- [SDR UPS02237691](https://openairdocs.org/sdr/UPS02237691), Feb 15, 2002: LIGHT. UNSECURE. INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT LENS COVER HANGING BY ONE END. FOUND FWD END OF EMERGENCY EXIT LIGHT ASSY NOT SECURED. SECURED LIGHT ASSY AND L
- [SDR UPS02237393](https://openairdocs.org/sdr/UPS02237393), Jan 5, 2002: LENS. LOOSE. INSPECTION TYPE:AS PLASTIC LENS FOR ENTRY DOOR EMERGENCY EXIT LIGHT FALLS OFF. REPLACED LIGHT LENS.
- [SDR UPS02237389](https://openairdocs.org/sdr/UPS02237389), Jan 3, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:IN ENTRY DOOR EMERGENCY LIGHT INOP. INSTALLED NEW BATTERIES IN EMERGENCY EXIT LIGHT OVER ENTRY DOOR. OPS CHECK GOOD.
- [SDR UPS01236732](https://openairdocs.org/sdr/UPS01236732), Aug 29, 2001: GUARD. INOPERATIVE. INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS SWITCH GUARD IS INOP; WHEN LIGHTS ARE TURNED ON TO TEST & GUARD IS CLOSED, LIGHTS REMAIN ON INSTEAD OF MOVING TO ARMED 
- [SDR UPS01235909](https://openairdocs.org/sdr/UPS01235909), May 15, 2001: SKIN. CRACKED. INSPECTION TYPE:C, CRACK ON ANTI-ICE SKIN NR 3 L/E FLAP I/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW UPS EO B727-5750-3082.
- [SDR UPS01235978](https://openairdocs.org/sdr/UPS01235978), May 11, 2001: WEB. CRACKED. INSPECTION TYPE:C NR 3 SLAT ANTI ICE WEB IS CRACKED AT CUTOUT FOR ANTI ICE DUCT. REPAIRED IAW UPS AUTORIZATION B727-57-20028 AND SMRO EO 2001-016-006.
- [SDR UPS01235908](https://openairdocs.org/sdr/UPS01235908), May 11, 2001: WEB. CRACKED. INSPECTION TYPE:C STRUCTURE ABOVE NR 2 ENGINE, WEB CRACKED AT BS 1388 APPROX RT SIDE. NEW WEB INSTALLED IAW SRM 51-30-02 & BOEING DRAWING 65-17555.
- [SDR UPS01235946](https://openairdocs.org/sdr/UPS01235946), May 10, 2001: DOOR FRAME. CRACKED. INSPECTION TYPE:C, SUSPECT CRACK IN LWR AFT CORNER OF FWD CARGO DOOR FRAME. REPLACED LWR AFT CORNER OF FWD CARGO DOOR FRAME IAW DRAWING 65-18620.
- [SDR UPS01235979](https://openairdocs.org/sdr/UPS01235979), May 9, 2001: FITTING. CRACKED. INSPECTION TYPE:C NDI ON BS 950 RT FITTING CONFIRMED CRACK ON OUTBOARD FLANGE BETWEEN S9R AND 10R. RT 950 FRAME FITTING REPLACED IAW UPS EO B727-5310-3011.
- [SDR UPS01235975](https://openairdocs.org/sdr/UPS01235975), May 9, 2001: BEAM. CORRODED. INSPECTION TYPE:C MCD UPPER BEAM AND UPPER BEAM DOUBLER CORRODED. DOOR REMOVED AND UPPER BEAM AND UPPER BEAM DOUBLER REPLACED.
- [SDR UPS01235968](https://openairdocs.org/sdr/UPS01235968), May 9, 2001: STRAP. CRACKED. INSPECTION TYPE:C CRACK INDICATIONS IN REINFORCING STRAP AT MID GALLEY DOOR FWD UPPER CORNER. REPAIR CARRIED OUT IAW UPS EO B727-5330-2685.
- [SDR UPS01235967](https://openairdocs.org/sdr/UPS01235967), May 9, 2001: DOOR FRAME. CRACKED. INSPECTION TYPE:C, CRACK ON AFT UPPER SECTION OF GALLEY DOOR FRAME. REPAIR CARRIED OUT IAW UPS EO B727-5240-4626.
- [SDR UPS01235953](https://openairdocs.org/sdr/UPS01235953), May 8, 2001: STRINGER. CORRODED. INSPECTION TYPE:C, AREA OF SUSPECT CORROSION AT S4L BS 1185. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-10-00, 51-30-4.
- [SDR UPS01235907](https://openairdocs.org/sdr/UPS01235907), May 8, 2001: SKIN. DAMAGED. INSPECTION TYPE:C, FUSELAGE SKIN FOUND TO HAVE WEAR HOLE AT BS 1187 BETWEEN S24 LT & S26 LT SECT 48. REPAIR CARRIED OUT IAW SRM 53-30-3, 51-30-1, 51-20-00, 51-1
- [SDR UPS01235877](https://openairdocs.org/sdr/UPS01235877), May 7, 2001: BRACKET. CRACKED. INSPECTION TYPE:C, WING TO BODY FAIRING ATTACH BRACKET BS 945 S18A LT CRACKED. NEW BRACKET FABRICATED
- [SDR UPS01235113](https://openairdocs.org/sdr/UPS01235113), Feb 28, 2001: LIGHT. INOPERATIVE. INSPECTION TYPE:PFLT, ON PREDEPT CK FOUND COCKPIT EMERGENCY EXIT ASSY INOP IN ARM OR ON. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY, OPS CHECK OK.
- [SDR UPS01234996](https://openairdocs.org/sdr/UPS01234996), Feb 15, 2001: LIGHT. INOPERATIVE. INSPECTION TYPE:IN ON PREFLIGHT CHECK EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WOULD NOT TEST WITH EMERGENCY EXIT LIGHT SWITCH ON O/H. LIGHTS WORK OK AT LIGHT ASS
- [SDR UPS01234654](https://openairdocs.org/sdr/UPS01234654), Jan 19, 2001: LIGHT. DETACHED. INSPECTION TYPE:PFLT CREW REPORTS MAIN ENTRY EMERGENCY EXIT LIGHT FELL OFF AT LANDING. REPLACED EMERGENCY EXIT LIGHT ASSY, OPS NORMAL.
- [SDR UPS00233348](https://openairdocs.org/sdr/UPS00233348), Jul 12, 2000: GENERATOR. OVERHEATED. INSPECTION TYPE:N/A, A/C DECLARED EMERGENCY WITH SMOKE IN THE COCKPIT WITH A CORRESPONDING TRIP ON THE NR 3 GENERATOR BREAKER. AIRCRAFT DIVERTED TO KMDT. MAINTE
- [SDR UPS00232976](https://openairdocs.org/sdr/UPS00232976), Jun 23, 2000: CARTRIDGE. OUT OF ADJ. INSPECTION TYPE:N/A ATB-AILERON BINDING T/S PER MM CHAPT 27-10-00 PG 102,106,AND 107 ADJUSTED AILERON SPRING CARTRIDGE PER MM 27-10-00 OPS CHECKS GOOD ***SUPPLE
- [SDR UPS00231383](https://openairdocs.org/sdr/UPS00231383), Jan 21, 2000: LIGHT. MALFUNCTIONED. L-1 DOOR EMERGENCY LIGHTS DIM. RESEATED L-1 DOOR EMERGENCY LIGHT PACK, LIGHT CHECKS NORMAL PER MM 3 3-50-01.
- [SDR UPS00231382](https://openairdocs.org/sdr/UPS00231382), Jan 5, 2000: SUPPORT. CRACKED. INSPECTION TYPE:C LEFT WING FIXED LEADING EDGE CAVITY VERTICLE OUTBOARD SUPPORT IS CRACKED FOR THE NR 2 SLAT INBOARD TRACK, INBOARD SUPPORT RIB. REPLACED LEFT W
- [SDR UPS99229358](https://openairdocs.org/sdr/UPS99229358), Apr 15, 1999: ENGINE. MALFUNCTIONED. INSPECTION TYPE:N/A ON TEST FLIGHT, PERFORMED TEST EVENT SHUT DOWN OF NR 2 ENGINE. ENGINE NR 2 WAS THEN RESTARTED WITH ALL PARAMETERS NORMAL. MINUTES LATER AS N
- [SDR UPS99228533](https://openairdocs.org/sdr/UPS99228533), Jan 22, 1999: SKIN. CORRODED. INSPECTION TYPE-S, CORROSION BEYOND LIMITS FS 1080 STR 17R EXTERNAL FUSELAGE SKIN. REPAIRED IAW SRM 53-30-3.
- [SDR UPS99228322](https://openairdocs.org/sdr/UPS99228322), Jan 5, 1999: LIGHT. INOP. INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT AT MAIN PAX DOOR INOP. RELAMPED, OPS CHECK GOOD.
- [SDR UPS98227289](https://openairdocs.org/sdr/UPS98227289), Jul 31, 1998: FLOORBEAM. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM ON AND AT NUT PLATES BS 760 TO 848 LBL 45 WL 208. CORRODED PART OUT OF LIM
- [SDR UPS98227283](https://openairdocs.org/sdr/UPS98227283), Jul 31, 1998: BULKHEAD. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) ON BS 1183 BULKHEAD RBL 15 WL 178. REMOVED CORROSION AND ACCOMPLISHED EO B727-5311-0635 WITH THE ADDITION OF EX
- [SDR UPS98227339](https://openairdocs.org/sdr/UPS98227339), Jul 28, 1998: BRACKET. CORRODED. INSPECTION TYPE:SI, CORROSION AROUND EXPANSION LINK BRACKET. REPLACED BRACKET PER SRM 53-10-1.
- [SDR UPS98227337](https://openairdocs.org/sdr/UPS98227337), Jul 28, 1998: SEAT TRACK. CORRODED. INSPECTION TYPE:SI, SEAT TRACK CORRODED BS 760-785 RBL 25. REPLACED TRACK PER SRM 53-10-5.
- [SDR UPS98227284](https://openairdocs.org/sdr/UPS98227284), Jul 28, 1998: SKIN. CORRODED. INSPECTION TYPE-SI, DISHED RIVETS AND PILLOWED SKIN STA 1120 TO 1150 LT 3 STR TO STR 4 LT AND 3 STR RT TO 4 STR RT. REPLACED SKIN PER EO 98-2608.
- [SDR UPS98227336](https://openairdocs.org/sdr/UPS98227336), Jul 27, 1998: LINK. CORRODED. INSPECTION TYPE:SI, CORROSION ON EXPANSION LINK BS 870 RBL 25. REPLACED PER DRAWING 65-34144.
- [SDR UPS98227335](https://openairdocs.org/sdr/UPS98227335), Jul 24, 1998: FLOORBEAM. CORRODED. INSPECTION TYPE:SI CORROSION ON FLANGES OF LONGITUDINAL FLOORBEAM. REPLACED PER DWG 65-34144.

All 109: https://openairdocs.org/deregistered/N906UP-2007-05-10/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CHI96IA200](https://openairdocs.org/ntsb/CHI96IA200), Jun 14, 1996: Boeing 727-30C (N906UP), Chicago, IL, incident, no damage. Probable cause: low pressure in the fuel lines caused when the crossfeed valve was closed and the boost pumps to the effected fuel tank were turned off, a fuel pressure surge (spike) accompanied by a rapid drop in…

## 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 20000712034919I](https://openairdocs.org/incident/20000712034919I), Jul 12, 2000: Boeing 72730C (N906UP), Middletown, PA. (-23) The aircraft declared an emergency due to fumes in the cockpit. The aircraft landed on runway 31 at 2303E. The ARFF responded and the aircraft taxied to…

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