# N691UP: 1969 Boeing 747-121, registration cancelled 2002-05-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 2, 2002
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 747-121](https://openairdocs.org/model/boeing-747-121) (registry code 1384871)
- Engine: [Pratt & Whitney JT9D-3A](https://openairdocs.org/engine/pratt-whitney-jt9d-3a) (registry code 52050)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE), [TCDS E20EA](https://openairdocs.org/tcds/E20EA) (OpenAirDocs)
- Serial number: 19641
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 18, 1970
- Certificate issued: March 13, 1996
- Last registry action: March 18, 2008
- Mode S code: A9303D
- Owner when cancelled: [C C & E I LLC](https://openairdocs.org/faa-owner/C%20C%20%26%20E%20I%20LLC)
- 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/N691UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=691UP
- Page: https://openairdocs.org/deregistered/N691UP-2002-05-02

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 747-121: https://openairdocs.org/model/boeing-747-121.md

## Service difficulty reports (251, newest 50)

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

- [SDR UPS01436395](https://openairdocs.org/sdr/UPS01436395), Jul 25, 2001: AILERON. MALFUNCTIONED. INSPECTION TYPE:N/A PRE-FLT- AILERONS BND WHEN YOKE IS TURNED LEFT. BINDING OCCURS APPR E LEFT LIMIT FURTHER DEFLECTION OF THE LEFT SPOILER IS IND ON THE CP I W
- [SDR UPS01436167](https://openairdocs.org/sdr/UPS01436167), Jun 24, 2001: LIGHT. INTERMITTENT. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER COCKPIT IS INTERMITTENT. REPLACED LIGHT ASSY, OPS CHECK NORMAL.
- [SDR UPS01435269](https://openairdocs.org/sdr/UPS01435269), Mar 13, 2001: ENGINE. MALFUNCTIONED. INSPECTION TYPE:PFLT DURING INITIAL ROTATION FOR T/O SMOKE (LITE SMOKE) ENTERED COCKPIT AND SPREAD INTO CABIN. PUT ON OXY MASKS, INCLUDING 1 ACM FOLLOWED SMOKE 
- [SDR UPS00434550](https://openairdocs.org/sdr/UPS00434550), Dec 17, 2000: CIRCUIT BOARD. FAILED. INSPECTION TYPE:N/A ON LEVEL OFF AT 11,000, ON DECENT LOWER CARGO FIRE LIGHT ILLUMINATED INTERMITTENTLY REPLACED FIRE WARING CARD "A8" ON FIRE WARNING P6 CARD F
- [SDR UPS00434542](https://openairdocs.org/sdr/UPS00434542), Dec 12, 2000: BATTERY PACK. INOPERATIVE. INSPECTION TYPE:PFLT CEILING EMERGENCY LIGHT INOP R/R EMERGENCY LIGHT POWER PACK
- [SDR UPS00434517](https://openairdocs.org/sdr/UPS00434517), Nov 29, 2000: BOTTLE. DISCHARGED. INSPECTION TYPE:N/A CREW AND COURIER O2 DEPLETED IN ROUTE R AND R BOTTLES ALL REGS OP CHECK NORMAL
- [SDR UPS00434113](https://openairdocs.org/sdr/UPS00434113), Sep 9, 2000: FRAME. CRACKED. INSPECTION TYPE: C, LT WING CRACK FOUND ON UPPER AND LOWER CHORD AND WEB ON L/E AT ILES 1110. NEW CHORDS FABRICATED IAW EO206770 AND EO206774 AND REFITTED IAW Q
- [SDR UPS00434112](https://openairdocs.org/sdr/UPS00434112), Sep 8, 2000: STIFFENER. CRACKED. INSPECTION TYPE:C, NR 1 STRUT STIFFENER CRACKED AT VERT BULKHEAD NAC STA 180. NEW BRACKET FABRICATED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434111](https://openairdocs.org/sdr/UPS00434111), Sep 6, 2000: FLOOR PANEL. CRACKED. INSPECTION TYPE:C, CRACK IN FWD CARGO HOLD FLOOR SKIN AT BS 478 RBL 36. REPAIRED IAW SRM 51-40-02.
- [SDR UPS00434047](https://openairdocs.org/sdr/UPS00434047), Sep 2, 2000: ANGLE. CRACKED. INSPECTION TYPE:C, RT WING T/E SPOILER SUPPORT BEAM WEB CRACKED AFT OF 6 FLAP TRANSMISSION. REPAIR ACCOMPLISHED, SPLICE REPAIR USING 15.5 PH CRES ANGLES IAW QUE
- [SDR UPS00434119](https://openairdocs.org/sdr/UPS00434119), Aug 25, 2000: FLANGE. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1453. REPAIR CARRIED OUT IAW SRM 57-20-03.
- [SDR UPS00434110](https://openairdocs.org/sdr/UPS00434110), Aug 9, 2000: FORGING. CORRODED. INSPECTION TYPE:C, PLEASE REPLACE CORRODED WINDOW FORGINGS AT BS 240 - 260 LT SIDE IAW SRM. WINDOW FORGING REMOVED IAW SRM 51-30-02 NEW FORGING FITTED SRM 51-30
- [SDR UPS00434039](https://openairdocs.org/sdr/UPS00434039), Aug 7, 2000: FORGING. CRACKED. INSPECTION TYPE:C, REPLACE CRACKED WINDOW FORGING BS 1460 - 1480 RT SIDE. WINDOW FORGING REPLACED IAW SRM 51-30-02.
- [SDR UPS00434127](https://openairdocs.org/sdr/UPS00434127), Aug 4, 2000: BEAM. CRACKED. INSPECTION TYPE:C, VERTICAL STABILIZER T/E CRACK ON TRAILING EDGE BEAM AT FIN STA 245 RT. REPAIRED TRAILING EDGE BEAM WEB IAW SRM 55-30-06.
- [SDR UPS00434126](https://openairdocs.org/sdr/UPS00434126), Aug 4, 2000: WEB. CRACKED. INSPECTION TYPE:C, LOWER RUDDER L/E FAIRING, TWO WEBS CRACKED AT FOLLOWING LOCATIONS RT RUD STA 147 AND LT RUD STA 32. WEB AT RT RUD STA 147 REPAIRED IAW SRM 51
- [SDR UPS00434124](https://openairdocs.org/sdr/UPS00434124), Aug 2, 2000: INTERCOSTAL. CRACKED. INSPECTION TYPE:C, CONTROL CABIN INTERCOSTAL IS CRACKED AT BS 360 - 380 BETWEEN STR 1 AND 2 RT. CRACKED INTERCOSTAL REMOVED AND NEW INTERCOSTAL FABRICATED AND F
- [SDR UPS00433726](https://openairdocs.org/sdr/UPS00433726), Aug 2, 2000: FITTING. CORRODED. INSPECTION TYPE:C, RT HORIZONTAL STABILIZER INTERIOR CORROSION FOUND ON A RIGHT ANGLE FITTING AT STAB STA 243, BETWEEN REAR SPAR AND S1 UPPER SURFACE. PLEASE IN
- [SDR UPS00434122](https://openairdocs.org/sdr/UPS00434122), Aug 1, 2000: STIFFENER. CRACKED. INSPECTION TYPE:C, AIR COND CRACK IN RAM AIR DUCT STIFFENER AT BS 960. NEW STIFFENER FABRICATED IAW BAC5300 AND FITTED IAW SRM 51-30-02.
- [SDR UPS00434099](https://openairdocs.org/sdr/UPS00434099), Jul 28, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE FOUND CRACKED BY NDT INSP ON L/E RIB AT OLES 1411.85. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434097](https://openairdocs.org/sdr/UPS00434097), Jul 28, 2000: FLANGE. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE FOUND CRACKED ON L/E RIB AT OLES 1421.35. REPAIRED RIB IAW SRM 57-20-03 FIG 1.
- [SDR UPS00434095](https://openairdocs.org/sdr/UPS00434095), Jul 28, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE ON L/E RIB AT OLES 1525.45 FOUND CRACKED. RIB REPLACED IAW SRM 51-30-02.
- [SDR UPS00434093](https://openairdocs.org/sdr/UPS00434093), Jul 28, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1534.95. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434092](https://openairdocs.org/sdr/UPS00434092), Jul 28, 2000: RIB. WORN. INSPECTION TYPE:C, TAIL VERTICAL FIN LWR L/E SECTION OF RIB WORN AT CONTACT AREA WITH DORSAL FIN. RIB REPLACED IAW SRM 51-30-02.
- [SDR UPS00434091](https://openairdocs.org/sdr/UPS00434091), Jul 28, 2000: FRAME. CRACKED. INSPECTION TYPE:C, APU COMPT FRAME CRACKED RT SIDE BS 2675 WL 310. FRAME REPAIRED IAW SRM 51-40-03 USING 2024 T3 .040.
- [SDR UPS00434089](https://openairdocs.org/sdr/UPS00434089), Jul 26, 2000: SPAR. CORRODED. INSPECTION TYPE:C, LT HORZ STAB REAR SPAR UPPER CHORD CORRODED AT STAB BL 380. CHORD REPAIRED IAW QUERY NOTE 56/200.
- [SDR UPS00434086](https://openairdocs.org/sdr/UPS00434086), Jul 26, 2000: RIB. CRACKED. INSPECTION TYPE:C, CRACKED RIB UPPER CHORD ON LT HORZ STAB BEHIND R/SPAR AT STAB BL 39 1. CHORD REPAIRED IAW SRM 51-40-03.
- [SDR UPS00434083](https://openairdocs.org/sdr/UPS00434083), Jul 26, 2000: BEAM. CRACKED. INSPECTION TYPE:C, TAIL VERTICAL STABILIZER T/E BEAM SUPPORTS FOUND CRACKED AT RUD STA 132 LT, RT, 157 LT, 267 LT RT ,282 LT & RT, 307 LT & RT, 332 RT AND 367 R
- [SDR UPS00434033](https://openairdocs.org/sdr/UPS00434033), Jul 26, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING L/E CRACKING ON UPPER FLANGE OF L/E RIB AT OLES 1390.75. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434101](https://openairdocs.org/sdr/UPS00434101), Jul 25, 2000: DOOR FRAME. CRACKED. INSPECTION TYPE:C, DOOR 4 LT REMOVED FOR REPAIR OF FWD FRAME DAMAGE. NR 4 DOOR FWD FRAME REPAIRED IAW SRM 52-10-02 FIG 13. MATERIAL AIS I301 .050 HFEC INSP ACCO
- [SDR UPS00434035](https://openairdocs.org/sdr/UPS00434035), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT L/E CRACKING ON UPPER FLANGE ON L/E RIB AT OLES 1493.45. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434031](https://openairdocs.org/sdr/UPS00434031), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1048.25. NEW RIB INSTALLED RIB REPLACED IAW SRM 51-30-02.
- [SDR UPS00434029](https://openairdocs.org/sdr/UPS00434029), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 705.55. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434026](https://openairdocs.org/sdr/UPS00434026), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 974.05. REPAIR CARRIED OUT IAW SRM 57-20-03 FIG 1.
- [SDR UPS00434022](https://openairdocs.org/sdr/UPS00434022), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1014.95. NEW RIB INSTALLED IAW 51-30-02.
- [SDR UPS00434021](https://openairdocs.org/sdr/UPS00434021), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 964.55. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434019](https://openairdocs.org/sdr/UPS00434019), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 852.45. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434018](https://openairdocs.org/sdr/UPS00434018), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 878.55. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434017](https://openairdocs.org/sdr/UPS00434017), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE ON L/E RIB AT ILES 889.5. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434015](https://openairdocs.org/sdr/UPS00434015), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIBS AT ILES 928.96. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434014](https://openairdocs.org/sdr/UPS00434014), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 928.96. NEW RIB INSTALLLED IAW SRM 51-30-02.
- [SDR UPS00434013](https://openairdocs.org/sdr/UPS00434013), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 938.45. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434012](https://openairdocs.org/sdr/UPS00434012), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE ON L/E RIB AT ILES 1024.45. CRACKS REPAIRED IAW SRM 57-20-03 FIG 3 USING 2024 T3 X 0.125.
- [SDR UPS00434010](https://openairdocs.org/sdr/UPS00434010), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE OF L/E RIB CRACKED AT ILES 756.95. REPAIR CARRIED OUT IAW SRM 57-20-03 FIG 1. FASTENERS FITTED IAW SRM 51-30-02.
- [SDR UPS00434009](https://openairdocs.org/sdr/UPS00434009), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 768.45. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434008](https://openairdocs.org/sdr/UPS00434008), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1014.95. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434007](https://openairdocs.org/sdr/UPS00434007), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 974.05. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434006](https://openairdocs.org/sdr/UPS00434006), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 802.6. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434005](https://openairdocs.org/sdr/UPS00434005), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED AT ILES 964.55 L/E RIB CRACKS. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434004](https://openairdocs.org/sdr/UPS00434004), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 842.96. NEW RIB INSTALLED IAW SRM 51-30-02.
- [SDR UPS00434003](https://openairdocs.org/sdr/UPS00434003), Jul 25, 2000: RIB. CRACKED. INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E AT ILES 928.95. NEW RIB INSTALLED IAW SRM 51-30-02.

All 251: https://openairdocs.org/deregistered/N691UP-2002-05-02/reports.md

## Other aircraft with N691UP

- [Registered now](https://openairdocs.org/aircraft/N691UP): Embraer Executive EMB-505, S/N 50500511, built 2019

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