# N69348: 1987 Boeing 737-3TO, registration cancelled 2009-10-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 8, 2009
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 23586
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 15, 1987
- Certificate issued: October 26, 1987
- Last registry action: October 17, 2006
- Mode S code: A938E0
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N69348
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=69348
- Page: https://openairdocs.org/deregistered/N69348-2009-10-08

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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md

## Service difficulty reports (47)

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

- [SDR CALA2009070100342](https://openairdocs.org/sdr/CALA2009070100342), Jun 30, 2009: CHARGER. INTERMITTENT. AFT EXIT DOOR EMERGENCY LIGHTS RIGHT AND LEFT SIDE ILUMINATED. REMOVED AND REPLACED BATTERY CHARGER, AND BATTERY PACK. OPS CHECKS GOOD.
- [SDR CALA2008122301163](https://openairdocs.org/sdr/CALA2008122301163), Dec 22, 2008: SKIN. CRACKED. STRINGER 24L, STATION 727E - 718 OUTER SKIN HAS 1 INCH CRACK. REPAIRED CRACK IN OUTER SKIN STRINGER 24L STATION 727 - 718 PER B737 SRM 53-00-01 FIG 201. TOTAL W
- [SDR CALA2008122201162](https://openairdocs.org/sdr/CALA2008122201162), Dec 22, 2008: INTERCOSTAL. CORRODED. FUSELAGE FRAME, SKIN AND SURROUNDING STRUCTURE CORRODED STATION 227.8 FROM LBL-12 TO RBL-12 (BILGE). REMOVED CORROSION FROM HORIZONTAL CHORD, FOUND TO BE WITHIN
- [SDR CALA2008122201159](https://openairdocs.org/sdr/CALA2008122201159), Dec 20, 2008: SKIN. DELAMINATED. RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE INBOARD AND OUTBOARD PROTECTIVE FINISH FOUND DELAMINATION ON OUTBOARD TRAILING EDGE. FABRICATED REPAIR DOUBLER AND REPL
- [SDR CALA2008121901153](https://openairdocs.org/sdr/CALA2008121901153), Dec 18, 2008: SKIN. DELAMINATED. LEFT WING NR 3 SLAT INBOARD END SKIN IS DELAMINATED. REPAIRED LEFT WING NR 3 SLAT TRAILING EDGE WEDGE PER SRM 51-70-10.
- [SDR CALA2008121901152](https://openairdocs.org/sdr/CALA2008121901152), Dec 18, 2008: FLOORBEAM. CRACKED. FLOORBEAM BS 328 LBL 12 UPPER TEE CAP CRACKED SL-7 69. REPAIRED CRACKED FLOORBEAM AT BS 328 LBL 12 UPPER TEE CAP PER SRM 53-10-51 FIG 201.
- [SDR CALA2008121101138](https://openairdocs.org/sdr/CALA2008121101138), Dec 11, 2008: DOOR FRAME. CRACKED. FORWARD CARGO DOOR CUTOUT FORWARD FRAME CRACKED AT LOWER DOOR STOP FITTING AT STR 24R. REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT FORWARD FRAME PER SRM 51-1
- [SDR CALA0800700](https://openairdocs.org/sdr/CALA0800700), Jul 3, 2008: SKIN. CORRODED. GENERATED DIP DUE TO HEAVY CORROSION AT STATION 967, STR 27LT TO STR 27RT, PERFORM A PERMANET REPAIR PER EC/RA 5331-01244 WITHIN 6,000 FLIGHT CYCLES OR 24 MONTH
- [SDR CALA0700525](https://openairdocs.org/sdr/CALA0700525), Sep 20, 2007: ACTUATOR. INOPERATIVE. THE LEFT MLG DID NOT INDICATE DOWN & LOCKED WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. MANUAL EXTENSION WAS PERFORMED AND YAW WAS FELT WHEN LEFT MAIN EXTENDED. 
- [SDR CALA0700490](https://openairdocs.org/sdr/CALA0700490), Aug 20, 2007: CONTROLLER. INOPERATIVE. THE CREW RECEIVED A CABIN ALTITUDE WARNING CLIMBING THROUGH FL 270. THE QRH WAS FOLLOWED AND A RAPID DESCENT TO 13,000 FEET WAS ACCOMPLISHED. CABIN PRESSURE WAS
- [SDR CALA0600239](https://openairdocs.org/sdr/CALA0600239), Jul 3, 2006: BRACE. CORRODED. INSPECTION FOUND HORIZONTAL STABILIZER CENTER BRACE RT LOWER I/B CHORD CORRODED BETWEEN STA 1104 AND 1112. THE AREA WAS REPAIRED IAW ECRA 5510-01840.
- [SDR CALA0600238](https://openairdocs.org/sdr/CALA0600238), Jul 3, 2006: FRAME. CORRODED. INSPECTION FOUND HORIZONTAL STABILIZER CENTER BRACE LT LOWER I/B CHORD CORRODED BETWEEN STA 1121 AND 1129. THE AREA WAS REPAIRED IAW ECRA 5510-01841.
- [SDR CALA0600237](https://openairdocs.org/sdr/CALA0600237), Jul 3, 2006: SKIN. CORRODED. INSPECTION FOUND CORROSION ON AFT INTERIOR SURFACE OF THE LT WING AFT FUEL BOOST PUMP SKIN CUTOUT AT WS 70.85-140. A REPAIR WAS INSTALLED IAW ECRA 5720-01990.
- [SDR CALA0600236](https://openairdocs.org/sdr/CALA0600236), Jul 3, 2006: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 967, S27R. A SKIN REPAIR WAS INSTALLED IAW ECRA 5331-01244.
- [SDR CALA0600228](https://openairdocs.org/sdr/CALA0600228), Jul 1, 2006: FLOORBEAM. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK ON THE TOP EDGE OF FLOORBEAM WEB AT STA 328, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5321-01373.
- [SDR CALA0600227](https://openairdocs.org/sdr/CALA0600227), Jun 30, 2006: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT FORWARD PASSENGER DOOR CUTOUT ON STRINGER 15L SPLICE CHANNEL, STA 360, LBL 50. THE STRINGER WAS REPAIRED IAW ECRA 5311-01259 
- [SDR CALA0600297](https://openairdocs.org/sdr/CALA0600297), Jun 29, 2006: SKIN. CRACKED. INSPECTION FOUND A CRACK AT THREE EACH LIGHTENING HOLES ON THE INNER SKIN OF THE FORWARD CARGO DOOR. THE SKIN WAS REPAIRED IAW ECRA 5232-01076.
- [SDR CALA0600223](https://openairdocs.org/sdr/CALA0600223), Jun 28, 2006: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 765 JUST ABOVE STRINGER 21R ON BONDED DOUBLER LINE. THE CRACKED SECTION OF SKIN WAS CUT OUT AND A DOUBLE
- [SDR CALA0600221](https://openairdocs.org/sdr/CALA0600221), Jun 26, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 328, RBL 11-36. REPLACED T-CAP ON FLOORBEAM IAW SRM 53-10-5, REPAIR 5.
- [SDR CALA0600218](https://openairdocs.org/sdr/CALA0600218), Jun 24, 2006: BELTFRAME. CORRODED. INSPECTION FOUND FORWARD BAGGAGE BIN BELT FRAME CORRODED AT STA 500D, S27L, LBL11-13. A DOUBLER WAS INSTALLED IAW SRM 53-00-07 FIGURE 201 REPAIR 7.
- [SDR CALA0600217](https://openairdocs.org/sdr/CALA0600217), Jun 23, 2006: BELTFRAME. CORRODED. INSPECTION FOUND FORWARD BAGGAGE BIN BELT FRAME CORRODED AT STA 480, S27L, LBL 13-17. REPAIRED IAW SRM 53-00-07.
- [SDR CALA0600214](https://openairdocs.org/sdr/CALA0600214), Jun 21, 2006: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 947-999, LBL 40. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600224](https://openairdocs.org/sdr/CALA0600224), May 13, 2006: FRAME. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN THE FORWARD CARGO DOOR LOWER CORNER FRAME JUST BELOW DOOR HOLD OPEN HOOK. THE DOOR FRAME WAS REPAIRED IAW SRM 51-40-02 AND 
- [SDR CALA0500324](https://openairdocs.org/sdr/CALA0500324), Oct 3, 2005: WIRE. SHORTED. THE FIRST CLASS EMERGENCY ESCAPE AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE FOUND SHORTED WIRING TO TRANSFORMER. THE WIRING WAS REPAIRED AND OPERATI
- [SDR CALA0400713](https://openairdocs.org/sdr/CALA0400713), Nov 9, 2004: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BELOW FASTENER ROW BETWEEN STA 727E AND 747, S24R. A REPAIR DOUBLER AND TRIPLER WERE INSTALLED IAW SRM 53-00-01
- [SDR CALA0400584](https://openairdocs.org/sdr/CALA0400584), Jul 23, 2004: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AND CRACKED AT STA 259.5-360, S24L TO S29L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5310-04421.
- [SDR CALA0400535](https://openairdocs.org/sdr/CALA0400535), Jun 13, 2004: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 747, STRINGER 23L. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 229.
- [SDR CALA0300044](https://openairdocs.org/sdr/CALA0300044), Feb 12, 2003: SKIN. CRACKED. INSPECTION FOUND A 3" CRACK IN FUSELAGE SKIN AT STA 727A, S23L. REPAIRED IAW ECRA 5330-03090.
- [SDR CALA0200352](https://openairdocs.org/sdr/CALA0200352), Jun 19, 2002: KEELBEAM. CORRODED. INSPECTION FOUND KEEL BEAM LT LOWER O/B CHORD CORRODED AT STA 727. REPAIRED IAW ECRA 5311-01127.
- [SDR CALA0200351](https://openairdocs.org/sdr/CALA0200351), Jun 18, 2002: SKIN. CRACKED. INSPECTION FOUND #6 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01.
- [SDR CALA0200339](https://openairdocs.org/sdr/CALA0200339), Jun 13, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND MAIN CABIN FLOOR R/H I/B SEAT TRACK HAD CORROSION AND WORN LOBES AT BS 787 AND 797, THE CORRODED AND WORN SECTION OF SEAT TRACK WAS REMOVED AND
- [SDR CALA0200337](https://openairdocs.org/sdr/CALA0200337), Jun 12, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 907-940. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0200335](https://openairdocs.org/sdr/CALA0200335), Jun 10, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 907-935. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-60-52.
- [SDR CALA0200332](https://openairdocs.org/sdr/CALA0200332), Jun 8, 2002: STRAP. CORRODED. INSPECTION FOUND R/H SIDE Y STRAP CORRODED FROM STA 1006 TO AFT PRESSURE BULKHEAD, RBL 6. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200331](https://openairdocs.org/sdr/CALA0200331), Jun 7, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT UNDER R2 DOOR Z-ANGLE AT STA 969 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02, 51-40-02, AND 51-30-01.
- [SDR CALA0200330](https://openairdocs.org/sdr/CALA0200330), Jun 7, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0000552](https://openairdocs.org/sdr/CALA0000552), Apr 25, 2000: HARNESS. BROKEN. EMERGENCY AISLE PATH LIGHTING INOP AT ROW 6 AND 22. REPLACED WIRE HARNESS AT BOTH ROWS PER MAINTENANCE MANUAL 33-51-02 PG 501.
- [SDR CALA9900540](https://openairdocs.org/sdr/CALA9900540), May 10, 1999: TRIGGER. OUT OF POSITION. FORWARD ENTRY DOOR WILL NOT OPEN. FOUND RELEASE LATCH MECHANISM DISSASSEMBLED AND TRIGGER OUT OF POSITION. REASSEMBLED AND TESTED PER MM 52-11-00 PAGE 501.
- [SDR CALA9801501](https://openairdocs.org/sdr/CALA9801501), Aug 24, 1998: STRINGER. CORRODED. INSPECTION FOUND STRINGER CORRODED JUST BELOW RT AFT LAV DUMP CHUTE FROM STA 1006 TO 1016. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STR
- [SDR CALA9801487](https://openairdocs.org/sdr/CALA9801487), Aug 20, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344, LBL 30 TO 20. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9801486](https://openairdocs.org/sdr/CALA9801486), Aug 19, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 15 AND LBL 20. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-10-51.
- [SDR CALA9800721](https://openairdocs.org/sdr/CALA9800721), Apr 29, 1998: OVEN. DIRTY. THE CREW REPORTED SMOKE COMING FROM NR 1 AND NR 2 AFT GALLEY OVENS IN FLIGHT. THE SMOKE WAS MOMENTARY. THE FLIGHT WAS CONTINUED TO DEN WITHOUT FURTHER PROBLEM. 
- [SDR CALA9800016](https://openairdocs.org/sdr/CALA9800016), Jan 12, 1998: LOGIC CARD. INOPERATIVE. THE RT MLG INDICATION WAS SHOWING RED AND GREEN AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE RED LIGHT ILLUMINATED INTERMITTEN
- [SDR CALA9701711](https://openairdocs.org/sdr/CALA9701711), Dec 6, 1997: TIRE. FAILED. A LT MLG TIRE BLEW ON TAKEOFF, THE A-HYD SYSTEM PRESSURE AND QUANTITY WAS LOST. THE AIRCRAFT WAS RETURNED. UPON LANDING THE OTHER LT MLG TIRE BLEW. THE BLOWN TI
- [SDR CALA9700971](https://openairdocs.org/sdr/CALA9700971), Jun 26, 1997: WINDSHIELD. FAILED. A STRONG ODOR ACCOMPANIED BY SMOKE WAS OBSERVED IN THE COCKPIT DURING CLIMB-OUT OF DTW ENROUTE TO EWR. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT 
- [SDR CALA9601302](https://openairdocs.org/sdr/CALA9601302), Sep 4, 1996: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT STA 540, STRINGER 22R. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-11.
- [SDR CAL960191](https://openairdocs.org/sdr/CAL960191), Feb 25, 1996: ROLLERS/TRACKS. LACK OF LUBE. FLT NR 1708 - EWR - WHEN FLAPS WERE SELECTED BEYOND 5 DEGREES CREW RECEIVED T/E FLAP ASYMMETRY. THE SAFETY WIRES WERE BROKEN ON GPWS AND ALTERNATE FLAP MASTER S

## 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 NYC88IA109](https://openairdocs.org/ntsb/NYC88IA109), Mar 19, 1988: Boeing 737 (N69348), Morristown, NJ, incident, no damage

## FAA accident and incident reports (2)

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 20040624016459I](https://openairdocs.org/incident/20040624016459I), Jun 24, 2004: Boeing 7373TO (N69348), Miami, FL. (-23) Flight attendant [privacy data omitted] reported an injury due to turbulence on June 24, 2004. As part of an ongoing company campaign to reduce…
- [Incident 19900316031639I](https://openairdocs.org/incident/19900316031639I), Mar 16, 1990: Boeing 737300 (N69348), Washington, DC. Diverted due to low fuel state. Right fuel gauge problem suspected.

---
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.