# N17402: Boeing 727-243, registration cancelled 2001-04-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 27, 2001
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-243](https://openairdocs.org/model/boeing-727-243) (registry code 138408D)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 21265
- Type of aircraft: Fixed wing multi engine
- Certificate issued: April 5, 2001
- Last registry action: April 5, 2001
- Mode S code: A12A7C
- Owner when cancelled: [International Trading Company Of Yukon Inc](https://openairdocs.org/faa-owner/INTERNATIONAL%20TRADING%20COMPANY%20OF%20YUKON%20INC)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Corporation
- Owner's area on the map: 35.5180° N, 97.5730° W: Placed by OpenAirDocs at the center of ZIP code 73112, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N17402
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17402
- Page: https://openairdocs.org/deregistered/N17402-2001-04-27

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 727-243: https://openairdocs.org/model/boeing-727-243.md

## Service difficulty reports (67, newest 50)

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

- [SDR CALA9901738](https://openairdocs.org/sdr/CALA9901738), Dec 29, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE IN CABIN AND AT OVERWING EXITS, BOTH SIDES. MAINTENANCE REPLACED A BAD FUSE. THE BATTERY PACKS WERE REMOVE
- [SDR CALA9900418](https://openairdocs.org/sdr/CALA9900418), Apr 15, 1999: SKIN. CORRODED. INSPECTION FOUND AFT LAV SERVICE PANEL AFT LOWER SKIN CORRODED. THE PANEL WAS REMOVED AND THE CORRODED INNER SKIN WAS REMOVED. A NEW SKIN AND INTERNAL AND OUTER
- [SDR CALA9900417](https://openairdocs.org/sdr/CALA9900417), Apr 15, 1999: STRINGER. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN STRINGER 23L BETWEEN STA 1183 AND 1161, JUST BELOW LAV SERVICE PANEL INSIDE AFT CARGO COMPARTMENT. THE CRACKED SECTION OF STR
- [SDR CALA9900407](https://openairdocs.org/sdr/CALA9900407), Apr 14, 1999: SKIN. CRACKED. INSPECTION FOUND A .5 AND .375 INCH CRACK IN LT O/B AILERON LOWER SKIN WITH A BEND AT I/B EDGE. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-31.
- [SDR CALA9900401](https://openairdocs.org/sdr/CALA9900401), Apr 13, 1999: WIRE. BROKEN. THE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED IAW WPM 20-10-13, PAGE 1. OPERATION OF THE EXI
- [SDR CALA9900400](https://openairdocs.org/sdr/CALA9900400), Apr 13, 1999: ANGLE. CRACKED. INSPECTION FOUND A 2.75 INCH CRACK IN LT WING REAR SPAR O/B SUPPORT ANGLE WHERE NR 2 SPOILER ACTUATOR AND FLAP DRIVE CASTING MOUNTS. THE SUPPORT ANGLE WAS REMOV
- [SDR CALA9900398](https://openairdocs.org/sdr/CALA9900398), Apr 13, 1999: BRACKET. CRACKED. INSPECTION FOUND A .125 INCH CRACK AT UPPER END OF OUTBOARD BRACKET AT RT WING LEADING EDGE WHERE NR 5 L/E FLAP ACTUATOR MOUNTS. THE FASTENERS AND SUPPORT BRACK
- [SDR CALA9900397](https://openairdocs.org/sdr/CALA9900397), Apr 13, 1999: SKIN. DEBONDED. INSPECTION FOUND LT WING I/B MIDFLAP I/B END OF TRAILING EDGE SKIN DEBONDED. THE DEBONDED AREA WAS CUT OUT, A SKIN AND DOUBLER HOT BOND REPAIR WAS PERFORMED IAW
- [SDR CALA9900396](https://openairdocs.org/sdr/CALA9900396), Apr 13, 1999: CONTROL TAB. DENTED. INSPECTION FOUND THE RT ELEVATOR CONTROL TAB UPPER O/B TRAILING EDGE SKIN DENTED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.
- [SDR CALA9900387](https://openairdocs.org/sdr/CALA9900387), Apr 12, 1999: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT O/B FOREFLAP I/B END CASTING AT LEADING EDGE AND TRAILING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.
- [SDR CALA9900386](https://openairdocs.org/sdr/CALA9900386), Apr 12, 1999: SKIN. DEBONDED. INSPECTION FOUND LT I/B FOREFLAP UPPER SURFACE DEBONDED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-14.
- [SDR CALA9900385](https://openairdocs.org/sdr/CALA9900385), Apr 12, 1999: SKIN. DEBONDED. INSPECTION FOUND RT WING UPPER AND LOWER SKIN DEBONDED O/B AND AFT OF APU EXHAUST AREA. THE SKIN PANEL WAS REPAIRED IAW SRM 51-30-08 PAGE 1.
- [SDR CALA9900384](https://openairdocs.org/sdr/CALA9900384), Apr 12, 1999: SKIN. CRACKED. INSPECTION FOUND A .3125 INCH CRACK IN RT INBOARD AFT FLAP LOWER LEADING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-02.
- [SDR CALA9900372](https://openairdocs.org/sdr/CALA9900372), Apr 7, 1999: WEDGE. DEBONDED. INSPECTION FOUND RT WING O/B MID FLAP T/E WEDGE DEBONDED. THE TRAILING WAS REMOVED AND REPLACED IAW SRM 51-30-2, PAGE 1.
- [SDR CALA9900371](https://openairdocs.org/sdr/CALA9900371), Apr 7, 1999: TAB. DENTED. INSPECTION FOUND LEFT ELEVATOR CONTROL TAB LOWER O/B LEADING EDGE SKIN DENTED. THE LEFT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.
- [SDR CALA9900370](https://openairdocs.org/sdr/CALA9900370), Apr 7, 1999: BULKHEAD ANGLE. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FWD BULK VERT ANGLE AT RT WHEEL WELL BS 870 KEEL BEAM. THE FWD BULK VERT ANGLE WAS REPLACED IAW SRM 51-10-1, PAGE 4 AND 51-
- [SDR CALA9900369](https://openairdocs.org/sdr/CALA9900369), Apr 7, 1999: PRESSURE DECK. CRACKED. INSPECTION FOUND A 3.5 INCH CRACK IN NOSE WHEEL WELL PRESSURE DECK AT FS 270, LBL 14. THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40
- [SDR CALA9900368](https://openairdocs.org/sdr/CALA9900368), Apr 7, 1999: CHORD. CRACKED. INSPECTION FOUND A .375 INCH AND .125 INCH CRACK AT LT WING NR 2 SLAT LOWER CHORD BELOW TELESCOPING ANT-ICE TUBE. THREE ACCESS PANELS WERE REMOVED PER SRM 51-30
- [SDR CALA9900367](https://openairdocs.org/sdr/CALA9900367), Apr 7, 1999: CHORD. CRACKED. INSPECTION FOUND A .3125 INCH CRACK AT LT WING NR 1 SLAT LOWER CHORD AT CUTOUT BELOW TELESCOPING ANTI-ICE TUBE. THE CRACK WAS STOP DRILLED AND AN ANGLE REPAIR W
- [SDR CALA9900366](https://openairdocs.org/sdr/CALA9900366), Apr 7, 1999: CHORD. CRACKED. INSPECTION FOUND A 3 INCH AND .375 INCH CRACK AT RT WING NR 7 SLAT LOWER CHORD. THE LOWER SLAT PANEL WAS REMOVED FOR ACCESS AND REMOVED ANGLE IAW SRM 51-30-2, P
- [SDR CALA9900365](https://openairdocs.org/sdr/CALA9900365), Apr 7, 1999: FLOORBEAM WEB. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FLOORBEAM WEB AT FS 294, RBL 48. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-2 FIGURE 1, SHEET 6.
- [SDR CALA9900364](https://openairdocs.org/sdr/CALA9900364), Apr 7, 1999: SKIN. DEBONDED. INSPECTION FOUND RT O/B FLAP AFT SEGMENT DEBONDED AT TRAILING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.
- [SDR CALA9900363](https://openairdocs.org/sdr/CALA9900363), Apr 7, 1999: SKIN. DENTED. INSPECTION FOUND LT O/B FLAP AFT SEGMENT UPPER SURFACE DENTED AND DEBONDED. THE FLAP WAS REPAIRED IAW SRM 51-40-6.
- [SDR CALA9900362](https://openairdocs.org/sdr/CALA9900362), Apr 7, 1999: SKIN. DEBONDED. INSPECTION FOUND LT INBOARD AFT FLAP LOWER SURFACE DEBONDED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-2.
- [SDR CALA9801915](https://openairdocs.org/sdr/CALA9801915), Oct 1, 1998: BATTERY. DISCHARGED. INSPECTION FOUND RT AFT CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED AND LIGHT WAS RELAMPED.
- [SDR CALA9801234](https://openairdocs.org/sdr/CALA9801234), Jul 11, 1998: GEAR HANDLE. LACK OF LUBE. WHEN GEAR WAS EXTENDED ON APPROACH, CREW RECEIVED THREE GREEN AND THREE RED GEAR INDICATION LIGHTS. THE GEAR WAS CYCLED AND CREW GOT THREE GREEN. THE AIRCRAFT L
- [SDR CALA9800202](https://openairdocs.org/sdr/CALA9800202), Feb 9, 1998: DOOR FRAME. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN UPPER AFT SECTION OF R-1 DOOR FRAME AT BS 410. THE CRACKED SECTION OF DOOR FRAME WAS CUTOUT IAW BOEING DRAWING 69-69978. A NE
- [SDR CALA9800198](https://openairdocs.org/sdr/CALA9800198), Feb 7, 1998: WEB. CRACKED. INSPECTION FOUND A .125 CRACK IN RT MLG WHEEL WELL PRESSURE WEB AT BS 872.5, RBL 52.25. A PRESSURE WEB REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03671.
- [SDR CALA9800191](https://openairdocs.org/sdr/CALA9800191), Feb 4, 1998: SUPPORT. CRACKED. INSPECTION FOUND CABIN FLOOR SUPPORT WEB CRACKED .125 BEYOND STOP DRILL HOLE AT STA 303.9, LBL 45. THE FLOOR SUPPORT WEB WAS REMOVED. A REPAIR WAS FABRICATED AN
- [SDR CALA9800190](https://openairdocs.org/sdr/CALA9800190), Feb 4, 1998: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27R CORRODED IN AFT CARGO COMPARTMENT BETWEEN STA 720 AND 720A. THE CORRODED SECTION OF STRINGER AND SKIN WERE REMOVED. A STRINGER REP
- [SDR CALA9800183](https://openairdocs.org/sdr/CALA9800183), Feb 4, 1998: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 279, STRINGER 22L. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-1, FIGURE 1, 53-30-3, FIGURE 13, 
- [SDR CALA9800182](https://openairdocs.org/sdr/CALA9800182), Feb 4, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT CLIP NUTS, STA 380 BETWEEN RBL 24 AND 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-8.
- [SDR CALA9800181](https://openairdocs.org/sdr/CALA9800181), Feb 4, 1998: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN TEAR STRAP CORRODED IN FORWARD CARGO COMPARTMENT AT BS 68, STRINGER 28R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-4, 
- [SDR CALA9800180](https://openairdocs.org/sdr/CALA9800180), Feb 3, 1998: SUPPORT. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK IN LT ELEVATOR SUPPORT AT TRAILING EDGE OF ELEVATOR OUTBOARD OF INBOARD TRIM TAB HINGE BEARING. A 1.25 INCH CRACK WAS FOUND I
- [SDR CALA9800179](https://openairdocs.org/sdr/CALA9800179), Feb 3, 1998: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R IN FORWARD CARGO COMPARTMENT CORRODED BETWEEN STA 680 AND 700. THE STRINGER SPLICE WAS REMOVED AND A STRINGER SPLICE WAS FABRICATE
- [SDR CALA9800178](https://openairdocs.org/sdr/CALA9800178), Feb 3, 1998: SKIN. CRACKED. INSPECTION FOUND A 5.25 INCH CRACK IN FUSELAGE SKIN AT STA 510 BETWEEN STRINGER 25 AND 26R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. THE DOUBLER 
- [SDR CALA9800177](https://openairdocs.org/sdr/CALA9800177), Feb 3, 1998: SUPPORT. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK ON UPPER FLANGE OF CABIN FLOOR SUPPORT THREE INCHES AFT OF FLOORBEAM AT STA 294.5, RBL 45. THE FLOOR SUPPORT WAS REMOVED, A RE
- [SDR CALA9700977](https://openairdocs.org/sdr/CALA9700977), Jun 29, 1997: SEQUENCE VALVE. LEAKING. THE SYSTEM-A HYDRAULIC FAILURE LIGHTS ILLUMINATED ON CO-PILOT PANEL AFTER GEAR RETRACTION. ALSO, THE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHTS ON SECOND OFFICER'S 
- [SDR CALA9700796](https://openairdocs.org/sdr/CALA9700796), Jun 1, 1997: HYD MODULE. CRACKED. THE AIRCRAFT WAS DIVERTED TO PHX, AFTER LOSING THE A-HYDRAULIC SYSTEM FLUID QUANTITY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRA
- [SDR CAL960373](https://openairdocs.org/sdr/CAL960373), Mar 20, 1996: FLEX HOSE. LEAKING. FLT NR 477 - TPA - A/C LOST THE 'B' SYS HYD FLUID IN FLT. THE LOSS WAS ACCOMPANIED BY FLICKERING 'B' SYS HYD LOW PRESS LIGHTS. CHECKLIST PROCEDURES WERE COMPLIE
- [SDR CAL960251](https://openairdocs.org/sdr/CAL960251), Feb 2, 1996: ANGLE. CORRODED. STATION 31J - INSPECTION FOUND CORROSION AT BOTTOM OF FLOOR BEAM AT GILL SUPPORT FRAME ANGLE IN AFT CARGO PIT AT BS 1168, RBL 55. THE CORRODED AREA OF ANGLE WAS
- [SDR CAL960266](https://openairdocs.org/sdr/CAL960266), Jan 27, 1996: FLOOR PAN. CORRODED. INSPECTION FOUND CENTER OF LT AFT LAV FLOOR PAN CORRODED AT BS 1140 TO BS 1176. THE CORROSION WAS REMOVED FROM THE FLOOR PAN. A REPAIR DOUBLER WAS FABRICATED AN
- [SDR CAL960272](https://openairdocs.org/sdr/CAL960272), Jan 26, 1996: CHANNEL SUPPORT. CORRODED. STATION 31J - INSPECTION FOUND CORROSION ON CHANNEL SUPPORT AT BS 803, BL 0. THE CORROSION WAS REMOVED AND A 'T' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW S
- [SDR CAL960271](https://openairdocs.org/sdr/CAL960271), Jan 25, 1996: PANEL SUPPORT. CORRODED. STATION 31J - INSPECTION FOUND LOWER FUSELAGE PANEL SUPPORT CORRODED AT BS 880, LBL 9 AND RBL 9. THE CORRODED AREA WAS CUT OUT. REPAIR ANGLES AND FILLERS WERE F
- [SDR CAL960274](https://openairdocs.org/sdr/CAL960274), Jan 24, 1996: FLAP TRACK. CORRODED. STATION 31J - INSPECTION FOUND CORROSION AT RIGHT MLG BEAM INBOARD FLAP INBOARD TRACK ATTACH POINT. THE AREA WAS REPAIRED IAW ECRA 5750-02438. (M)
- [SDR CAL960273](https://openairdocs.org/sdr/CAL960273), Jan 24, 1996: BEAM. CORRODED. INSPECTION FOUND CORROSION ON LT MLG BEAM LOWER FLANGE AT INBOARD FLAP INBOARD TRACK ATTACH POINT. A REPAIR WAS PERFORMED IAW ECRA 5750-02437 AND SRM 51-10-6 AD
- [SDR CAL960269](https://openairdocs.org/sdr/CAL960269), Jan 24, 1996: FLOOR BEAM. CORRODED. STATION 31J - INSPECTION FOUND ELONGATED HOLES AND PITTING CORROSION IN FLOOR BEAM AND SEAT TRACK AT BS 1010, RBL 55. THE AREA OF ELONGATED HOLES WAS CUT OUT. R
- [SDR CAL960265](https://openairdocs.org/sdr/CAL960265), Jan 21, 1996: FLOOR BEAM. CORRODED. INSPECTION FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1110, RBL 26 TO RBL 44. THE CORRODED SECTION OF FLOOR BEAM UPPER CHORD WAS REMOVED. A REPAIR WAS FABRICAT
- [SDR CAL960258](https://openairdocs.org/sdr/CAL960258), Jan 21, 1996: SUPPORT. CORRODED. STATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, RBL 9 BETWEEN HEAT EXCHANGERS. THE CORRODED AREA WAS CUT OUT, TWO 'L'
- [SDR CAL960257](https://openairdocs.org/sdr/CAL960257), Jan 21, 1996: SUPPORT. CORRODED. STATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, LBL 9 BETWEEN LEFT AND RIGHT HEAT EXCHANGER. THE CORROSION WAS REMOVE

All 67: https://openairdocs.org/deregistered/N17402-2001-04-27/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 FTW92LA001](https://openairdocs.org/ntsb/FTW92LA001), Oct 5, 1991: Boeing 727-243 (N17402), Little Rock, AR, no damage. Probable cause: THE PILOT'S FAILURE TO SPECIFICALLY WARN THE FLIGHT ATTENDANTS OF THE HAZARDOUS CONDITIONS WARNINGS. A FACTOR WAS THE TURBULENCE.

## 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.

- [Accident 19911005045669A](https://openairdocs.org/incident/19911005045669A), Oct 5, 1991: Boeing 727243 (N17402), Little Rock, AR. Severe turbulence near thunderstorms at FL350. Seat sign on. Flight attendant injured. Pilot failed advise.

## Other aircraft with N17402

- [Registered now](https://openairdocs.org/aircraft/N17402): Boeing 737-9, S/N 67639, built 2025
- [Cancelled 1937-09-26](https://openairdocs.org/deregistered/N17402-1937-09-26): Aeronca C-3, S/N A-715. Owner: [Witch Duck Aeroplane Corp](https://openairdocs.org/faa-owner/WITCH%20DUCK%20AEROPLANE%20CORP), [Norfolk, VA](https://openairdocs.org/faa-place/VA/Norfolk)

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