# N69741: 1980 Boeing 727-224, registration cancelled 2013-07-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 23, 2013 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 727-224](https://openairdocs.org/model/boeing-727-224) (registry code 1384076) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22250 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 18, 1980 - Certificate issued: May 8, 2000 - Last registry action: November 18, 2004 - Mode S code: A947B5 - Owner when cancelled: [Planet Airways Inc](https://openairdocs.org/faa-owner/PLANET%20AIRWAYS%20INC) - Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) - Owner type: Corporation - Owner's area on the map: 26.0870° N, 80.1530° W: Placed by OpenAirDocs at the center of ZIP code 33315, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N69741 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=69741 - Page: https://openairdocs.org/deregistered/N69741-2013-07-23 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 727-224: https://openairdocs.org/model/boeing-727-224.md ## Service difficulty reports (148, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COOSDR02158](https://openairdocs.org/sdr/COOSDR02158), Jun 1, 2002: SPAR. CORRODED. RT HORIZONTAL STABILIZER REAR SPAR LOWER CHORD WITH CORROSION. - [SDR COOSDR02157](https://openairdocs.org/sdr/COOSDR02157), Jun 1, 2002: SKIN. DAMAGED. EXTERNAL FUSELAGE FWD C/C CUTOUT SKIN DAMAGED AT BS 560. - [SDR COOSDR02156](https://openairdocs.org/sdr/COOSDR02156), Jun 1, 2002: SKIN. DELAMINATED. SPOILER NR 1 (PN 65-17347-81A)(SN 2445) UPPER AND LOWER SKIN DELAMINATED. - [SDR COOSDR02155](https://openairdocs.org/sdr/COOSDR02155), Jun 1, 2002: SKIN. DELAMINATED. SPOILER NR 6 (PN 65-17348-108A)(SN 1214) UPPER AND LOWER SKIN DELAMINATED. - [SDR COOSDR02154](https://openairdocs.org/sdr/COOSDR02154), Jun 1, 2002: TAB. DELAMINATED. LEFT ELEVATOR TAB (PN 6572799-43)(SN 74084) UPPER AND LOWER SKIN DELAMINATED. - [SDR COOSDR02153](https://openairdocs.org/sdr/COOSDR02153), Jun 1, 2002: SKIN. DELAMINATED. RIGHT WING SPOILER NR 14 (PN 65-17347-81A)(SN 2420) UPPER SKIN DELAMINATED. - [SDR COOSDR02151](https://openairdocs.org/sdr/COOSDR02151), Jun 1, 2002: SKIN. CORRODED. LOWER FUSELAGE SKIN CORRODED, BETWEEN STA 481 AND STA 500-STR 28R. - [SDR 20000712SH005](https://openairdocs.org/sdr/20000712SH005), Jun 21, 2000: SKIN. CORRODED. LEFT FUSELAGE SKIN AT APPROXIMATE STA 700 AND STR 29L, AREA HAD CORROSION. (X) - [SDR 20000712SH004](https://openairdocs.org/sdr/20000712SH004), Jun 21, 2000: WEB. CORRODED. LEFT AFT LAVATORY SHEAR WEB BETWEEN STA 1130 AND STA 1176, LBL 17 TO LBL 62 HAS CORROSION THROUGHOUT. (X) - [SDR 20000712SH003](https://openairdocs.org/sdr/20000712SH003), Jun 21, 2000: STRINGER. CRACKED. FOUND SKIN BULGING AT APPROXIMATELY STA 1052 AND STR 27R. CUT OUT SKIN, NO CORROSION ON SKIN. FOUND CORROSION AND CRACK ON LOWER SURFACE OF STR 27R BY RADIUS LO - [SDR CALA9901458](https://openairdocs.org/sdr/CALA9901458), Nov 1, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND EMERGENCY EXIT LIGHTS AT FORWARD ENTRY DOOR AND OVERHEAD AT ROW 17 INOPERATIVE. THE BATTERY PACKS WERE REMOVED, RECHARGED, AND REINSTALLED. OPE - [SDR CALA9901457](https://openairdocs.org/sdr/CALA9901457), Nov 1, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND THE CENTER OVERHEAD EMERGENCY EXIT LIGHTS ALL DIM OR INOPERATIVE. THE BATTERY PACK WAS REMOVED, THE CONNECTORS WERE CLEANED AND THE BATTERY PAC - [SDR CALA9901456](https://openairdocs.org/sdr/CALA9901456), Nov 1, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND THE LT AND RT FORWARD EXIT DOOR OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, THE CONNECTOR WAS CLEANED, AND THE BAT - [SDR CALA9901455](https://openairdocs.org/sdr/CALA9901455), Nov 1, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND THE FORWARD GALLEY DOOR RT OUTSIDE EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS RECHARGED AND OPERATION CHECKED GOOD IAW MM 33-50-0, PAGE - [SDR CALA9901454](https://openairdocs.org/sdr/CALA9901454), Nov 1, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND THE LT AND RT AFT EXIT DOOR OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED, THE CONNECTOR WAS CLEANED, AND THE BATTER - [SDR CALA9901452](https://openairdocs.org/sdr/CALA9901452), Nov 1, 1999: SKIN. DELAMINATED. INSPECTION FOUND NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1, PAGE 401 & 403. - [SDR CALA9901446](https://openairdocs.org/sdr/CALA9901446), Oct 29, 1999: SKIN. GOUGED. INSPECTION FOUND RIGHT I/B FOREFLAP O/B LEADING EDGE GOUGED. THE RIGHT I/B FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1, PAGE 404 AND 406. - [SDR CALA9900712](https://openairdocs.org/sdr/CALA9900712), Jun 18, 1999: SWITCH. INOPERATIVE. THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING IAH. GEAR RECYCLING DID NOT HELP. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO - [SDR CALA9900188](https://openairdocs.org/sdr/CALA9900188), Feb 22, 1999: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 5 FLAP TRACK CARRIAGE LOWER FORWARD ROLLER I/B YOKE FITTING. THE FLAP CARRIAGE WAS REMOVED AND REPLACED IAW MM 27-51-3. - [SDR CALA9900187](https://openairdocs.org/sdr/CALA9900187), Feb 22, 1999: ACOUSTIC PANEL. TORN. INSPECTION FOUND NR 2 ENGINE INLET ACOUSTIC PANEL TORN. THE TORN AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 54-10-3. - [SDR CALA9900186](https://openairdocs.org/sdr/CALA9900186), Feb 22, 1999: SKIN. CORRODED. INSPECTION FOUND LT O/B MIDFLAP UPPER TRAILING EDGE SKIN CORRODED AND SEPARATING I/B TO O/B END. INSTALLED NEW TRAILING EDGE IAW SRM 51-30-2. - [SDR CALA9900184](https://openairdocs.org/sdr/CALA9900184), Feb 22, 1999: SKIN. DELAMINATED. INSPECTION FOUND LT TRAILING EDGE O/B AFT FLAP UPPER SURFACE DELAMINATED. THE LT O/B AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-12. - [SDR CALA9900183](https://openairdocs.org/sdr/CALA9900183), Feb 22, 1999: SKIN. CORRODED. INSPECTION FOUND THE LT WING NR 10 SPOILER CORRODED WITH SCREWS PULLING THROUGH SKIN AT TOP CENTER HINGE. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1. - [SDR CALA9900182](https://openairdocs.org/sdr/CALA9900182), Feb 22, 1999: SKIN. DELAMINATED. INSPECTION FOUND THE LT WING NR 13 SPOILER UPPER TRAILING EDGE DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-00. - [SDR CALA9900181](https://openairdocs.org/sdr/CALA9900181), Feb 22, 1999: SKIN. CORRODED. INSPECTION FOUND LT WING NR 6 L/E SLAT O/B END UPPER AND LOWER SURFACES CORRODED AT SCREWS. THE SLAT WAS REMOVED AND REPLACED IAW MM 27-80-00. - [SDR CALA9900180](https://openairdocs.org/sdr/CALA9900180), Feb 22, 1999: SKIN. DELAMINATED. INSPECTION FOUND RT TRAILING EDGE O/B AFT FLAP LOWER SURFACE DELAMINATED. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-50-02. - [SDR CALA9900179](https://openairdocs.org/sdr/CALA9900179), Feb 22, 1999: SKIN. CORRODED. INSPECTION FOUND RT O/B FOREFLAP CORRODED ON LOWER AND UPPER SURFACE I/B TO O/B. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11. - [SDR CALA9900178](https://openairdocs.org/sdr/CALA9900178), Feb 22, 1999: SKIN. DEBONDED. INSPECTION FOUND THE LT WING NR 2 SPOILER DEBONDED AT TRAILING EDGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-81. - [SDR CALA9900177](https://openairdocs.org/sdr/CALA9900177), Feb 22, 1999: SPAR CHORD. CORRODED. INSPECTION FOUND TOP SURFACE OF LT WING FRONT SPAR LOWER CHORD CORRODED AT FS 355 TO 367. THE FASTENERS AND RIB WERE REMOVED FOR ACCESS. THE CORROSION WAS REMOV - [SDR CALA9900174](https://openairdocs.org/sdr/CALA9900174), Feb 19, 1999: WIRE. FAILED. INSPECTION FOUND FORWARD AISLE EMERGENCY CEILING LIGHT INOPERATIVE. MAINTENANCE FOUND EMERGENCY AISLE LIGHT FORWARD SECTION WIRING SPLICE AT FAULT. THE WIRING S - [SDR CALA9900173](https://openairdocs.org/sdr/CALA9900173), Feb 19, 1999: FITTING. BROKEN. INSPECTION FOUND RT O/B AILERON TAB SUPPORT FITTING (SECOND FROM O/B END) BROKEN OFF INSIDE AILERON. THE TAB SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51 - [SDR CALA9900172](https://openairdocs.org/sdr/CALA9900172), Feb 19, 1999: SKIN. DELAMINATED. INSPECTION FOUND LT WING I/B AFT FLAP DELAMINATED. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-50-2. - [SDR CALA9900171](https://openairdocs.org/sdr/CALA9900171), Feb 19, 1999: WIRE. FAILED. INSPECTION FOUND LT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND POWER WIRE AT BATTERY PACK AT FAULT. THE WIRING SPLICE WAS REPAIRED IAW - [SDR CALA9900170](https://openairdocs.org/sdr/CALA9900170), Feb 19, 1999: WIRE. LOOSE. INSPECTION FOUND L-2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE AT POWER SUPPLY CONNECTOR. THE WIRING WAS SECURED AND OPERATIONAL CHE - [SDR CALA9900160](https://openairdocs.org/sdr/CALA9900160), Feb 15, 1999: SKIN. DEBONDED. INSPECTION FOUND LT WING NR 4 SPOILER UPPER SURFACE OB T/E DEBONDED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1. - [SDR CALA9900159](https://openairdocs.org/sdr/CALA9900159), Feb 15, 1999: SPOILER. DELAMINATED. INSPECTION FOUND NR 11 SPOILER SPLIT AND DELAMINATED AT CENTER T/E TOP SURFACE AREA. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1. - [SDR CALA9900158](https://openairdocs.org/sdr/CALA9900158), Feb 15, 1999: BEAM. CRACKED. INSPECTION FOUND A .25 CRACK IN J BEAM ABOVE LT WING NR 7 SPOILER ACTUATOR. THE J BEAM WAS REMOVED IAW SRM 51-30-2. A NEW J BEAM WAS INSTALLED WITH NUT PLATE IA - [SDR CALA9900157](https://openairdocs.org/sdr/CALA9900157), Feb 15, 1999: MIDFLAP. BENT. INSPECTION FOUND LT WING IB MIDFLAP BENT AT AFT IB AREA. THE BENT AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 57-50-2, PAGE 5. - [SDR CALA9900137](https://openairdocs.org/sdr/CALA9900137), Feb 12, 1999: WIRE. SHORTED. INSPECTION FOUND EMERGENCY PATH SEAT MOUNTED LIGHTS INOPERATIVE FROM ROW 5 TO 15. CAPPED SHORTED WIRES AND OPERATION CHECKED NORMAL IAW MM 33-51-00, PAGE 112. - [SDR CALA9800837](https://openairdocs.org/sdr/CALA9800837), May 11, 1998: BEAM. CORRODED. LEFT MLG SUPPORT BEAM LOWER ATTACH BORE FOR SWING LINK FORWARD AND AFT FACES CORRODED. REMOVED CORROSION, PEENED AREA, ALODINED AND PRIMED AREA, FABRICATED AND - [SDR CALA9800840](https://openairdocs.org/sdr/CALA9800840), May 9, 1998: TRUNNION. CORRODED. LEFT MLG FWD TRUNNION I/B SIDE OF FITTING INNER SIDE CORRODED. REPAIRED PER EO 97-871 AND EC/RA 5740-01840. - [SDR CALA9800839](https://openairdocs.org/sdr/CALA9800839), May 9, 1998: PANEL. STAINED. AFT CARGO COMPARTMENT FS 950 TO 1183, LBL 60 TO RBL 60 STAINED WITH BLUE WATER. FABRICATED AND INSTALLED NEW CEILING AND SIDE WALL PANELS PER EC/RA 2550-01040 A - [SDR CALA9800838](https://openairdocs.org/sdr/CALA9800838), May 9, 1998: FITTING. CORRODED. LEFT MLG FWD TRUNNION ATTACH ANGLE FITTING ON LEG CORRODED. REPAIRED PER EO 98-871 AND EC/RA 5740-01840. - [SDR CALA9800836](https://openairdocs.org/sdr/CALA9800836), May 9, 1998: SWING LINK. CORRODED. LEFT MLG SWING LINK ATTACH LUGS ARE CORRODED ON FACES AND BORE HOLES. COMPLIED WITH REWORK PER EO 98-0847 AND EC/RA 5740-01842. - [SDR CALA9800835](https://openairdocs.org/sdr/CALA9800835), May 9, 1998: SKIN. CORRODED. COMPLY WITH FWD DRAIN HOLE EA 5330-01463. REMOVED BELLY SKIN AND VERIFIED DOUBLERS INSTALLED. CLEANED AND REINSTALLED EXISTING DOUBLERS PER EA 5330-01463. - [SDR CALA9800834](https://openairdocs.org/sdr/CALA9800834), May 9, 1998: 0OWNLOCK. WORN. LEFT MLG DOWNLOCK CRANK HOLES ARE OVERSIZED. FABRICATED AND INSTALLED TWO BUSH INGS PER OHM 32-01-02. - [SDR CALA9800833](https://openairdocs.org/sdr/CALA9800833), May 9, 1998: STRINGER. CORRODED. AFT CARGO PIT STR 29R STA 950 CORRODED. REMOVED AND REPLACED STRINGER PER DWGS 65C20489 AND 65C13913. - [SDR CALA9800832](https://openairdocs.org/sdr/CALA9800832), May 9, 1998: SKIN. CORRODED. AFT CARGO PIT STR 29R STA950 CORRODED. REMOVED AND REPLACED NR 4 BELLY SKIN PER DWGS 65C20489 AND 65C13913. - [SDR CALA9800831](https://openairdocs.org/sdr/CALA9800831), May 9, 1998: ANGLE. CRACKED. AFT FUSELAGE AT FS 950 RT ELEPHANT EAR FAIRING ATTACH ANGLE CRACKED (3). CUT OUT CRACKED PORTION OF FAIRING ATTACH ANGLE. FABRICATED AND INSTALLED REPAIR PER SR - [SDR CALA9800841](https://openairdocs.org/sdr/CALA9800841), May 8, 1998: PANEL. CRACKED. LT UPPER INBOARD T/E PANEL HAS SURFACE CORROSION AND CRACK. REMOVED SURFACE CORROSION. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-10-1, 51-10-6, AND 51 All 148: https://openairdocs.org/deregistered/N69741-2013-07-23/reports.md ## 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 20031001029949I](https://openairdocs.org/incident/20031001029949I), Oct 1, 2003: Boeing 727224 (N69741), Chicago, IL, Minor damage. (-23) On the 1 October 2003 planet airways flight 41 (originally given as department of justice flight 41) a Boeing 727-200 registration number N69741 landed… - [Incident 19921022054759I](https://openairdocs.org/incident/19921022054759I), Oct 22, 1992: Boeing 727224 (N69741), Babelthuap, KQ, Minor damage. Aircraft experienced severe turbulence at cruise altitude. Seat belt on. Continued to koror. ## Other aircraft with N69741 - [Cancelled 1974-09-24](https://openairdocs.org/deregistered/N69741-1974-09-24): Cessna 310Q, S/N 310Q0953. Exported to France. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), Zaventem --- 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.