# N8882Z: 1978 Boeing 727-225, registration cancelled 2010-07-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 20, 2010
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-225](https://openairdocs.org/model/boeing-727-225) (registry code 1384077)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21579
- Year built: 1978
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 16, 1978
- Certificate issued: June 29, 2004
- Last registry action: June 15, 2010
- Mode S code: AC3E43
- Owner when cancelled: [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC)
- Location: [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul)
- Owner type: Corporation
- Owner's area on the map: 38.5420° N, 95.1245° W: Placed by OpenAirDocs at the center of ZIP code 66079, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N8882Z
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8882Z
- Page: https://openairdocs.org/deregistered/N8882Z-2010-07-20

From the FAA registry file of November 3, 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 727-225: https://openairdocs.org/model/boeing-727-225.md

## Service difficulty reports (58, newest 50)

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

- [SDR DL72S030304](https://openairdocs.org/sdr/DL72S030304), Mar 31, 2003: PROXIMITY SENSOR. OUT OF ADJUST. ON T/O AT APPROX 80 KTS NR 3 REVERSER LIGHT CAME ON. T/O ABORTED. ADJUSTED PROX SWITCH.
- [SDR DL72S030279](https://openairdocs.org/sdr/DL72S030279), Mar 26, 2003: FAIRING. LOOSE. AT FL300 SPEED .78/285KTS THE AIRCRAFT HAD MODERATE TO SEVERE VIBRATION IN AIRCRAFT AND CONTROLS. FOUND INBOARD RT FLAP ELEPHANT EAR AND CANOE LOOSE. REPAIRED S
- [SDR DL72S021475](https://openairdocs.org/sdr/DL72S021475), Dec 26, 2002: RIB. CRACKED. VERT. STAB RIB L/H ATTACH ANGLE CRACKED AT FIN STA 133.800 AND STR 9LEFT REPAIR PER M/M 55-30-000-8
- [SDR DL72S020642](https://openairdocs.org/sdr/DL72S020642), Jun 9, 2002: WARNING SYSTEM. ACTIVATED. CREW REPORTS NOSE GEAR UNSAFE INDICATION AND VIBRATION ON GEAR RETRACTION. JACKED NOSE AND SWUNG GEAR, ALL OPS NORMAL.
- [SDR DL72S020571](https://openairdocs.org/sdr/DL72S020571), May 17, 2002: SKIN. CRACKED. THE UPPER HINGE CUTOUT OF THE L1 DOOR CUTOUT WAS FOUND WITH A .5 INCH CRACK IN THE SKIN AND A CRACK INDICATION AT A FASTENER HOLE IN THE BEAR STRAP. THE CRACKS 
- [SDR DL72S020549](https://openairdocs.org/sdr/DL72S020549), May 14, 2002: STRINGER. CORRODED. FOUND ON D1 LETTER CK, CORROSION AT STR 28 RT AT STA 620. REPAIRED PER SRM 53-10-3.
- [SDR DL72S011714](https://openairdocs.org/sdr/DL72S011714), Oct 21, 2001: SKIN. CRACKED. FUSELAGE / SKIN / FWD GALLEY DOOR CUTOUT / LWR AFT CORNER : CRACK REPAIR THE LOWER AFT CORNER OF THE FWD GALLEY DOOR CUTOUT WAS FOUNDWITH A CRACK EMANATING FROM
- [SDR DL72S011688](https://openairdocs.org/sdr/DL72S011688), Oct 18, 2001: SKIN. CRACKED. FOUND ON C2 LETTER CK 5/16 IN CRACK FUSELAGE SKIN R-1 DOOR LOWER AFT CUTOUT. REPAIRED PER ERA 381969-14 AND EO 4-58974-3AD.
- [SDR DL72S011451](https://openairdocs.org/sdr/DL72S011451), Aug 29, 2001: CHARGER. INOPERATIVE. L-1 WING EMERGENCY EXIT LIGHT INOP, REPLACED CHARGER.
- [SDR DL72S010282](https://openairdocs.org/sdr/DL72S010282), Feb 17, 2001: BATTERY PACK. DISCHARGED. ON L/O CHECK, FOUND R-2 OVERHEAD EMERGENCY EXIT DOOR LIGHT INOP. REPLACED R-2 OVERHEAD EMERGENCY EXIT DOOR BATTERY PACK, OPS NOW NORMAL.
- [SDR DL72S002502](https://openairdocs.org/sdr/DL72S002502), Dec 21, 2000: FRAME. CRACKED. FUSELAGE / OVERWING EXIT / LT / FRAME / FS 783.95 : CRACK REPAIR. INSPECTIONS OF THE LH OVERWING EMERGENCY EXIT OPENING FRAMESREVEALED CRACKING IN THE FS 783.95
- [SDR DL72S002006](https://openairdocs.org/sdr/DL72S002006), Oct 13, 2000: START VALVE. FAILED. NR 2 ENGINE START VALVE CAME AT CLIMBOUT POWER 1.96 EPR WITH THE AIRCRAFT PASSING 5000 FT MSL. AFTER ENGINE NR 2 WAS RETARDEDTHE START VALVE OPEN LIGHT EXTINGUI
- [SDR DL72S001506](https://openairdocs.org/sdr/DL72S001506), Aug 9, 2000: WEB. CRACKED. A 1.5 INCH CRACK IN VERTICAL TORQUE BOX WEB RT FS 121, 3 INCHES JUST ABOVE THIRD STEP FROM TOP (48 SEC). REPAIRED PER M/M.
- [SDR DL72S001463](https://openairdocs.org/sdr/DL72S001463), Aug 2, 2000: SKIN. CORRODED. THE FUSELAGE SKIN AND UNDERLYING STRINGER WERE FOUND CORRODED BETWEEN FS 680 & 700 AT STRINGER 27R. THE DAMAGED SECTION OF SKIN AND STRINGER WERE CUTOUT AND REM
- [SDR DL72S001424](https://openairdocs.org/sdr/DL72S001424), Jul 27, 2000: BEAM. TOOL DAMAGE. WHILE ACCOMPLISHING INSPECTIONS OF THE LBL 17.8 VERTICAL BEAM ON THE FS 1183 BULKHEAD PER BAC S/B 727-53-0210 AND AD 99-18-05, AN ELONGATED HOLE WAS FOUND COMMO
- [SDR DL72S001126](https://openairdocs.org/sdr/DL72S001126), Jun 10, 2000: VALVE. INOPERATIVE. LEFT PACK WILL NOT HOLD CABIN PRESS ABOVE 10,000 FEET. CARGO HEAT OUTFLOW VALVE CLOSED AND PACK ON PRESSURE IN MANUAL OUTFLOW VALVE FULL CLOSED. DUCT PRESSURE W
- [SDR DL72S001015](https://openairdocs.org/sdr/DL72S001015), May 24, 2000: BATTERY PACK. INOPERATIVE. OVERWING EMERG LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S991844](https://openairdocs.org/sdr/DL72S991844), Aug 9, 1999: STRINGER. CRACKED. VERTICAL STAB INTERIOR, STRINGER CRACKED AT TIE TO RIB LEFT SIDE AT FIN STA 1338. INSTALLED REPAIR PER SRM 55-30-0 FIG 803.
- [SDR DL72S991317](https://openairdocs.org/sdr/DL72S991317), Jun 10, 1999: ANGLE. CRACKED. MLG W/W STA 913 ANGLE CRACKED AT UPPER RADIUS BLOCK ABOVE UPLOCK. REPAIRED PER DAL M/M 53-11-0 PGS 834-837 AND ERA 367582-14 ALLOWING USE OF DAL M/M REPAIR ON E
- [SDR DL72S991316](https://openairdocs.org/sdr/DL72S991316), Jun 10, 1999: FRAME. CRACKED. LTR CHECK A2, 1 INCH CRACK AT C-2 DOOR CUTOUT FWD FRAME WEB AT LOWER END. REPAIRED PER SRM 53-10-4.
- [SDR DL72S991314](https://openairdocs.org/sdr/DL72S991314), Jun 10, 1999: WEB. CRACKED. FOUND ON A2 LETTER CK. .25 INCH CRACK AT RT TORQUE BOX VERT WEB LOWER LIGHTENING HOLE STA 1243. REPAIRED PER MM 53-11-0.
- [SDR DL72S991313](https://openairdocs.org/sdr/DL72S991313), Jun 10, 1999: WEB. CRACKED. FOUND ON A-2 LETTER CK, .5 INCH CRACK AT LT TORQUE BOX VERTICAL WEB AT THE UPPER LIGHTENING HOLE STA 1243. REPAIRED PER MM 53-11-0.
- [SDR DL72S991099](https://openairdocs.org/sdr/DL72S991099), May 18, 1999: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN OVER 2R SERVICE DOOR FLICKERS FROM DIM TO BRIGHT WITH EMERGENCY LIGHT SYSTEM OFF.
- [SDR DL72S990732](https://openairdocs.org/sdr/DL72S990732), Apr 3, 1999: VALVE. LEAKING. LOSS OF B HYD IN FLT. REPLACED LEAKING CHECK VALVE IN LEFT WHEEL WELL.
- [SDR DL72S990401](https://openairdocs.org/sdr/DL72S990401), Feb 26, 1999: WIRE. CRACKED. ON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL CRACKS ON INSULATION ON ALL 3 GEN FEED CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48SEC TO FIREWAL
- [SDR DL72S990368](https://openairdocs.org/sdr/DL72S990368), Feb 22, 1999: SKIN. DAMAGED. INCORPORATION OF SKIN DAMAGE INTO MODIFICATION DOUBLER WHILE ACCOMPLISHING A MODIFICATION TO THE AIRCRAFT. INSTALLED FED-EX HUSHKITS AND EXISTING SKIN REPAIR WA
- [SDR DL72S990323](https://openairdocs.org/sdr/DL72S990323), Feb 18, 1999: ANGLE. CORRODED. ON HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLE WITH NEW MFG RT SIDE.
- [SDR DL72S990322](https://openairdocs.org/sdr/DL72S990322), Feb 17, 1999: CORD ANGLE. NEW. ON HUSH-KIT MOD, FOUND LT NR 2 ENG MOUNT CHORD ANGLE CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLE WITH ANGLE OF NEW MFG.
- [SDR DL72S982629](https://openairdocs.org/sdr/DL72S982629), Dec 26, 1998: VALVE. FAILED. LEFT PACK ON, CAUSED SMOKE IN CABIN. REPLACED FWD PACK VALVE AND MIX VALVE. CK OK.
- [SDR DL72S982277](https://openairdocs.org/sdr/DL72S982277), Nov 5, 1998: WEB. CRACKED. FOUND ON A1 LETTER CK, .5 INCH CRACK LT LOWER TORQUE BOX VERTICAL WEB STA 1283. REPAIRED PER MM 53-11-0 AND ERA 366033-14.
- [SDR DL72S982276](https://openairdocs.org/sdr/DL72S982276), Nov 5, 1998: WEB. CRACKED. FOUND ON A1 LETTER CK, 1 INCH CRACK LT TORQUE BOX VERTICAL WEB FWD OF STA 1223. REPAIRED PER MM 53-11-0 AND ERA 366033-14.
- [SDR DL72S982275](https://openairdocs.org/sdr/DL72S982275), Nov 5, 1998: RIB. CRACKED. FOUND ON A1 LETTER CK, 1 INCH CRACK L/E RIB O/B OF ACTUATOR ON NR 4 SLAT. REPAIRED PER MM 57-54-0 AND ERA 366036-14.
- [SDR DL72S981552](https://openairdocs.org/sdr/DL72S981552), Jul 24, 1998: BATTERY PACK. DISCHARGED. EXTERIOR EMERGENCY LIGHT INOP RT SIDE 2ND LIGHT AFT OF OVERWING ESCAPE HATCHES. REPLACED BULBS, BATTERY PACK, CLEANED SOCKETS AND CHECKS OK.
- [SDR DL72S981551](https://openairdocs.org/sdr/DL72S981551), Jul 24, 1998: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP ABOVE AFT AIRSTAIR BOTTOM STEP IN CEILING. RELAMPED AND CLEANED SOCKET, CHECKS OK.
- [SDR DL72S981102](https://openairdocs.org/sdr/DL72S981102), May 22, 1998: OUTFLOW VALVE. STUCK. AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. ALL MODES TRIED, PULLED AND RESET C/B, NO HELP. REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER AND CONTROL PANEL.
- [SDR DL72S980991](https://openairdocs.org/sdr/DL72S980991), May 11, 1998: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT M1088 FAIL TEST. REPLACED BATTERY PACK, CHECKS OK.
- [SDR DL72S980850](https://openairdocs.org/sdr/DL72S980850), Apr 20, 1998: FRAME. CORRODED. INBD CHORD OF THE FS 620 FRAME WAS FOUND CORRODED APPROX 2 INCHES OUTBD OF S26R. CORROSION WAS ON THE INBD CHORD ONLY. REPAIRED PER ERA 331533-14.
- [SDR DL72S980798](https://openairdocs.org/sdr/DL72S980798), Apr 10, 1998: SKIN. DAMAGED. AN EXISTING REPAIR WAS REMOVED FROM THE LOWER SKIN PANEL NEAR THE STRINGER 20R LAP SPLICE. THE UNDERLYING SKIN CUTOUT WAS 3.5 X 4. THE SKIN CUTOUT AND SURROUNDI
- [SDR DL72S980785](https://openairdocs.org/sdr/DL72S980785), Apr 7, 1998: FLOORBEAM. CORRODED. THE UPPER CAP OF THE FS 1110 PASSENGER FLOORBEAM WAS FOUND CORRODED. A SECTION OF THE CAP WAS CUT OUT BETWEEN RBL 12 AND LBL 12. THE CAP WAS REPAIRED WITH A FIL
- [SDR DL72S980510](https://openairdocs.org/sdr/DL72S980510), Feb 18, 1998: SKIN. WORN. DURING SHOP VISIT THE LEADING EDGE SKIN WAS FOUND WORN BEYOND LIMITS AT THE I/B END OF FLAP. THE SKIN WAS REPAIRED PER 727 MM 57-52-0, FIG 803 BY REMOVING THE D
- [SDR DL72S980324](https://openairdocs.org/sdr/DL72S980324), Dec 23, 1997: SPAR. CRACKED. AFT SPAR LWR RAIL GOUGED 57 FROM I/B END N/R 004267. AFT SPAR LWR RAIL, CRACKED FROM I/B END. N/R 004268, BOTH AREAS REPAIRED PER M/M 57-52-0 FIG 802. AFT SPAR 
- [SDR DL72S980156](https://openairdocs.org/sdr/DL72S980156), Dec 22, 1997: ANGLE. CRACKED. THE MIDFLAP WAS FOUND TO HAVE A CRACKED REAR SPAR ANGLE DURING SHOP VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.
- [SDR DL72S980155](https://openairdocs.org/sdr/DL72S980155), Dec 22, 1997: ANGLE. CRACKED. THE MIDFLAP WAS FOUND WITH A CRACKED REAR SPAR ANGLE DURING SHOP VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.
- [SDR DL72S980154](https://openairdocs.org/sdr/DL72S980154), Dec 22, 1997: COVE SKIN. CRACKED. DURING SHOP VISIT/INSPECTION, THE NR 2 MIDFLAP COVESKIN WAS FOUND CRACKED 31 INCHES FROM I/B END AT DRIVE ROD CUTOUT. THE COVESKIN WAS REPAIRED PER 727 MM 57-52
- [SDR DL72S980153](https://openairdocs.org/sdr/DL72S980153), Dec 22, 1997: ANGLE. CRACKED. DURING SHOP VISIT/INSPECTION, THE NR 2 MIDFLAP AFT SPAR ANGLE WAS FOUND CRACKED 32 FROM THE I/B END OF FLAP. THE DAMAGE WAS REPAIRED PER 727 MM 57-52-0 BY INSTA
- [SDR DL72S980509](https://openairdocs.org/sdr/DL72S980509), Dec 18, 1997: RIB. CRACKED. DURING SHOP VISIT, THE AFT RIB WAS FOUND CRACKED AT AFT SPAR I/B END OF FLAP. THE RIB WAS REPAIRED PER 727 MM 57-52-0 FIG 808 BY STOP DRILLING THE CRACK AND INS
- [SDR DL72S980400](https://openairdocs.org/sdr/DL72S980400), Dec 18, 1997: SKIN. WORN. DURING SHOP INSPECTION, THE FLAP WAS FOUND WITH LEADING EDGE SKIN WORN BEYOND ALLOWABLE DAMAGE LIMITS AT O/B END. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGED 
- [SDR DL72S980058](https://openairdocs.org/sdr/DL72S980058), Dec 11, 1997: ANGLE. CRACKED. AFT LOWER SPAR CHORD ANGLE IS CRACKED 22 FROM O/B END OF FLAP. REPAIRED PER M/M 57-52-0.
- [SDR IXKA9700003](https://openairdocs.org/sdr/IXKA9700003), Feb 2, 1997: BATTERY PACK. DISCHARGED. AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK OK PER MM 33-50-23. (M)
- [SDR IXKA9600075](https://openairdocs.org/sdr/IXKA9600075), Sep 2, 1996: LIGHT. BROKEN. EMERGENCY LIGHT AT L1 DOOR BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND OPS CHECKED OK AS PER MM 33-50-01. (M)

All 58: https://openairdocs.org/deregistered/N8882Z-2010-07-20/reports.md

## 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 20001014037489I](https://openairdocs.org/incident/20001014037489I), Oct 14, 2000: Boeing 727225 (N8882Z), Buffalo, NY. (-23) On Saturday, October 14, 2000, during climb out from Buffalo niagara international airport (buf), a B-727-225, operated by delta airlines as flight 875,…

## Other aircraft with N8882Z

- [Cancelled 2022-10-01](https://openairdocs.org/deregistered/N8882Z-2022-10-01): DJI PHANTOM 3 PROFESSION, S/N P76DCH31A26314. Registration expired, pending cancellation. Owner: [Bain Ben Martin](https://openairdocs.org/faa-owner/BAIN%20BEN%20MARTIN), [Auburn, WA](https://openairdocs.org/faa-place/WA/Auburn)

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