# N492DA: Boeing 727-232, registration cancelled 2000-06-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 22, 2000
- Status when cancelled: Sale reported
- Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 21061
- Type of aircraft: Fixed wing multi engine
- Last registry action: February 14, 2000
- Mode S code: A617D2
- Location: [Aurora, CO](https://openairdocs.org/faa-place/CO/Aurora)
- Owner type: Individual
- Owner's area on the map: 39.6636° N, 104.8378° W: Placed by OpenAirDocs at the center of ZIP code 80014, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N492DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=492DA
- Page: https://openairdocs.org/deregistered/N492DA-2000-06-22

From the FAA registry file of October 28, 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 727-232: https://openairdocs.org/model/boeing-727-232.md

## Service difficulty reports (82, newest 50)

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

- [SDR DL72S992119](https://openairdocs.org/sdr/DL72S992119), Sep 21, 1999: SKIN. CRACKED. TPA LTR CHK D-2 09/21/99, .625 INCH CRACK AT FUSE SKIN STA 1250 AND STR 21R. REPAIRED PER SRM 53-30-03 FIG 25 AND ERA 368334-14.
- [SDR DL72S992117](https://openairdocs.org/sdr/DL72S992117), Sep 21, 1999: WEB. CRACKED. ONE CRACK ON VERT WEB ABOVE S-DUCT AT STA 1303 ON LT SIDE AT STR CUTOUT. REPAIRED PER SRM 53-10-4.
- [SDR DL72S992116](https://openairdocs.org/sdr/DL72S992116), Sep 21, 1999: SKIN. CRACKED. TPA LTR CHK D-2 9/21/99, 1 CRACK ON S-DUCT HOUSING RT SIDE AT UPPER END OF PANEL 9524. REPAIRED PER MM 54-30-0.
- [SDR DL72S992115](https://openairdocs.org/sdr/DL72S992115), Sep 21, 1999: CASTING. CRACKED. VERT STAB LT TENSION TIE BOLT CASTING CRACKED I/B SIDE. REPLACED FITTING PER BAC DWG 65-17509 REV M. TPA LTR CHK D-2 09/21/99.
- [SDR DL72S991797](https://openairdocs.org/sdr/DL72S991797), Aug 11, 1999: BATTERY PACK. DISCHARGED. RT OVERWING EMERGENCY LIGHTS WERE INOP. REPLACED BATTERY CHARGER AND BATTERY PACK. OPS NOW NML.
- [SDR DL72S990703](https://openairdocs.org/sdr/DL72S990703), Mar 25, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION
- [SDR DL72S990311](https://openairdocs.org/sdr/DL72S990311), Feb 16, 1999: FRAME. CRACKED. FOUND ON D1 LETTER CK AFT ENTRY DOOR FRAME CUTOUT CRACKED RT SIDE APPROX 10 INCHES FROM THE TOP. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990310](https://openairdocs.org/sdr/DL72S990310), Feb 16, 1999: FRAME. CRACKED. FOUND ON D1 LETTER CK AFT ENTRY DOOR FRAME CUTOUT CRACKED LEFT SIDE APPROX 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 53-10-9.
- [SDR DL72S980656](https://openairdocs.org/sdr/DL72S980656), Mar 22, 1998: BEAR STRAP. CRACKED. FUSELAGE SKIN R1 DOOR SURROUND UPPER HINGE CUTOUT, REPAIR FOR CRACK IN DOOR SURROUND BEAR STRAP. THE INTERNAL R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) 
- [SDR DL72S980281](https://openairdocs.org/sdr/DL72S980281), Jan 22, 1998: STIFFENERS. CRACKED. 2 EA WING L/E SPAR STIFFENERS CRACKED AT NR 4 L/E SLAT INBD TRACK ROLLER FITTING ATTACH. REPLACED STIFFENERS PER M/M 57-20-21.
- [SDR DL72S980279](https://openairdocs.org/sdr/DL72S980279), Jan 22, 1998: STIFFENERS. CRACKED. 2 EA WING L/E SPAR STIFFENERS CRACKED NR 3 L/E SLAT OUTBD TRACK ROLLER FITTING ATTACH. INSTALLED NEW ANGLES PER M/M 57-20-21.
- [SDR DL72S972279](https://openairdocs.org/sdr/DL72S972279), Nov 5, 1997: PWR SUPPLY. INOPERATIVE. EMERGENCY TRACK LIGHTS INOP. REPAIRED SHORTED WIRES AND REPLACED POWER SUPPLY.
- [SDR DL72S971844](https://openairdocs.org/sdr/DL72S971844), Sep 21, 1997: SMOKE DETECTOR. INOPERATIVE. AFT RIGHT SMOKE DETECTOR WILL NOT TEST. REPLACED DETECTOR, CHECKS NORMAL.
- [SDR DL72S971737](https://openairdocs.org/sdr/DL72S971737), Sep 5, 1997: BATTERY PACK. DISCHARGED. EMERGENCY TRACK LIGHTING INOP FROM ROW 26 THUR 36. REPLACED BATTERY PACK, SYSTEM CHECKS NORMAL.
- [SDR DL72S971496](https://openairdocs.org/sdr/DL72S971496), Jul 29, 1997: BULB. FAILED. EMER TRACK LIGHTS INOP AT ROW 21 AND ROW 25. REPLACED BULBS AND LENSES.
- [SDR DL72S970927](https://openairdocs.org/sdr/DL72S970927), May 14, 1997: WEB. CRACKED. 1.75 INCH CRACK UPPER RT TORQUE BOX VERT WEB STA 1213. REPAIRED PER M/M 53-11-0 PG 832.
- [SDR DL72S970363](https://openairdocs.org/sdr/DL72S970363), Feb 26, 1997: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT, EXTERIOR LOWER RT ON AFT CARGO DOOR, INOP. REPLACED BATTERY PACK. EMERGENCY LIGHTS OPS CHK OK.
- [SDR DL72S962784](https://openairdocs.org/sdr/DL72S962784), Dec 29, 1996: BATTERY. DISCHARGED. AIRSTAIRS EMER LIGHTS INOP. REPLACED BATT, OPS CK GOOD.
- [SDR DL72S962432](https://openairdocs.org/sdr/DL72S962432), Sep 3, 1996: SPAR. CRACKED. REAR SPAR WAS FOUND CRACKED. REPAIRED SPAR PER SRM 51-40-3 FIG 1.
- [SDR DL72S960760](https://openairdocs.org/sdr/DL72S960760), Apr 3, 1996: WEB. CRACKED. FOUND ON A2 LETTER CHECK, .375 INCH CRACK IN LT TORQUE BOX WEB STA 1263. REPAIRED PER MM 53-11-0.
- [SDR DL72S953556](https://openairdocs.org/sdr/DL72S953556), Aug 30, 1995: STIFFENER. CRACKED. DURING A-1 LETTER CHECK, O/B LEADING EDGE SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 2 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21.
- [SDR DL72S953555](https://openairdocs.org/sdr/DL72S953555), Aug 30, 1995: STIFFENER. CRACKED. DURING A-1 LETTER CHECK, FOUND I/B SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 3 SLAT I/B TRACK. O/B SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 3 SLAT I/B TRACK. REPAI
- [SDR DL72S953554](https://openairdocs.org/sdr/DL72S953554), Aug 30, 1995: SKIN. CRACKED. DURING A-1 LETTER CHECK, FOUND COVE SKIN SUPPORT ANGLE CRACKED 1 INCH FROM O/B END ON NR 4 SLAT. REPAIRED PER MM 57-54-0.
- [SDR DL72S953553](https://openairdocs.org/sdr/DL72S953553), Aug 30, 1995: SKIN. CRACKED. DURING A-1 LETTER CHECK, FOUND COVE SKIN SUPPORT ANGLE CRACKED .3750 INCH UNDER TAI DUCT ON NR 2 SLAT. REPAIRED PER M/M 57-54-0 AND ID PER PS 900-5-1 NR 4.
- [SDR DL72S953385](https://openairdocs.org/sdr/DL72S953385), Aug 13, 1995: ACTUATOR. FAILED. AT CRUISE LOSS A-HYD SYS QTY AND PRESS NR 4 SLAT DID NOT EXTEND ON LANDING. REPLACED NR 4 SLAT ACTUATOR, NR 1 AND 2 ENG DRIVEN HYD PUMPS AND FILTERS.
- [SDR DL72S951626](https://openairdocs.org/sdr/DL72S951626), Apr 20, 1995: ANGLE. DENTED. NR 3 MID FLAP AFT SPAR LOWER ANGLE DENTED APPROX 59 INCHES FROM I/B END. INSTALLED DOUBLER AND SPAR PER MM 57-52-0.
- [SDR DL72S951625](https://openairdocs.org/sdr/DL72S951625), Apr 20, 1995: HOUSING. CORROSION. NR 3 MID FLAP O/B CARRIAGE SUPPORT HOUSING LOWER SURFACE, TWO FASTENER HOLES CORRODED. REAMED HOLES TO .312 TREATED AND INSTALLED BUSHING.
- [SDR DL72S951623](https://openairdocs.org/sdr/DL72S951623), Apr 20, 1995: FITTING. CORROISON. NR 3 MID FLAP O/B CARRIAGE FITTING LOWER SURFACE HAS CORROSION IN ONE HOLE. FOUND AT SHOP INSPECTION, REAMED HOLE TO .312 TREATED AND INSTALLED BUSHING.
- [SDR DL72S950750](https://openairdocs.org/sdr/DL72S950750), Feb 19, 1995: STRINGER. CORRODED. STR 27L HAS SEVERAL AREAS OF CORROSION AROUND FASTENERS FROM STA 550 TO 590 FOUND AT HMV. REPAIRED PER SRM 53-10-3
- [SDR DL72S950589](https://openairdocs.org/sdr/DL72S950589), Feb 4, 1995: SKIN. PUNCTURED. DURING HMV, FOUND C-2 DOOR HAS HOLE PUNCHED IN IT ABOVE AFT LOWER CORNER, REPAIRED PER SRM 52-00-3 FIG 3.
- [SDR DL72S950721](https://openairdocs.org/sdr/DL72S950721), Feb 3, 1995: SEAT TRACK. CORROSION. DURING HMV, FOUND SEAT TRACK CORROSION AT STA 344 LEFT I/B TRACK, REPAIRED BY REPLACING SEAT TRACK LT I/B FROM STA 380 FWD PER MM 53-20-11 FIG 802.
- [SDR DL72S951857](https://openairdocs.org/sdr/DL72S951857), Feb 2, 1995: SKIN. DELAMINATED. NR 2 MID FLAP DURING HMV SHOP INSP, WAS FOUND TO BE DELAMINATED FROM 0 TO 3 FROM O/B END AND POTTING COMPOUND DETERIOIATED. REPAIRD PER SRM 57-50-4 .
- [SDR DL72S950751](https://openairdocs.org/sdr/DL72S950751), Feb 2, 1995: FLOOR BEAM. CORRODED. STA 360 FLOOR BEAM NUT CLIP HOLES CORRODED MANY PLACES FOUND AT HMV. REPAIRED PER SRM 53-10-8 FIG 1.
- [SDR DL72S950689](https://openairdocs.org/sdr/DL72S950689), Feb 2, 1995: RIB. CRACKED. AT HMV, FOUND NR 2 LEADING EDGE SLAT WITH CRACKED RIB AT 2ND LOCATION FROM THE OUTBD END OF SLAT. REPAIRED PER SRM 57-54-0 PG 819.
- [SDR DL72S950551](https://openairdocs.org/sdr/DL72S950551), Feb 2, 1995: FLOOR BEAM. CORRODED. AT HMV, FOUND FS 400 CABIN FLOOR BEAM UPPER CAP WITH CORROSION DAMAGE ALONG ITS LENGTH. REPAIRED PER SRM 53-10-8 FIG 3 AT RBL 10 TO LBL 10 AND SRM 53-20-11.
- [SDR DL72S950550](https://openairdocs.org/sdr/DL72S950550), Feb 2, 1995: FLOOR BEAM. CORRODED. AT HMV, FOUND FS 1070 CABIN FLOOR SUPPORT BEAM UPPER CAP CORRODED, OUTBOARD OF RT OUTBOARD SEAT TRACK. REPAIRED PER MM 53-20-11 FIG 804 A.
- [SDR DL72S950501](https://openairdocs.org/sdr/DL72S950501), Feb 2, 1995: CLIP. CRACKED. DURING HMV, FOUND SKIN CLIP CRACKED AT FS 1050 BETWEEN STR 30 AND 29L, REPAIRED PER M/M 53-11-0 FIG 815.
- [SDR DL72S950495](https://openairdocs.org/sdr/DL72S950495), Feb 2, 1995: CLIP. CORRODED. AT HMV, FOUND FS 950F FRAME TO SKIN SHEAR TIE CORRODED AT STRINGER 29R. REPAIRED PER MM 53-11-0 FIG 815.
- [SDR DL72S950478](https://openairdocs.org/sdr/DL72S950478), Feb 2, 1995: CLIP. BROKEN. AT HMV, FOUND FS 980 FRAME TO SKIN CLIP CRACKED BETWEEN STRINGERS 29R AND 30. REPAIRED PER MM 53-11-0 FIG 815.
- [SDR DL72S950477](https://openairdocs.org/sdr/DL72S950477), Feb 2, 1995: CLIP. CRACKED. AT HMV, FOUND FS 950A FRAME TO SKIN SHEAR TIE CRACKED BETWEEN STRINGERS 28-27R. REPAIRED PER MM 53-11-0 FIG 815.
- [SDR DL72S950696](https://openairdocs.org/sdr/DL72S950696), Feb 1, 1995: FRAME. CRACKED. FWD B/B STA 600 FRAME CRACKED AT STR CLIPS STR 23 AND 24 LEFT. REPAIRED PER SRM 53-10-4 PG 88-90. DAMAGE FOUND AND REPAIRED AT HMV VISIT.
- [SDR DL72S950695](https://openairdocs.org/sdr/DL72S950695), Feb 1, 1995: RIB. CRACKED. AT HMV, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIBS JUST INBOARD OF THE INBOARD SLAT TRACK AND OUTBOARD OF TAI DUCT. REPAIRED PER MM 57-54-0 PG 807.
- [SDR DL72S950694](https://openairdocs.org/sdr/DL72S950694), Feb 1, 1995: RIB. CRACKED. AT HMV, FOUND NR 3 L/E SLAT WITH RIBS NR 1 AND NR 2 CRACKED. REPAIRED PER SRM 57-50-3 FIG 9 AND MM 57-54-0 PG 819.
- [SDR DL72S950691](https://openairdocs.org/sdr/DL72S950691), Feb 1, 1995: CHANNELS. WORN. CHANNELS WORN FWD B/B AFT BULKHEAD TWO VERTICAL SUPPORT CHANNELS ARE WORN (LOC OVER STG 26L AND 26R) AT FLEX JOINTS. ALSO, RIVETS SHEARED LEFT SUPPORT AT CEILIN
- [SDR DL72S950690](https://openairdocs.org/sdr/DL72S950690), Feb 1, 1995: RIB. CRACKED. AT HMV, FOUND RT WING NR 6 SLAT WITH THE 2ND RIB FROM THE INBOARD END CRACKED AND 2 CRACKS IN RIB ON THE OUTBARD SIDE OF THE INBOARD TRACK. REPAIRED PER SRM 57-
- [SDR DL72S950622](https://openairdocs.org/sdr/DL72S950622), Feb 1, 1995: STRINGER. CRACKED. AT HMV, FOUND FUSELAGE STRINGER 7R, CRACKED FORWARD OF FS 560, REPAIRED PER SRM 51-10-3.
- [SDR DL72S950599](https://openairdocs.org/sdr/DL72S950599), Feb 1, 1995: STRINGER. CRACKED. AT HMV, FOUND STRINGER 9 LT CRACKED AT 3RD BULHEAD UP FROM ACCESS PANEL INSIDE VERTICAL STABILIZER. REPAIRED PER SRM 55.
- [SDR DL72S950598](https://openairdocs.org/sdr/DL72S950598), Feb 1, 1995: STRINGER. CRACKED. AT HMV, FOUND STRINGER 4 LT. CRACKED AT 5TH BULKHEAD FROM ACCESS PANEL IN VERTICAL STABILIZER. REPAIRED PER SRM 55.
- [SDR DL72S950596](https://openairdocs.org/sdr/DL72S950596), Feb 1, 1995: RIB. CRACKED. RIB CRACKED, 3RD RIB OUTBOARD OF ACTUATOR MOUNT ON NR 6 L/E SLAT. FOUND DURING INSP AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 819.
- [SDR DL72S950595](https://openairdocs.org/sdr/DL72S950595), Feb 1, 1995: ANGLE. CRACKED. LOWER CHORD ANGLE CRACKED AT 2ND RIB O/B OF ACTUATOR FITTING ON NR 6 L/E SLAT. FOUND DURING INSP AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 816.

All 82: https://openairdocs.org/deregistered/N492DA-2000-06-22/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 19950813029399I](https://openairdocs.org/incident/19950813029399I), Aug 13, 1995: Boeing 727232 (N492DA), Rochester, NY. Hydraulic and NR4 leading edge slat problems landing. Towed to gate. Replace NR4 slat actuator a pump and filters.

## Other aircraft with N492DA

- [Registered now](https://openairdocs.org/aircraft/N492DA): Cirrus Design SR20, S/N 1838, built 2007

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