# N507DA: 1977 Boeing 727-232, registration cancelled 2002-09-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 9, 2002
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21309
- Year built: 1977
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 13, 1977
- Certificate issued: June 17, 2002
- Last registry action: June 17, 2002
- Mode S code: A6543D
- Owner when cancelled: [Linc Aircraft LLC](https://openairdocs.org/faa-owner/LINC%20AIRCRAFT%20LLC)
- Location: [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne)
- Owner type: Corporation
- Owner's area on the map: 41.1001° N, 104.9249° W: Placed by OpenAirDocs at the center of ZIP code 82001, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N507DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=507DA
- Page: https://openairdocs.org/deregistered/N507DA-2002-09-09

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 727-232: https://openairdocs.org/model/boeing-727-232.md

## Service difficulty reports (85, newest 50)

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

- [SDR DL72L011286](https://openairdocs.org/sdr/DL72L011286), Aug 5, 2001: LIGHT. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHT BETWEEN EXTERIOR EMERGENCY EXIT DOORS INOP. RELAMPED. CHECKS OKAY
- [SDR DL72L011222](https://openairdocs.org/sdr/DL72L011222), Jul 24, 2001: LIGHT. INTERMITTENT. LEFT AFT DOOR EMERGENCY EXIT LIGHT INTERMITTENTLY BLINKING EMERGENCY EXIT OVER CENTER CABIN IS INTERMITTENTLY BLINKING. RELAMPED LIGHT OVER LEFT AFT DOOR AND CE
- [SDR DL72L011041](https://openairdocs.org/sdr/DL72L011041), Jun 22, 2001: CONTROLLER. FAILED. CABIN PRESSURIZATION FAILED IN AUTO, STBY, AND MAN AC OUTFLOW VALVE WAS CONTROLLABLE IN MAN DC ONLY. REPLACED CABIN PRESSURE CONTROLLER AFTER VERIFYING OLD CONT
- [SDR DL72L002298](https://openairdocs.org/sdr/DL72L002298), Nov 24, 2000: BATTERY. INOPERATIVE. IRREG / L1 DOOR EMERGENCY LIGHT WILL NOT GO BRIGHT . REPLACED BATTERY - OPN CKS NML
- [SDR DL72L002209](https://openairdocs.org/sdr/DL72L002209), Nov 8, 2000: LIGHT. BROKEN. EMERGENCY SEAT LIGHT ROW 10D LENS MISSING. REPLACED ASSY, CKS GOOD.
- [SDR DL72L002166](https://openairdocs.org/sdr/DL72L002166), Nov 4, 2000: BATTERY PACK. DISCHARGED. DURING EMERGENCY LIGHT CHECK OUT FOUND RT OUTSIDE OVERWING EXIT LIGHT OUT. REPLACED BATTERY PACK.
- [SDR DL72L002004](https://openairdocs.org/sdr/DL72L002004), Oct 13, 2000: LIGHT. INOPERATIVE. ON LAYOVER FOUND ESCAPE PATH LIGHTING INOP AT SEAT 3AB. FOUND PIN PULLED ON CABLE UNDER SEAT. RESET PIN, OPS CKS GOOD.
- [SDR DL72L001975](https://openairdocs.org/sdr/DL72L001975), Oct 10, 2000: MOUNT. CRACKED. ROUTINE HFEC BOLT HOLE INSPECTIONS OF THE NR 3 ENGINE PYLON FWD ENGINE MOUNT SUPPORT FITTING REVEALED A CRACK INDICATION IN HOLE G. THE CRACKING IS TYPICAL OF B
- [SDR DL72L001452](https://openairdocs.org/sdr/DL72L001452), Aug 1, 2000: BATTERY. INOPERATIVE. ON LAYOVER INSPECTION FOUND PORTABLE EMERGENCY EXIT LIGHT OVER THE L-2 DOOR NOT TESTING. REPLACED BATTERIES AND LIGHT OPERATION NORMAL.
- [SDR DL72L001262](https://openairdocs.org/sdr/DL72L001262), Jul 4, 2000: BATTERY. INOPERATIVE. L-2 DOOR EMERGENCY O/H EXIT SIGN INOP. REPLACED BATTERY PACK LIGHT, OPS CHECK NORM.
- [SDR DL72L001226](https://openairdocs.org/sdr/DL72L001226), Jun 28, 2000: LIGHT. INOPERATIVE. DURING LAYOVER, FOUND LEFT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. CHECKS GOOD PER MM.
- [SDR DL72L001225](https://openairdocs.org/sdr/DL72L001225), Jun 28, 2000: BATTERY PACK. INOPERATIVE. DURING LAYOVER, FOUND AFT OVERHEAD CEILING EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. CHECKS GOOD PER M/M
- [SDR DL72L000563](https://openairdocs.org/sdr/DL72L000563), Mar 22, 2000: SIGN. INOPERATIVE. RT OVERWING EMERG EXIT IDENTIFIER INOP ON STANDBY POWER CHECK. REPLACED RACK, OPERATION NML.
- [SDR DL72L000527](https://openairdocs.org/sdr/DL72L000527), Mar 17, 2000: SPAR. CRACKED. CRACKS IN AFT SPAR RAIL AT 21 AND 35 FROM I/B END OF FLAP. ALSO DOUBLER SHORT AT 30 FROM O/B END OF FLAP. CORRECTED ON SHOP ORDER NR 957610.
- [SDR DL72L000270](https://openairdocs.org/sdr/DL72L000270), Feb 7, 2000: FLAP TRACK. CORRODED. DURING OVERHAUL OF THE I/B FLAP, I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PADS AREAS. IN ADDITION, WEAR WAS FOUND AT THE F
- [SDR DL72L000256](https://openairdocs.org/sdr/DL72L000256), Feb 3, 2000: FLAP TRACK. CORRODED. DURING OVERHAUL OF THE I/B FLAP I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS AND TYPICAL WEAR WAS FOUND AT THE FWD A
- [SDR DL72L000280](https://openairdocs.org/sdr/DL72L000280), Jan 28, 2000: STRINGER. CRACKED. STRINGER 6 RT CRACKED VERT INTERIOR 4TH FRAME DOWN FROM 9504 RIB NR 2. BEGAN FABRICATED REPAIR PER M/M 55-30-0 PG 803. FINISHED FABRICATING REPAIR ANGLE PER M/M
- [SDR DL72L000259](https://openairdocs.org/sdr/DL72L000259), Jan 28, 2000: RIB. CRACKED. NR 5 SLAT NR 12 RIB CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72L000252](https://openairdocs.org/sdr/DL72L000252), Jan 28, 2000: SKIN. CRACKED. STOP DRILLED CRACK AND BEGAN FABRICATING REPAIR PER M/M 55-30-0 FIG 803. CHEM TREATED PER PS 900-2-4-1 NR 2. TREATED AND PAINTED PER PS 900-2 NR 5. OK TO INSTAL
- [SDR DL72L000567](https://openairdocs.org/sdr/DL72L000567), Jan 27, 2000: SKIN. CRACKED. NR 2 MIDFLAP AFT SPAR DOUBLER CRACKED TWO PLACES AND COVE SKIN CRACKED. REPAIRED PER M/M 57-52-0 FIGURE 802 AND FIGURE 809.
- [SDR DL72L000286](https://openairdocs.org/sdr/DL72L000286), Jan 27, 2000: ANGLE. WORN. SUPPORT ANGLE WORN VERT STAB LT SIDE JUST FWD OF SLIDING SEAL. REMOVED DAMAGED AREA AND DRILLED UP REPAIR PER SRM 55-30-6D. INSTALLED REPAIR PER SRM 55-30-6D.
- [SDR DL72L000197](https://openairdocs.org/sdr/DL72L000197), Jan 26, 2000: RIB. CRACKED. SLAT RIB NR 11 WAS CRACKED AT THE UPPER FWD END. INSTALLED A REPAIR DOUBLER PER 57-54-0 FIG 804.
- [SDR DL72L000196](https://openairdocs.org/sdr/DL72L000196), Jan 26, 2000: RIB. CRACKED. SLAT RIB WAS CRACK AT THE O/B LWR AFT END. REPAIRED PER MM 57-54-0 FIG 814.
- [SDR DL72L000238](https://openairdocs.org/sdr/DL72L000238), Jan 25, 2000: SKIN. CRACKED. ANTI-ICE SKIN CRACKED AT 4 LOCATIONS. INSTALLED DOUBLER PER MM 57-54-0.
- [SDR DL72L000195](https://openairdocs.org/sdr/DL72L000195), Jan 24, 2000: RIB. CRACKED. SLAT RIB WAS CRACKED AT LWR AFT END NR 2 RIB. INSTALLED A REPAIR DOUBLER PER MM 57-54-0 FIG 814.
- [SDR DL72L000194](https://openairdocs.org/sdr/DL72L000194), Jan 24, 2000: SKIN. CRACKED. SLAT CRACKED. INSTALLED REPAIR DOUBLER PER MM 57-54-0 FIG 814.
- [SDR DL72L992508](https://openairdocs.org/sdr/DL72L992508), Nov 13, 1999: ANGLE. CORRODED. ON HEAVY WEIGHT HUSH-KIT MOD, FOUND RT AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED RT CHORD ANGLE WITH ONE OF NEW MFG.
- [SDR DL72L992507](https://openairdocs.org/sdr/DL72L992507), Nov 12, 1999: ANGLE. CORRODED. ON HEAVY WEIGHT HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT SUPPORT LT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT CHORD ANGLE WITH ONE OF NEW MFG.
- [SDR DL72L991886](https://openairdocs.org/sdr/DL72L991886), Aug 23, 1999: BRACKET. CRACKED. FOUND ON A1 LETTER CK, NR 1 L/E FLAP ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72L991885](https://openairdocs.org/sdr/DL72L991885), Aug 23, 1999: SKIN. CRACKED. FOUND AT A-1 LETTER CK, .5 INCH CRACK IN EMPENNAGE SKIN RT SIDE STA 1234 + STR 22. REPAIRED PER SRM 53-30-3 FIG 25.
- [SDR DL72L991895](https://openairdocs.org/sdr/DL72L991895), Aug 20, 1999: TRACK. CORRODED. NR 5 INB'D FLAP TRACK AD 90-07-05 AND 90-06-09 TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUGS. AUTHORIZED MACHINING CORROSION AND
- [SDR DL72L991073](https://openairdocs.org/sdr/DL72L991073), May 15, 1999: RETURN LINE. CRACKED. SYS A HYD QTY IND DROPPED TO ZERO QTY APPROX ONE HR AND 20 MINS INTO FLT. NR 1 ENG HYD LOW PRESS LIGHT ILLUMINATED. CHECKLIST PROCEDURE INITIATED LANDING UNEVEN
- [SDR DL72L990921](https://openairdocs.org/sdr/DL72L990921), Apr 27, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 481-681, STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS 
- [SDR DL72L990917](https://openairdocs.org/sdr/DL72L990917), Apr 27, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 360-481 STRINGER 4L, SKIN LAP SPLICE, CRACK REPAIR. INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4L SKI
- [SDR DL72L990916](https://openairdocs.org/sdr/DL72L990916), Apr 27, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 360-480 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS I
- [SDR DL72L990915](https://openairdocs.org/sdr/DL72L990915), Apr 27, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 680-740 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS I
- [SDR DL72L982350](https://openairdocs.org/sdr/DL72L982350), Nov 14, 1998: LIGHT. INOP. L-1 AND FWD AISLE AREA EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN THE L-1 DOOR POS AND REPLACED LIGHT ASSY FOR THE FWD AISLE EMERGENCY LIGHT.
- [SDR DL72L981898](https://openairdocs.org/sdr/DL72L981898), Sep 13, 1998: WEB. CRACKED. FOUND ON MV2 CK, .5 INCH CRACK IN THE STA 1309 WEB LEFT SIDE ABOVE THE S DUCT. REPAIRED PER SRM 53-10-4.
- [SDR DL72L981897](https://openairdocs.org/sdr/DL72L981897), Sep 13, 1998: WEB. CRACKED. FOUND ON MV2 CK, 1 INCH AND .5 INCH CRACKS FOUND IN STA 1309 WEB RT SIDE ABOVE S DUCT. REPAIRED PER SRM 53-10-4.
- [SDR DL72L981909](https://openairdocs.org/sdr/DL72L981909), Sep 12, 1998: SKIN. CORRODED. THE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL AREAS OF CORROSION AT THE S-26R LAP SPLICE BETWEEN FS 700 AND 720C. THE CORRODED AREAS WERE LOCALLY CUT OUT AND L
- [SDR DL72L981850](https://openairdocs.org/sdr/DL72L981850), Sep 2, 1998: SKIN. CORRODED. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 700 BETWEEN STR 28R AND 28L. THE CORROSION WAS CUT OUT WITH A 9 X 6.5 CUTOUT. THE CUTOUT WAS ADJACENT TO AN EXISTING 
- [SDR DL72L981873](https://openairdocs.org/sdr/DL72L981873), Aug 28, 1998: WEB. CRACKED. A .375 INCH CRACK IN TORQUE BOX VERTICAL WEB STA 1223 LT SIDE, ABOVE STAIRS CLOSE OUT PANEL. REPAIRED PER MM 53-11-0.
- [SDR DL72L981895](https://openairdocs.org/sdr/DL72L981895), Aug 26, 1998: ANGLE. CORROSION. FOUND DURING MV2 CORROSION VISIT NRC 154, WHILE WORKING NRC 91 FOUND RT SKIN SUPPORT ANGLE CORRODED UNDER STR 27R STA 740. REPLACED SKIN SUPPORT ANGLE PER M/M 5
- [SDR DL72L981890](https://openairdocs.org/sdr/DL72L981890), Aug 26, 1998: STIFFENER. CRACKED. A .625 INCH CRACK IN SPAR STIFFENER AT NR 5 SLAT ACTUATOR INBD ATTACH FITTING. REMOVED OLD STIFFENER. DRILLED UP STIFFENER PER M/M 57-20-21 PG 813.
- [SDR DL72L981872](https://openairdocs.org/sdr/DL72L981872), Aug 26, 1998: FRAME. CRACKED. 2 INCH CRACK ON R-1 DOOR AFT FRAME AT LOWER CORNER. REPAIRED PER MM 52-12-0 FIG 804.
- [SDR DL72L981547](https://openairdocs.org/sdr/DL72L981547), Jul 24, 1998: TRANSFORMER. FAILED. STRONG ELECTRICAL SMELL IN COCKPIT AND FWD CABIN FL 310. FOUND ESSENTIAL T/R AT FAULT. SWAPPED WITH NR 2 T/R AND PUT NR 2 T/R ON MCO.
- [SDR DL72L981530](https://openairdocs.org/sdr/DL72L981530), Jul 22, 1998: SKIN. DELAMINATED. ON T/C, FOUND LEFT O/B AILERON DELAMINATED BEYOND SRM LIMITS. REPLACED LT O/B AILERON TRAILING EDGE WEDGE.
- [SDR DL72L981486](https://openairdocs.org/sdr/DL72L981486), Jul 16, 1998: POWER PACK. INOPERATIVE. EMERGENCY TRACK LIGHTING FROM ROW 27 AFT INOP. REPLACED POWER PACK.
- [SDR DL72L981458](https://openairdocs.org/sdr/DL72L981458), Jul 13, 1998: BATTERY. DISCHARGED. AFT CABIN EMER TRACK LIGHT SECTION INOP. REPLACED BATTERY PACK AND CHARGER, OPS CK OK.
- [SDR DL72L981450](https://openairdocs.org/sdr/DL72L981450), Jul 13, 1998: POWER SUPPLY. INOPERATIVE. AFT FLOOR EMERGENCY LIGHTS DID NOT GO ON WHEN TESTED. REPLACED POWER SUPPLY.

All 85: https://openairdocs.org/deregistered/N507DA-2002-09-09/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 19790829033299I](https://openairdocs.org/incident/19790829033299I), Aug 29, 1979: Boeing 727232 (N507DA), New Orleans, LA. Za zk flight returned after fire warning. Found brown anti-ice duct.

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