# N6813: 1968 Boeing 727-223, registration cancelled 2006-06-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 22, 2006 - Status when cancelled: Valid registration - Airframe: [Boeing 727-223](https://openairdocs.org/model/boeing-727-223) (registry code 1384074) - 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: 19488 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 11, 1968 - Certificate issued: May 21, 2004 - Last registry action: May 21, 2004 - Mode S code: A909AF - Owner when cancelled: [Aircorp Inc](https://openairdocs.org/faa-owner/AIRCORP%20INC) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: Corporation - Owner's area on the map: 32.7883° N, 96.7996° W: Placed by OpenAirDocs at the center of ZIP code 75201, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N6813 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6813 - Page: https://openairdocs.org/deregistered/N6813-2006-06-22 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 727-223: https://openairdocs.org/model/boeing-727-223.md ## Service difficulty reports (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EISA20010146](https://openairdocs.org/sdr/EISA20010146), Dec 12, 2001: STRUCTURE. CORRODED. CHORD CORRODED BS 312-348 LBL 14.6, WL 169. FOUND ON CPCP C53-111-03 PAGE 4 N/R CARD 401 WRITTEN. REMOVED CHORD IAW B727 SRM 51-30-2, INSTALLED NEW CHORD IAW B7 - [SDR EISA20010145](https://openairdocs.org/sdr/EISA20010145), Dec 12, 2001: ANGLE. CORRODED. ANGLE IN R/H W/W CORRODED, BS 870 RBL 48.0FOUND DURING CPCP C53-100-01 PAGE 1, N/R CARD 411 WRITTENCORRECTIVE ACTION:REMOVED ANGLE, FABRICATED NEW ANGLE FROM 70 - [SDR EISA20010144](https://openairdocs.org/sdr/EISA20010144), Dec 12, 2001: STIFFENER. CORRODED. VERTICAL STIFFENER CORRODED BS 336 RBL 14.6 BELOW FLOOR PAN.FOUND ON CPCP C53-111-03 PAGE 4, N/R CARD 405 WRITTENCORRECTIVE ACTION:REMOVED AND REPLACED STIFFENE - [SDR EISA20010143](https://openairdocs.org/sdr/EISA20010143), Dec 12, 2001: FRAME. CORRODED. NOSE WHEEL WELL STA 296, LBL 12 UPPER FRAME CORRODED. FOUND ON CPCP CHECK. REMOVED AND REPLACED FRAME IAW B727 SRM 51-10-1 & 51-30-2. - [SDR EISA20010142](https://openairdocs.org/sdr/EISA20010142), Dec 12, 2001: FRAME. CORRODED. NOSE WHEEL WELL STA 296, RBL 12 UPPER CHORD CORRODED. FOUND ON CPCP CHECK. REMOVED AND REPLACED FRAME IAW B727 SRM 51-10-1 & 51-30-2. - [SDR EISA20010141](https://openairdocs.org/sdr/EISA20010141), Dec 12, 2001: STIFFENER. CRACKED. L/H MLG W/W BS 870 LBL 45 VERTICAL STIFFENER CRACKED.FOUND ON CPCP INSP. C-53-100-01 PAGE 1, N/R CARD 410 WRITTENCORRECTIVE ACTION:FABRICATED AND INSTALLED REPA - [SDR EISA20010140](https://openairdocs.org/sdr/EISA20010140), Dec 12, 2001: PANEL. CORRODED. NOSE W/W PANEL BS 330 TO 350 STR L27 CORRODEDFOUND ON CPCP C53-100-01 PAGE 1, N/R CARD 444 WRITTENCORRECTIVE ACTION:REMOVED CORROSION IAW B727 SRM 51-10-6 FABRI - [SDR EISA20010139](https://openairdocs.org/sdr/EISA20010139), Dec 12, 2001: SKIN. CRACKED. FUSELAGE SKIN BS 211, STR 25R GOUGED AND CRACKED AT FWD E/E DOOR CUTOUT.FOUND ON SERVICE CHECK--N/R CARD 431 WRITTENCORRECTIVE ACTION: STOP DRILLED CRACK IAW B7 - [SDR EISA20010138](https://openairdocs.org/sdr/EISA20010138), Dec 12, 2001: SKIN. CORRODED. FUSELAGE SKIN CORRODED AT BS 336, STR 25R.WRITTEN FROM NON-ROUTINE CARD 405 FROM CPC C53-111-03 PAGE 4--N/R CARD 435 WRITTENCORRECTIVE ACTION:REMOVED DAMAGED SK - [SDR EISA20010125](https://openairdocs.org/sdr/EISA20010125), Oct 11, 2001: DOOR. OUT OF ADJ. F/E PANEL MAIN CARGO DOOR WARNING LIGHT ILLUMINATE, PRESSURIZATION NORMAL, ALT FL310 PSID 8.0. MAIN CARGO DOOR PANEL, DOOR WARNING LIGHT, VENT DOOR OPEN, AND MA - [SDR EISA20010124](https://openairdocs.org/sdr/EISA20010124), Oct 5, 2001: SWITCH. INOPERATIVE. DURING CLIMB, RED MCD LIGHT ALONG WITH AMBER VENT DOOR NOT CLOSED ILLUM. ALONG WITH UNSCHEDULED CLIMB IN CABIN ALT. ACC. AERONAUTICAL MCD WARNING ILLUM. IN FLT. - [SDR EISA20010094](https://openairdocs.org/sdr/EISA20010094), Jun 8, 2001: RIVET. SHEARED. RIVET MIGRATED AT 1183 BULKHEAD AFT LT. SIDE 12" O/B OF DOOR CUT-OUT & 10" BELOW DOOR TOP (EO)FOUND DURING B-2 CHECKCORRECTIVE ACTION:CUT-OFF HEAD OF TRAPPED (M - [SDR EISA20000145](https://openairdocs.org/sdr/EISA20000145), Sep 7, 2000: CONTROLLER. FLUCTUATES. NR 1 GENERATOR UNDERVOLTAGE LIGHT ILLUMINATED, TRIPPED NR 1 BUS TIE AT 5000 FT, AIR TURNBACK. REMOVED AND REPLACED NR 1 GENERATOR LOAD CONTROLLER AND GCU, OPS C - [SDR EISA20000059](https://openairdocs.org/sdr/EISA20000059), Jul 27, 2000: UPLOCK SWITCH. FAILED. AFTER GEAR EXTENSION, NOSE GEAR RED LIGHT REMAINED ILLUMINATED, AS WELL AS AFTER MANUAL GEAR EXTENSION. FOUND BROKEN WIRE ON NOSE GEAR UPPER LOCK SWITCH, RE-CRI - [SDR EISA99209](https://openairdocs.org/sdr/EISA99209), Oct 19, 1999: MECHANISM. FAILED. AIRCRAFT LOST PRESSURIZATION, DIVERTED TO BRU AT 0200Z) UNABLE TO OPEN L1 DOOR. (M) - [SDR EISA99162](https://openairdocs.org/sdr/EISA99162), Aug 30, 1999: BATTERY. DISCHARGED. ON LANDING, APU FAILED TO START FOUND BATTERY VOLTAGE AT 4, BATTERY CHARGER C/B POPPED. BATTERY WARMS TO TOUCH. NOTICED SMOKE IN COCKPIT. REMOVED AND REPLACED B - [SDR EISA99124](https://openairdocs.org/sdr/EISA99124), May 30, 1999: COMPRESSOR. STALLED. NR 2 ENGINE COMPRESSOR STALLS. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK GOOD. REPLACED 13TH STAGE SURGE BLEED VALVE. (M) - [SDR EISA99028](https://openairdocs.org/sdr/EISA99028), Feb 16, 1999: WIRE. BROKEN. NOSE GEAR RED UNSAFE LIGHT ON AND GREEN LIGHT ON WITH GEAR EXTENDED. REPAIRED GROUND WIRE FROM LOCK SWITCH. (M) - [SDR EISA99027](https://openairdocs.org/sdr/EISA99027), Feb 16, 1999: SWITCH. FAILED. AFTER NOSE GEAR EXTENSION, BOTH GREEN AND RED ILLUMINATED. AFTER MAIN GEAR EXTENDED, ONLY GREEN LIGHT ON. REMOVED AND REPLACED NOSE GEAR LOCK SWITCH, PERFORMED - [SDR EISA99021](https://openairdocs.org/sdr/EISA99021), Jan 19, 1999: DUCT. CRACKED. LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED WHILE ENGINE ANTI-ICE WING ANTI-ICE WERE IN USE. CLOSING THE WING ANTI-ICE AND A CO-INCIDENTAL REDUCTION IN POWER DURI - [SDR EISA98284](https://openairdocs.org/sdr/EISA98284), Dec 4, 1998: OVERHEAT LIGHT. ILLUMINATED. SHORTLY AFTER SELECTING WING ANTI-ICE ON, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, EXTINGUISHED AFTER TURNING OFF ENGINE NR 3 ANTI-ICE. ENGINE NR 1 OPENED - [SDR EISA98213](https://openairdocs.org/sdr/EISA98213), Aug 27, 1998: INDICATOR. MALFUNCTIONED. NR 2 ENGINE OIL TEMP EXCEEDED RED LINE DURING FLIGHT. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED PER FLIGHT MANUAL. FOUND NR 2 OIL TEMP BULB GROUND WIRE BROKEN - [SDR EISA97278](https://openairdocs.org/sdr/EISA97278), Dec 12, 1997: ANGLE. CORRODED. MAIN CABIN, FLOOR SUPPORT FS 400-420 HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-04. (M) - [SDR EISA97277](https://openairdocs.org/sdr/EISA97277), Dec 12, 1997: DOUBLER. CRACKED. LT WING, OUTBOARD MID FLAP, LOWER FORWARD SKIN HAS SEVERAL CRACKS ON DOUBLER AT OUTBOARD FORE FLAP TRACK AREA. FABRICATED DOUBLER AND FILLER PER SRM 51-40-03. ( - [SDR EISA97276](https://openairdocs.org/sdr/EISA97276), Dec 12, 1997: SKIN. DELAMINATED. RT WING, NR 7 SPOILER DELAMINATED AT FWD CENTER SECTION. REPAIRED SPOILER DELAMINATION PER SRM 51-40-06 AND 51-40-09. (M) - [SDR EISA97275](https://openairdocs.org/sdr/EISA97275), Dec 12, 1997: SKIN. CRACKED. LEFT WING LEADING EDGE UPPER SURFACE EXTERIOR SKIN HAS APPROX 0 INCH CRACK AT WS 450. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-1 AND 51-30-02. (M) - [SDR EISA97274](https://openairdocs.org/sdr/EISA97274), Dec 12, 1997: STRINGER. CRACKED. CIRCULAR CRACK BETWEEN TWO FAST ON STRINGER 24R AT FS 335. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-1 AND 51-30-02. (M) - [SDR EISA97273](https://openairdocs.org/sdr/EISA97273), Dec 12, 1997: FLOORBEAM. CORRODED. MAIN CABIN, FLOOR BEAM FS 320 HAS CORROSION ON TOP CAP. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-08. (M) - [SDR EISA97272](https://openairdocs.org/sdr/EISA97272), Dec 12, 1997: FLOORBEAM. CORRODED. MAIN CABIN, FLOORBEAM FS 360 HAS CORROSION ON TOP CAP. REMOVED AND REPLACED TO CAP PER SRM 53-10-08. (M) - [SDR EISA97271](https://openairdocs.org/sdr/EISA97271), Dec 12, 1997: ANGLE. CORRODED. MAIN CABIN, OUTBOARD ANGLE RIGHT SIDE HAS CORROSION AT FS 460. REMOVED AND REPLACED ANGLE PER SRM 51-10-06. (M) - [SDR EISA97270](https://openairdocs.org/sdr/EISA97270), Dec 12, 1997: INTERCOSTAL. CRACKED. MAIN CABIN, INTERCOSTAL AT FS 740 BL 20L HAS PREVIOUS REPAIR DOUBLER WITH 2 INCH LONG CRACK. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER PER S - [SDR EISA97269](https://openairdocs.org/sdr/EISA97269), Dec 12, 1997: SUPPORT. CRACKED. MAIN CABIN, SUPPORT WEB UPPER FLANGE HAS SEVERAL CRACKS FROM FS 720 TO 720B BL 0. UPPER FLANGE REMOVED DUE TO TRACK INSTALLATION FOR CARGO MOD, REF STC SA-1998- - [SDR EISA97268](https://openairdocs.org/sdr/EISA97268), Dec 12, 1997: SUPPORT. CRACKED. MAIN CABIN, FLOOR SUPPORT WEB UPPER FLANGE HAS SEVERAL CRACKS FROM FS 400 T0 420. UPPER FLANGE REMOVED DUE TO CARGO MOD AND REPLACED BY CHANNEL, REF STC SA-1998 - [SDR EISA97267](https://openairdocs.org/sdr/EISA97267), Dec 12, 1997: FLOORBEAM. CORROSION. MAIN CABIN, FLOORBEAM UPPER CAP HAS CORROSION AT FS 360 BL 15L TO BL 15R. FABRICATED AND INSTALLED NEW TOP CAP PER SRM 53-10-08. (M) - [SDR EISA97266](https://openairdocs.org/sdr/EISA97266), Dec 12, 1997: STRINGER. CRACKED. STRINGER S-1 CRACKED AT FS 400. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M) - [SDR EISA97265](https://openairdocs.org/sdr/EISA97265), Dec 12, 1997: STRINGER. CRACKED. STRINGER S-1 CRCKED AT FS 380. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M) - [SDR EISA97264](https://openairdocs.org/sdr/EISA97264), Dec 12, 1997: STRINGER. CRACKED. STRINGER S-1 CRACKED AT FS 360. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M) - [SDR AALA971123](https://openairdocs.org/sdr/AALA971123), Jun 20, 1997: ACTUATOR. BROKEN. PHL - FLT 0512 - DURING APPROACH TO PHL WHEN LANDING GEAR EXTENDED, RT MAIN LANDING GEAR FAILED TO EXTEND NORMALLY, RECYCLED LANDING GEAR WITH SAME RESULTS. ACC - [SDR AALA970989](https://openairdocs.org/sdr/AALA970989), May 28, 1997: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT CHECK, AFT VENTRAL STAIRWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT VENTRAL STAIRWAY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NOR - [SDR AALA970307](https://openairdocs.org/sdr/AALA970307), Feb 7, 1997: WIRE. BROKEN. DFW - FLT 475 - DURING APPROACH TO DFW, WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AN - [SDR AALA961733](https://openairdocs.org/sdr/AALA961733), Nov 13, 1996: SKIN. CRACKED. TUL - FOUND SKIN CRACKED AT 4 RIVITS HEADS, STATION 410. CUT OUT CRACKS IN SKIN INSTALLED REPAIR PER SRM 53-30-3 . (M) - [SDR AALA951067](https://openairdocs.org/sdr/AALA951067), Jun 5, 1995: WIRE. BROKEN. ORD - FLT 1262 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO GREEN LIGHT. RECYCLED LANDING GEAR ## 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 19800509051769I](https://openairdocs.org/incident/19800509051769I), May 9, 1980: Boeing 727223 (N6813), Palm Springs, CA. Aircraft descended dangerously low on final approach. ## Other aircraft with N6813 - [Cancelled 1929-10-23](https://openairdocs.org/deregistered/N6813-1929-10-23): Ireland N-2, S/N 17. Owner: [Curtiss Flying Service Inc](https://openairdocs.org/faa-owner/CURTISS%20FLYING%20SERVICE%20INC), [Garden City, NY](https://openairdocs.org/faa-place/NY/Garden%20City) --- 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.