# N682CA: 1980 Boeing 727-2S7, registration cancelled 2008-09-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 11, 2008 - Status when cancelled: Valid registration - Airframe: [Boeing 727-2S7](https://openairdocs.org/model/boeing-727-2s7) (registry code 138407Z) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22019 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 28, 1980 - Certificate issued: February 1, 2006 - Last registry action: February 1, 2006 - Mode S code: A90AD8 - Owners when cancelled: [Grand Holdings Inc DBA](https://openairdocs.org/faa-owner/GRAND%20HOLDINGS%20INC%20DBA), [Champion Air](https://openairdocs.org/faa-owner/CHAMPION%20AIR) - Location: [Bloomington, MN](https://openairdocs.org/faa-place/MN/Bloomington) - Owner type: Corporation - Owner's area on the map: 44.8512° N, 93.2261° W: Placed by OpenAirDocs at the center of ZIP code 55425, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N682CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=682CA - Page: https://openairdocs.org/deregistered/N682CA-2008-09-11 From the FAA registry file of October 31, 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 727-2S7: https://openairdocs.org/model/boeing-727-2s7.md ## Service difficulty reports (66, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR C1HA200682019](https://openairdocs.org/sdr/C1HA200682019), Nov 16, 2006: WIRE. BROKEN. "UPON RETRACTION OF FLAPS AFTER TAKEOFF, AMBER NR 7 LEADING EDGE LIGHT REMAINED ILLUMINATED, RUN COM PROCEDURE 2.27.12, DUMPED FUEL RETURN TO DEW. REMOVED AND R - [SDR C1HA200682018](https://openairdocs.org/sdr/C1HA200682018), Oct 11, 2006: SHUTOFF VALVE. FAILED. AT FL350 THE NR 3 BLEED AIR TRIP OFF LT ILLUMINATED.THE RT DUCT PRESSURE NEEDLE DROPPED FROM APPROX 24 PSI TO 10 PSI AND THE CABIN STARTED TO CLIMB. COM 2.36.2 - [SDR C1HA200682017](https://openairdocs.org/sdr/C1HA200682017), Oct 11, 2006: BLEED VALVE. FAILED. AT FL350 THE NR 3 BLEED AIR TRIP OFF LT ILLUMINATED.THE RT DUCT PRESSURE NEEDLE DROPPED FROM APPROX 24 PSI TO 10 PSI AND THE CABIN STARTED TO CLIMB. COM 2.36.2 - [SDR C1HA200682006](https://openairdocs.org/sdr/C1HA200682006), Jan 30, 2006: SEAT TRACK. CORRODED. BS 1010-1070 LBL 45 CABIN SEAT TRACK CHANNEL HAS CORROSION & IS CRACKED ON O/B FLANGE BS 1070. REMOVED SEAT TRACK LBL 45 BS 1010-1070 IAW B727 SRM 51-30-2, FABR - [SDR C1HA200682001](https://openairdocs.org/sdr/C1HA200682001), Jan 30, 2006: SEAT TRACK. CORRODED. BS 1010-1030 RBL 45 CABIN SEAT TRACK TOP & O/B FLANGE HAVE CORROSION. FOUND CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED DAMAGED TRACK FROM STA 9 - [SDR C1HA200682002](https://openairdocs.org/sdr/C1HA200682002), Jan 30, 2006: BEAM. CRACKED. STA 1183 BULKHEAD, VERTICAL BEAM AT RBL 36.83 IS CRACKED AT AFT RADIUS INBOARD SIDE AT WL 230. STOP DRILLED CRACK & INSTALLED REPAIR KIT P/N 65C34406-15, PER S/ - [SDR C1HA200682009](https://openairdocs.org/sdr/C1HA200682009), Jan 30, 2006: FLOORBEAM. CORRODED. FLOORBEAM BS 344 HAS CORROSION. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2, CUT OUT DAMAGED AREA, FABBED FILLER, 7075-T6, .080, 1 X .1875 INCH (2EA) REPAIR AN - [SDR C1HA200682007](https://openairdocs.org/sdr/C1HA200682007), Jan 30, 2006: FLOORBEAM. CORRODED. BS 1030 RBL 4 - 10 LBL CABIN FLOOR SUPPORT UPPER FLANGE HAS CORROSION. CUT OUT DAMAGE AREA AT BS 1030 RBL 20 TO LBL 10 IAW B727 SRM 51-10-1, FABRICATED T-SUPPOR - [SDR C1HA200682010](https://openairdocs.org/sdr/C1HA200682010), Jan 30, 2006: SKIN. BULGED. FUSELAGE EXTERIOR BS 1075 STRINGER 29 RT AT FWD END OF REPAIR DOUBLER HAS SKIN BULGED WITH POPPED RIVET. CUT OUT DAMAGED SKIN, FABBED AND INSTALLED FILLER (2024 - [SDR C1HA200682013](https://openairdocs.org/sdr/C1HA200682013), Jan 30, 2006: STRINGER. CORRODED. AFT LWR COMPARTMENT STRINGER 30 SPLICE AREA SECTION BETWEEN BS 1030 THRU BS 1050 CORROSION SPOTS BETWEEN STRINGER & FUSELAGE SKIN. REMOVED AND REPLACED STRINGER - [SDR C1HA200682014](https://openairdocs.org/sdr/C1HA200682014), Jan 30, 2006: WEB. CRACKED. RIGHT WHEEL WELL BS 870, WEB IS CRACKED FROM APU LOAD CONTROL VALVE ACCESS CUTOUT. STOP DRILLED CRACK, FABBED AND INSTALLED 2 EA DOUBLERS, FABBED FROM 15-5 PH S - [SDR C1HA200682016](https://openairdocs.org/sdr/C1HA200682016), Jan 30, 2006: FLOOR SUPPORT. BULGED. COCKPIT FLOOR SUPPORT AT FS 303 & LBL 12 IS BULGED. REMOVED, FABBED NEW & INSTALLED FLOOR SUPPORT IAW B727 SRM 53-10-2 FIG 7 & 51-30-2. - [SDR C1HA200682012](https://openairdocs.org/sdr/C1HA200682012), Jan 30, 2006: STRINGER. CORRODED. AFT LWR COMPARTMENT STRINGER 30 SPLICE AREA SECTION BETWEEN BS 1010 THRU BS 1030 SPOT OF CORROSION BETWEEN STRINGER & FUSELAGE SKIN. REMOVED AND REPLACED DAMAGE - [SDR C1HA200682005](https://openairdocs.org/sdr/C1HA200682005), Jan 30, 2006: SEAT TRACK. CORRODED. BS 1030-1090 LBL 24 CABIN SEAT TRACK O/B UPPER FLANGE IS CORRODED. REMOVED AND REPLACED SEAT TRACK LBL 24 BS 950-1090 WITH BAC 1520-792, DIM 129.5 INCH IAW 727 - [SDR C1HA200682004](https://openairdocs.org/sdr/C1HA200682004), Jan 30, 2006: VERTICAL BEAM. CRACKED. STA 1183 BULKHEAD, VERTICAL BEAM AT LBL 36.83 IS CRACKED AT AFT RADIUS INBOARD SIDE AT WL 230. STOP DRILLED CRACK & INSTALLED REPAIR KIT P/N 65C34406-14, PER S/ - [SDR C1HA200682003](https://openairdocs.org/sdr/C1HA200682003), Jan 30, 2006: SEAT TRACK. CORRODED. BS 1030-1120 RBL 24 CABIN SEAT TRACK HAS SMALL AREAS OF CORROSION. REMOVED DAMAGE TRACK BS 1010 - 1130 RBL 24 IAW B727 SRM 51-30-2. FABRICATED NEW TRACK P/N BAC - [SDR C1HA200682015](https://openairdocs.org/sdr/C1HA200682015), Jan 30, 2006: STIFFENER. CRACKED. RIGHT WHEEL WELL BS 870 & KEEL BEAM VERTICAL STIFFENER CRACKED (NDT CONFIRMED). REMOVED AND REPLACED DAMAGED STIFFENER P/N 65-18636-378, IAW 727 SRM 51-30-2. - [SDR C1HA200682008](https://openairdocs.org/sdr/C1HA200682008), Jan 30, 2006: FLOORBEAM. CORRODED. BS 1110 LBL 24 - RBL 24 TRANSVERSE FLOOR SUPPORT UPPER FLANGE HAS CORROSION (BOTH SIDES). REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. REMOVED LBL 24 TRACK IAW - [SDR C1HA200682011](https://openairdocs.org/sdr/C1HA200682011), Jan 30, 2006: STRINGER. CORRODED. AFT PIT STRINGER 29R CORRODED AT BS 1075. REMOVED AND REPLACED DAMAGED STRINGER SECTION MATERIAL USED BAC1498-147, DIM 18.375 INCH LENGTH IAW 727 SRM 53-10-2 FI - [SDR C1HA200582001](https://openairdocs.org/sdr/C1HA200582001), May 1, 2005: WINDOW. CRACKED. ENROUTE WINDOW CRACKED, REPLACED R2 WINDOW REF 56-12-11 AND AJUSTED AND OPS CK GOOD. - [SDR C1HA200482002](https://openairdocs.org/sdr/C1HA200482002), Jan 27, 2004: SKIN. DELAMINATED. LEFT IB FORE FLAP DELAMINATED AT IB AFT EDGE. PIN 65-21630-249A REQ NR 125615 REMOVED AND REPLACED. LT IB FORE FLAP, OPS CHECKED OK IAW MM 27-51-01 RII ACCOMPLI - [SDR C1HA200482001](https://openairdocs.org/sdr/C1HA200482001), Jan 14, 2004: SWITCH. OUT OF ADJUST. AFTER TAKEOFF ON GEAR RETRACTION, RIGHT GEAR DOOR LIGHT STAYED ILLUMINATED. RAN COM PROCEDURE 2.32.29. ADJUSTED RIGHT MLG DOOR SWITCH PER CHAMPION AIR MM 32-62- - [SDR C1HA200382011](https://openairdocs.org/sdr/C1HA200382011), Dec 15, 2003: SKIN. CRACKED. LOWER RUDDER TAB UPPER LEFT AND RIGHT SIDE IS DEBONDED AND CRACKED. - [SDR C1HA200382010](https://openairdocs.org/sdr/C1HA200382010), Nov 5, 2003: BATTERY. INOPERATIVE. AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES (2EA) FOR EMERGENCY EXIT IAW MM 33-50-71, OPS CHECKS GOOD. - [SDR C1HA200382009](https://openairdocs.org/sdr/C1HA200382009), Sep 6, 2003: ENGINE. MALFUNCTIONED. NR 2 ENG WAS FLUC EPR+- 4 N1, N2 EGT AND FUEL FLOW ALL WERE FLUCT. PRIOR TO SHUTDOWN NR 2 ENG FUEL HEAT ICING LIGHT STROBING EVEN WITH FUEL HEAT ON. ENG SHUT DO - [SDR C1HA200382007](https://openairdocs.org/sdr/C1HA200382007), Jun 26, 2003: SMOKE DETECTOR. MALFUNCTIONED. SMOKE DETECTOR FWD LAV ACTIVATES OCCASIONALLY WHEN DOOR IS SHUT. - [SDR C1HA200382006](https://openairdocs.org/sdr/C1HA200382006), Jun 25, 2003: SMOKE DETECTOR. WILL NOT TEST. SMOKE DETECTOR IN FWD LAV WILL NOT TEST EVERY TIME. - [SDR CH1A200382005](https://openairdocs.org/sdr/CH1A200382005), Mar 24, 2003: COMPRESSOR. STALLED. ON APPROACH TO LAS AT 500FT, NR 2 ENGINE COMPRESSOR STALLED. DID NOT USE NR 2 REVERSER. FLT ATTND REPORTED COMP STALL ON ROLL OUT - [SDR C1HA200382004](https://openairdocs.org/sdr/C1HA200382004), Feb 22, 2003: FIRE LOOP. OUT OF POSITION. NR 1 GROUND FAULT FIRE DETECTION SYSTEM LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED NR 1 ENGINE FIRE LOOP IAW M/M 26-11-01 GRND OPS. CHECKS GOOD. - [SDR C1HA200382003](https://openairdocs.org/sdr/C1HA200382003), Feb 21, 2003: FIRE LOOP. SHORTED. NR 1 ENGINE FIRE WARNING GROUND FAULT DECTOR LIGHT ILLUMINATED DURING FLIGHT. PERFORMED FIRE WARNING TEST PROCEDURES COM 2.26.3 TESTED NORMAL REPOSITIONED FIRE - [SDR C1HA200382002](https://openairdocs.org/sdr/C1HA200382002), Feb 10, 2003: CONNECTOR. DISCONNECTED. FIRE WARNING TEST FAILED NR 2 ENGINE "B" LOOP. INSPECTED FOUND CONNECTOR PLUG AT ENGINE LOOP DISCONNECTED. RE-CONNECTED OPS CHECK GOOD IN REF TO MM 26-11. - [SDR C1HA200382001](https://openairdocs.org/sdr/C1HA200382001), Jan 12, 2003: SLIDE. DISLODGED. L2 DOOR SLIDE OUT OF CONTAINER. REINSTALLED L2 SLIDE IN CONTAINER IAW MM 26-60, OK FOR SERVICE. - [SDR C1HA200282018](https://openairdocs.org/sdr/C1HA200282018), Dec 11, 2002: BATTERY PACK. LH FWD OVERWING EMERGENCY EXIT LIGHT INOPR&R L/H FWD EMERG EXIT LIGHT BATTERY PACK IAW MM 33-50-21, OPS CHECKS GOOD. - [SDR C1HA200282017](https://openairdocs.org/sdr/C1HA200282017), Dec 11, 2002: BULB. L-2 & R-2 EMERGENCY EXIT SIGNS INOPRELAMPED L-2 & R-2 EMERG EXIT LWR DOOR SIGNS IAW MM 33-50-11. OPS CHKS GOOD. - [SDR C1HA200282016](https://openairdocs.org/sdr/C1HA200282016), Oct 4, 2002: BATTERY. Aft Ceiling emergency exit sign INOPReplaced battery cartridge ASSY. - [SDR C1HA200282015](https://openairdocs.org/sdr/C1HA200282015), Aug 12, 2002: O-RING. LEAKING. ENGINE NR 3 OIL QUANTITY DROPPED TO 1.5 GALLONS. ENGINE OIL TEMPERATURE WAS 90 DEGREES, OIL PRESSURE WAS 44 AND OIL QUANTITY CONTINUED TO DROP TO .5 GALLONS. TE - [SDR C1HA200282014](https://openairdocs.org/sdr/C1HA200282014), Jun 29, 2002: COVER. BROKEN. LT MAIN GEAR LIGHT COVER BROKEN. RESECURED LIGHT COVER AS REQUIRED. - [SDR C1HA200282013](https://openairdocs.org/sdr/C1HA200282013), Jun 5, 2002: LIGHT. INOPERATIVE. EMERGENCY PORT LIGHT IN COCKPIT INOP. R&R LIGHT ASSY PER MM 33-50-101. OPS CK GOOD. - [SDR C1HA200282012](https://openairdocs.org/sdr/C1HA200282012), Jun 5, 2002: POWER SUPPLY. DISCHARGED. LEFT WING CENTER EMERGENCY LIGHT COVERWING INOP. R&R BATTERY POWER SUPPLY IAW MM 33-50-22. ALL OPS CKS NORMAL. - [SDR C1HA200282011](https://openairdocs.org/sdr/C1HA200282011), Apr 21, 2002: WARNING SYSTEM. ACTIVATED. AMBER AIRSTAIR ANNUNCIATOR ILLUMINATED INFLIGHT. VISUAL INSPECTION FROM AFT ENTRY REVEALED DAYLIGHT FROM RIGHT AFT STAIR. DIVERTED TO ORD AND DUMPED FUEL. UPON - [SDR C1HA200282010](https://openairdocs.org/sdr/C1HA200282010), Mar 2, 2002: POWER SUPPLY. DISCHARGED. FIXED INTERIOR EMERGENCY AREA LIGHTS AT AFT ENTRY INOP, 2 ROUND LIGHTS POINTING DOWN. REMOVED AND REPLACED BATTERY POWER SUPPLY FOR AFT ENTRY IAW MM 33-50-71. E - [SDR C1HA200282009](https://openairdocs.org/sdr/C1HA200282009), Feb 1, 2002: ACCESS DOOR. CORRODED. CONDITIONED AIR GROUND CONNECT ACCESS DOOR HAS A BULGE IN SKIN AT HINGE POINT. (CORROSION RELATED C CHECK FINDING). DOOR REPLACED PER SRM. - [SDR C1HA200282008](https://openairdocs.org/sdr/C1HA200282008), Feb 1, 2002: PANEL. CHAFED. RT WING UPPER I/B PANEL FOR APU EXHAUST LOUVER IS CHAFING INTO AFT I/B CORNER OF RECESSED PAN. (CORROSION RELATED C CHECK FINDING) PANEL REPLACED PER AMM. - [SDR C1HA200282007](https://openairdocs.org/sdr/C1HA200282007), Feb 1, 2002: SEAT TRACK. CORRODED. SEAT TRACK CHANNEL AT RBL 54 STA. 344 CORRODED (C CHECK FINDING) REPLACED SEAT TRACK SECTION PER SRM. - [SDR C1HA200282006](https://openairdocs.org/sdr/C1HA200282006), Feb 1, 2002: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 44 STA 344 TO STA 460 HAS CORROSION. (C CHECK FINDING) REPLACED SEAT TRACK SECTION PER SRM. - [SDR C1HA200282005](https://openairdocs.org/sdr/C1HA200282005), Feb 1, 2002: TAB. DELAMINATED. LOWER RUDDER TAB HAS DELAMINATED ON LT UPPER FWD CORNER. (C CHECK FINDING) REPAIR APPROVED BY 8110. - [SDR C1HA200282004](https://openairdocs.org/sdr/C1HA200282004), Feb 1, 2002: SPLICE. CORRODED. STA 480 SPLICE PLATE HAS CORROSION AT FWD END OF INTERCOSTAL BETWEEN STR 28 LT & RT. (C CHECK FINDING) REPAIR APPROVED BY 8110 - [SDR C1HA200282003](https://openairdocs.org/sdr/C1HA200282003), Feb 1, 2002: STRINGER. CORRODED. AFT PIT STR 29 LT CORRODED AT STA. 950 A. (C CHECK FINDING) REPAIR APPROVED BY 8110. - [SDR C1HA200282002](https://openairdocs.org/sdr/C1HA200282002), Feb 1, 2002: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED STA. 1070 LBL 22-44. (C CHECK FINDING) REPAIRED PER SRM - [SDR C1HA200282001](https://openairdocs.org/sdr/C1HA200282001), Feb 1, 2002: STRINGER. CORRODED. STA. 560 FWD SIDE OF TOP ANGLE IS EXFOLIATED ON O/B SIDE OF STR 26 RT, ALSO HAS ONE CORRODED FASTENER THRU WEB. (C CHECK FINDING) REPAIR APPROVED BY 8110. All 66: https://openairdocs.org/deregistered/N682CA-2008-09-11/reports.md ## Other aircraft with N682CA - [Registered now](https://openairdocs.org/aircraft/N682CA): Cirrus Design SR20, S/N 9867, built 2024 --- 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.