N6806, cancelled May 10, 2007

Service difficulty reports · 80

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

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N6806' AND deregistration_id = 'N6806-2007-05-10'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR GAIA04089OPLight · inoperativeON PREFLIGHT, FOUND EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED EXIT LIGHT FOR CHARGING AND INSTALLED SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jul 22, 2004 · N6806 · Boeing 727223 · Emergency LightingSDR GAIA04072Rod · unserviceableAT DEPARTURE, LT MAIN GEAR FAILED TO RETRACT. THIS WAS VERIFIED BY THE TOWER. CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT WHERE A LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED AFT RADIUS ROD ON OB DOOR LT MAIN WHEEL WELL. DOOR FIT AND OPS CHECK, May 6, 2004 · N6806 · Boeing 727223 · Landing Gear Retraction/Extension SystemSDR GAIA04007OPLight · inoperativeDURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT DOOR EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jan 23, 2004 · N6806 · Boeing 727223 · Emergency LightingSDR GAIA03105Frame · dentedDURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 1010 HAS A DENT ABOVE STRINGER 25R. REF FASI N/R 53289 CUT OUT DAMAGE, 7 INCHES BY 3.5 INCHES DOUBLER REPAIR PER B727 SRM 51-40-3, FIGURE 1 AND 53-10-2 FIGURE 5. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03094Floorbeam · corrodedDURNG B-2 CHECK, FOUND MAIN CABIN FLOORBEAM ANGLE CORRODED LBL 60 BS 848. REF FASI N/R 53138 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 AND 53-10-1 FIG 1. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA03093Floorbeam · corrodedDURING B-2 CHECK, FOUND MAIN CABIN FLOORBEAM UPPER 'T' CAP CORRODED RBL 45.5 BS 765 TO 848. REF FASI N/R 53136 REPLACED DAMAGED 'T' CAP P/N 65-16279-10 PER B-727 SRM 51-30-5, AND 51-30-2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA03092Stringer · crackedDURING B-2 CHECK, FOUND MAIN CABIN STRINGER 15 RT CRACKED AT AFT SIDE OF BS 720B. REF FASI N/R 53135, ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Longeron/StringerSDR GAIA03106Frame · dentedDURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 950E HAS A DENT BY STRINGER 25L. REF FASI N/R 53292. FABRICATED DOUBLER REPAIR FROM 7075-T6, .080, DIMENSIONS 17.75 INCH BY 2.5 INCHES REPAIRED IAW B727 SRM 51-10-2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03086Frame · dentedDURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 380 HAS A DENT IN THE RADIUS BELOW STRINGER 6LT. REF FASI N/R 53129, CUT OUT DAMAGE 4.75 BY 1.25, DOUBLER REPAIR PER B727 SRM 51-40-3 AND 53-10-4 FIG 1. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03091Stringer · crackedDURING B-2 CHECK FUOND MAIN CABIN STRINGER 15 LT CRACKED FORWARD OF BS 720C. REF FASI N/R 53134 ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Longeron/StringerSDR GAIA03090Frame · dentedDURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 600 DENTED IN RADIUS BELOW STRINGER 16RT. REF FASI N/R 53133, ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03089Frame · dentedDURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 580 DENTED IN RADIUS BELOW STRINGER 16RT. REF FASI N/R 53132 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03088Frame · crackedDURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 560 CRACKED BELOW STRINGER 16RT. REF FASI N/R 53131 CUTOUT DAMAGE, ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03085Flap Track · crackedDURING B-2 CHECK, FOUND NR 5 FLAP TRACK SPACER BLOCK CRACKED AT WBL 124. REF FASI N/R 50408, INSTALLED OVERSIZE FASTENERS IAW S/B 727-57-136 REV 1, FIGURE 2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Trailing Edge FlapsSDR GAIA03084Frame · crackedDURING B-2 CHECK, FOUND FUSELAGE FRAME AT BS 950D CRACKED, ABOVE STRINGER 22R. REF FASI N/R 50407, FABRICATED REPAIR DOUBLER FROM 7075-T6, .080, DIMENSIONS 9 INCHES BY 3 INCHES. REPAIRED IAW S-727 SRM 51-40-3, FIGURE 1. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03083Seat Track · corrodedDURING B-2 CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED AT BS 344 TO BS 360, RBL 45.5. REF FASI N/R 50403. FABRICATED REPAIR FROM BAC 1520-792 MATERIAL. LENGTH 14 INCHES REPAIRED IAW B727 SRM 53-10-05, FIGURE 7 AND 53-10-2, FIGURE 7. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA03096Floorbeam · corrodedDURING B-2 CHECK, FOUND FORWARD LAVATORY FLOORBEAM UPPER 'T' CORRODED BS 344 RBL 25 TO RBL 50 ALSO AT LBL 25. REF FASI N/R 53195, REPLACED FLOORBEAM UPPER 'T' CAP RBL 60 TO LBL 60 PER B77 53-10-8 FIG 3 AND 51-30-2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA03099Beam · crackedDURING B-2 CHECK, FOUND BS 1183 VERTICAL BEAM CRACKED LBL 36 INCHES WL 250. REF FASI N/R 53249, INSTALLED REPAIR PER S/B 727-53-0192 REV 2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, StructureSDR GAIA03098Rib · crackedDURING B-2 CHECK, FOUND RIGHT ELEVATOR SUPPORT RIB STATION 17.2 CRACKED. REF FASI N/R 53208, REPLACED ELEVATOR SUPPORT RIB PER S/B 727-55A0091. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Elevator, Spar/RibSDR GAIA03097Stiffener · crackedDURING B-2 CHECK, FOUND LEFT WING REAR SPAR VERTICAL STIFFENER CRACKED AT WS 556. REF FASI N/R 53206, REPLACED STIFFENER PER B727 SRM 51-30-2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Wing Miscellaneous StructureSDR GAIA03095Floorbeam · corrodedDURING B-2 CHECK, FOUND MAIN CABIN FLOORBEAM BS 480 CORRODED AT LBL 30 AND CRACKED AT LBL 59. REF FASI N/R 53187, CUT OUT DAMAGED AREA, INSTALLED REPAIR PER B727 SRM 53-10-8 FIG 1. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA03087Frame · dentedDURING B-2 CHECK, FOUND MAIN CARGO CABIN FRAME BS 540 HAS A DENT IN THE RADIUS BELOW STRINGER 16RT. REF FASI N/R 53130 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 53-10-2 FIG 2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03104Frame · dentedDURING B-2 CHECK, FOUND AFT CARGO FRAME DENTED BS 1070 AT STRINGER 25 RT. REF FASI N/R 53281, DOUBLER REPAIR IAW B727 SRM 53-10-2 FIG 5. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA03103Seat Track · corrodedDURING B-2, FOUND MAIN CABIN SEAT TRACK CORRODED BS 360 BL0. ERF FASI N/R 53268, REPLACED SEAT TRACK BS 344-480 BL 0 PER B727 SRM 53-10-5 FIG 7. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA03102Seat Track · corrodedDURING B-2 CHECK, FOUND MAIN CARGO SEAT TRACK CORRODED BS 360, LBL 25.5. REF FASI N/R 53267, REPLACED SEAT TRACK LBL 25.5 BS 344 TO 480 PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 7. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA03101Seat Track · corrodedDURING B-2 CHECK, FOUND MAIN CARGO SEAT TRACK CORRODED AT BS 760, RBL 45.5. REF FASI N/R 53265, REPLACED SEAT TRACK RBL 45.5, BS 760 TO 840 PER B727 SRM 51-30-2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA03100Floor Support · corrodedDURING B-2 CHECK, FOUND MAIN CABIN FLOOR SUPPORT ANGLE LBL 61 BS 1090 UPPER CHORD CORRODED. REF FASI N/R 53253, REPLACED UPPER CHORD PER B727 SRM 53-10-2 FIG 5 AND 51-30-2. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA03082Seat Track · corrodedDURING B-2 CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED AT BS 360 TO BS 344, RBL 25.5. REF FASI N/R 50402, FABRICATED REPAIR FROM BAC 1520-792 MATERIAL. LENGTH 140 INCHES REPAIRED IAW B727 SRM 53-10-5, FIGURE 7 AND 53-10-2, FIGURE 7. (M)Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA03008OPLight · inoperativeDURING ROUTINE MAINTENANCE AT IAH, IT WAS DISCOVERED THAT THE L-1 EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 14, 2003 · N6806 · Boeing 727223 · Emergency LightingSDR GAIA02166OPLight · inoperativeDURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 20, 2002 · N6806 · Boeing 727223 · Emergency LightingSDR GAIA02025OPDuct · warpedFLT 873 - FWA-LAX - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON FIVE MINUTES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO FWA AND THE LANDING WAS UNEVENTFUL. FOUND THE 13 STAGE DUCT IN THE STUB WING AT THE HIGH PRESSURE WING ANTI-ICE VALVE FLANGE WARPMar 14, 2002 · N6806 · Boeing 727223 · Pneumatic Distribution SystemSDR GAIA02024OPClamp · looseFLT 733 - DFW-FWA - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO DFW AND THE LANDING WAS UNEVENTFUL. FOUND THE CLAMP FOR THE EIGHT STAGE BLEED VALVE LOOSE. TIGHTENED THE SAME AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFTMar 12, 2002 · N6806 · Boeing 727223 · Engine Bleed Air SystemSDR GAI2001F00000Wire · dirtyAFTER TAKE OFF, THE FLIGHT CREW DISCOVERED THAT THE OUTBOARD FLAPS WERE STUCK AT THE 2 DEGREE POSITION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. RESET ASYMMETRY CIRCUIT AND CLEANED CANNON PLUG Oct 11, 2001 · N6806 · Boeing 727223 · Trailing Edge Flap Control SystemSDR GAIA01245OPWire · faultyKHA - FLT 202 - TYS TO DFW, ON CLIMB-OUT FROM TYS, THE NR 2 SLAT DID NOT RETRACT WHEN THE FLAP HANDLE WAS MOVED TO THE UP POSITION. EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO TYS. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED THAT A WIRING HAJun 26, 2001 · N6806 · Boeing 727223 · Leading Edge Slat Position Indicating SystemSDR GAIA00687Indicator · inoperativeDURING PREFLIGHT FOUND, EMERGENCY EXIT LIGHT ARMED INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED INDICATOR LIGHT BASE ASSEMBLY, OPS CHECK OK. AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 1, 2000 · N6806 · Boeing 727223 · Emergency LightingSDR 00683Fitting · crackedDISCREPANCY: DURING HEAVY CHECK FOUND: FUSELAGE FITTING AT FS 870 STR 18 HAS A CRACK INDICATION ON LOWER AFT BOLT HOLE CORRECTIVE ACTION: REPAIRED FITTING IAW TIMCO REO S00342 BY REAMING OUT DAMAGE AND INSTALLING A FREEZE PLUGOct 19, 2000 · N6806 · Boeing 727223 · Fuselage, Wing Attach FittingsSDR 00684Elevator · corrodedDISCREPANCY: DURING HEAVY CHECK FOUND: ELEVATOR TRAILING EDGE CORRODED AT STA 179CORRECTIVE ACTION: REPAIRED ELEVATOR IAW B727 SRM 55-20-2Oct 16, 2000 · N6806 · Boeing 727223 · Elevator Control SystemSDR 00685Seat Track · corrodedDISCREPANCY: DURING HEAVY CHECK FOUND: CORROSION ON THE SEAT TRACK FLANGE AT LBL 45 BS 854 TO 870CORRECTIVE ACTION: REPLACED SEAT TRACKOct 13, 2000 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR 00686Skin · corrodedDISCREPANCY: DURING HEAVY CHECK FOUND:CORROSION ON TEH SKIN DOUBLER AT FS 1163 STR 19RCORRECTIVE ACTION: REPAIRED SKIN AND DOUBLER IAW TIMCO REO S00343 BY CUTTING OUT DAMAGED AREA AND INSTALLING REPAIR DOUBERSOct 13, 2000 · N6806 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA00681Lap Joint · damagedDISCREPANCY: DURING HEAVY CHECK FOUND: SKIN PULLING FASTENER HEADS, STA 460 STR 19R LAP SEAM. CORRECTIVE ACTION: REPAIRED TAP SEAM IAW B727 SRM53-30-3 FIG 5 STA 460 STR 19ROct 12, 2000 · N6806 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA00680Attach Angle · crackedDISCREPANCY: DURING HEAVY CHECK FOUND: LBL 70.5 WL208, BS873-878, SKIN TO FLOOR WEB ATTACH "T" ANGLE CRACKED ON INNER FLANGE. CORRECTIVE ACTION: HAD EDDY CURRENT PERFORMED & STOP DRILLED HOLES AT END OF CRACK CHECKED EDDY CURRENT AGAIN & FOUND TO BE TERMINATOct 12, 2000 · N6806 · Boeing 727223 · Fuselage Main, Attach FittingsSDR GAIA00679Attach Angle · crackedDURING HEAVY CHECK FOUND BS 1343 AFT SPLICE LBL 20 WL 280 SKIN ATTACH ANGLE CRACKED. REMOVED ANGLE IAW B727 SRM 51-30-2 FAB. NEW ANGLE PER B727 51-40-3. INSTALLED NEW ANGLE IAW SRM 51-30-2. (X)Oct 12, 2000 · N6806 · Boeing 727223 · Fuselage Miscellaneous StructureSDR 00682Frames · dentedDISCREPANCY: DURING HEAVY CHECK FOUND: FUSELAGE FRAME AT FS 1166 ABOVE STR 17 WL 210 HAS A DENTED FLANGE CORRECTIVE ACTION: REPAIRED FRAME IAW TIMCO REO S00340 BY CUTTING OUT DAMAGED AREA AND INSTALLING REPAIR DOUBLERSOct 12, 2000 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA00667Keelbeam · crackedDISCREPANCY: DURING HEAVY CHECK FOUND: LEFT LOWER KEELBEAM CHORD ATTACH FLANGE CRACKED AT STA 875, LBL6 WL137.8. CORRECTIVE ACTION: REPAIRED KEELBEAM ATTACH FLANGE IAW SB727 53 0208 REV. 1 DATED FEB. 29, 1996.Oct 11, 2000 · N6806 · Boeing 727223 · Fuselage Main, KeelSDR GAIA00666Angle · corrodedDISCREPANCY: DURING HEAVY CHECK FOUND:C-2 DOOR CUT-OUT AFT FRAME INNER ANGLE CORRODED ABOVE S25 & S26 RT 2 AREAS. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 REPAIRED C-2 DOOR CUT-OUT AFT FRAME INNER ANGLE IAW REO S0Oct 11, 2000 · N6806 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA00665Frame · crackedDISCREPANCY: DURING HEAVY CHECK FOUND: FS360 FRAME CRACKED BELOW STRINGER 7L.CORRECTIVE ACTION: REMOVED DAMAGE FABRICATED NEW ANGLE & FILLERS, FASTENERS IAW REO S00331 INSTALLED ANGLE & FILLERS IAW REO S00331Oct 11, 2000 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA00668Floorbeam · corrodedDISCREPANCY: DURING HEAVY CHECK FOUND: FLOORBEAM STA 727 CORRODED ON UPPER CHORD UPPER SURFACE LBL30, LBL10 & RBL15 EXTENDING UNDER FLOOR SKIN. CORRECTIVE ACTION: CORROSION REMOVED WAS FOUND TO BE OUT OF LIMITS IAW BOEING 727 SRM 53-10-1. FABRICATED AND INSTOct 9, 2000 · N6806 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA00656Frame · dentedDISCREPANCY: DURING HEAVY CEHCK FOUND: FS460 FRAME DENTED BETWEEN STRINGERS 17R & 16RCORRECTIVE ACTION: FABRICATED BEW FRAME DOUBLER AT BS460 BETWEEN STR 16 & 17 & HAD NDT CHECK STOP DRILLED HOLES AT END OF CRACK, INSTALLED IAW B727 SRM 51-40-3 NDT 6-51-00-00Oct 3, 2000 · N6806 · Boeing 727223 · Fuselage Main, FrameSDR GAIA00655Lap Joint · bulgedDISCREPANCY: DURING HEAVY CEHCK FOUND: SKIN JOINT BS359-360, STR 11R-14R SKIN BULGING. CORRECTIVE ACTION: REMOVED FASTENERS, FOUND SKIN TO BE OUT OF LIMITS, FABRICATED REPAIR DOUBLER, ALODINED AND PRIMED REPAIR, & INSTALLED REPAIR IAW B727 SRM 51-30-2, 51-10-Oct 2, 2000 · N6806 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA00654Skin · corrodedDISCREPANCY: DURING HEAVY CHECK FOUND: SKIN, UNDER FORWARD LAV SERVICE DOOR, CORRODED & BULGING STA 304 STR 20R. CORRECTIVE ACTION: REPAIRED IAW B727 SRM 53-30-3 FIG 3Oct 2, 2000 · N6806 · Boeing 727223 · Fuselage Main, Plate/Skin
Back to N6806, cancelled May 10, 2007