N6809, cancelled Nov 2, 2011

Service difficulty reports · 101

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 = 'N6809' AND deregistration_id = 'N6809-2011-11-02'
  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 GAIA04092OPSkin · crackedDURING PS CHECK, A 2 INCH CRACK WAS FOUND ON THE RIGHT SIDE OF THE NOSE WHEEL WELL AT FS 290. REPAIRED WHEEL WELL IAW THE 727 SRM CH 51-40-2 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M)Sep 14, 2004 · N6809 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA04090OPArm · out of adjustL1 DOOR HARD TO CLOSE. ADJUSTED PROGRAMMING ARM. CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M)Aug 24, 2004 · N6809 · Boeing 727223 · Passenger/Crew DoorsSDR GAIA04034OPJackscrew · lack of lubeFLT 1736 - BNA-ATL - AIRCRAFT APPEARS OVERLY SENSITIVE IN PITCH WITH CHANGES IN STABILIZER TRIM. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED AND OPS CHECKED STAB TRIM, TRIM WHEEL COAST GOOD, MANUAL, ELECTRONIC CONTROLS TEST GOOD, SECURITY Feb 21, 2004 · N6809 · Boeing 727223 · Stabilizer Control SystemSDR GAIA02040OPJackscrew · damagedFLT 879 - FWA-SJC - DURING CLIMB-OUT WHEN FLAPS SELECTED TO RETRACT. THE OUTBOARD FLAPS WHERE SPLIT. THE CREW DECLARED AND EMERGENCY LANDING, DUMPED FUEL AND RETURNED TO FWA. THE LANDING WAS UNEVENTFUL. REMOVED AND REPLACED THE LEFT OUTBOARD FLAP OUTBOARD Apr 29, 2002 · N6809 · Boeing 727223 · Trailing Edge Flap Control SystemSDR GAIA01295OPWarning System · malfunctionedFLT 202 - SEA-GEG - DURING CRUISE, THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. THE CREW ACCOMPLISHED ABNORMAL PROCEDURES AND THE LIGHT EXTINGUISHED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN GEG. INSPECTED AIR DUCTS FOR LEAKS IN PYLON AREA. NO LEAKS WERAug 10, 2001 · N6809 · Boeing 727223 · Overheat DetectionSDR GAIA01184STSpar · corrodedDURING A LTC INSPECTION, THE LEFT FRONT SPAR LOWER CHORD WAS DISCOVERED CORRODED BELOW NR 3 SLAT OUTBOARD TRACK. ACCOMPLISHED LEFT WING LOWER SPAR CHORD REPAIR FSS 450 IAW REPAIR ORDER FASI-009RO-1 REV IR DATED 4/26/02. (M)May 5, 2001 · N6809 · Boeing 727223 · Wing SparSDR GAIA01183STSpar · corrodedDURING A LTC INSPECTION, THE LEFT LOWER SPAR CHORD WAS DISCOVERED CORRODED AT WING LEADING EDGE STATION 305 THROUGH STATION 325. ACCOMPLISHED LEFT WING LOWER SPAR CHORD REPAIR FSS 327 IAW REPAIR ORDER FASI-0099O-1 REV IR DATED 4/26/01. (M)May 5, 2001 · N6809 · Boeing 727223 · Wing SparSDR GAIA01182STFloorbeam · corrodedDURING A LTC INSPECTION, THE BS 950 FLOORBEAM UPPER CHORD WAS DISCOVERED CORRODED LBL 24.75 TO 45.50. ACCOMPLISHED BS 950 FLOORBEAM UPPER CHORD REPAIR LBL 32.75 IAW REPAIR ORDER FASI-101RO-1 REV IR DATED 04/26/01. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA01181STHinge Fitting · crackedDURING A LTC INSPECTION, THE NR 9 SPOILER HINGE SUPPORT FITTING WAS DISCOVERED CRACKED ON THE INBOARD SIDE, ABOVE HINGE BOLT. ACCOMPLISHED NR 9 SPOILER SUPPORT FITTING REPAIR PER REPAIR ORDER FASI-011RO-1 REV I/R DATED 4/26/2001. (M)May 5, 2001 · N6809 · Boeing 727223 · SpoilersSDR GAIA01180STFitting · corrodedDURING A LTC INSPECTION, BS 1183 STRINGER 19L STRINGER TIE FITTING WAS DISCOVERED CORRODED. ACCOMPLISHED BS 1183 STRINGER 19L STRINGER END TIE FITTING REMOVAL AND REPLACEMENT IAW SRM 53-10-3 AND SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01179STStringer · crackedDURING A LTC INSPECTION, DISCOVERED STRINGERS ABOVE AND BELOW NR 3 ENGINE PRECOOLER EXHAUST DUCT WERE CRACKED AT BS 1273 STRINGER 10R AND 11R. ACCOMPLISHED STRINGER REPAIRS BS 1273 STRINGER 10R AND 11R IAW SRM 53-10-3 FIG 2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Longeron/StringerSDR GAIA01178STWeb · corrodedDURING A LTC INSPECTION, THE FLOORBEAM IN AFT CARGO FLOOR WAS DISCOVERED TO HAVE A CORRODED FASTENER THAT IS WORKING INTO THE FACE OF THE FLOORBEAM AT BS 1166 AT BL 25L. ACCOMPLISHED SHEAR WEB REPAIR BS 1166 TO 1176 IAW SRM 53-10-2 AND SRM 51-30-2 AND SRM 51-May 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01177STTee Chord · crackedDURING A LTC INSPECTION IT WAS DISCOVERED THAT THE STATION 950 BULKHEAD UPPER ATTACH ANGLE IN LEFT WHEEL WELL (LBL 50) IS CRACKED. ACCOMPLISHED 950 BULKHEAD T-CHORD REPAIR LBL 50 IAW SRM 51-40-4 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, BulkheadSDR GAIA01176STSkin · corrodedDURING A LTC INSPECTION IT WAS DISCOVERED THAT THE LEFT ELEVATOR INBOARD TRAILING EDGE STATIC WICK MOUNT BASE HAS CORROSION UNDER BASE AND EDGES. ACCOMPLISHED LEFT ELEVATOR UPPER SKIN REPAIR ELEV STATION 209.96 IAW SRM 55-20-3 FIG 2. (M)May 5, 2001 · N6809 · Boeing 727223 · Elevator, Plate/SkinSDR GAIA01175STStiffener · corrodedDURING A LTC INSPECTION, A HORIZONTAL STIFFENER WAS DISCOVERED CORRODED AT BS 178 BULKHEAD, WL 188 LBL 25 TO RBL 25. ACCOMPLISHED BS 178 BULKHEAD HORIZONTAL STIFFENER REMOVAL AND REPLACEMENT BS 178 WL 188 LBL 25 TO RBL 25 IAW SRM 53-10-2 PAGE 3 AND SRM 51-30-May 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01174STPressure Panel · crackedDURING A LTC INSPECTION, A CRACK WAS DISCOVERED IN THE NOSE WHEEL WELL UPPER PRESSURE WEB AT BL 0 AT BS 277. ACCOMPLISHED NOSE WHEEL WELL UPPER PRESSURE WEB REPAIR BS 277 BL 0 IAW SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, BulkheadSDR GAIA01186STDoor Frame · dentedDURING A LTC INSPECTION, DISCOVERED C1 DOOR CUTOUT AREA UPPER SKIN HAS TWO DENTS IN WEB. ACCOMPLISHED FORWARD CARGO DOOR C-1 UPPER WEB REPAIR BS 580-600 WL 198 IAW B727 SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, StructureSDR GAIA01185STSkin · corrodedDURING A LTC INSPECTION, BULGING SKIN AND DISHED/POPPED FASTENERS WERE DISCOVERED ALONG STRINGER 27 LEFT, BS 305-312, LEFT LOWER NOSE CHORD. ACCOMPLISHED LOWER NOSE LANDING GEAR WHEEL WELL LOWER NOSE CHORD REMOVAL AND REPLACEMENT AND FUSELAGE SKIN REPAIR AND May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA01173STSkin · dentedDURING A LTC INSPECTION, A DENT WAS DISCOVERED ON FUSELAGE SKIN AT BS 244, 1 INCH UNDER STRINGER 17L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 244, 1 INCH BELOW STRINGER 17L IAW SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA01172STDoor Frame · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE C-1 CARGO DOOR FORWARD FRAME WEB IN THE CUT OUT IS CRACKED IN 4 AREAS. ACCOMPLISHED C-1 CARGO DOOR CUTOUT FORWARD FRAME WEB REPAIR BS 560 IAW SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, StructureSDR GAIA01171STStrap · corrodedDURING A LTC INSPECTION, CORROSION WAS DISCOVERED ON THE BS 950 DOUBLER/MODIFICATION, STRINGER 14R AND 17R. ACCOMPLISHED BLENDOUT REPAIR BS 950 AT STRIGNER 14R AND 17R ON THE WEIGHT UPGRADE REINFORCEMENT STRAP IAW B727 SRM 51-10-6. OK FOR CONTINUED SERVICE PMay 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01170STPressure Panel · crackedDURING A LTC INSPECTION, A CRACK WAS DISCOVERED IN THE NOSE WHEEL WELL LEFT WEB JUST BELOW FORWARD PRESS PANEL STATION 277. ACCOMPLISHED NOSE WHEEL WELL PRESSURE WEB REPAIR BS 277 LEFT IAW B727 SRM 53-10-2 FIG 2 AND SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, BulkheadSDR GAIA01169STSplice · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT OVERWING EXIT, AFT LOWER SIDE, BS 850 STRINGER 16L STRINGER SPLICE IS CRACKED IN TWO PLACES, UPPER AND LOWER SIDE OF STRINGER. ACCOMPLISHED STRINGER SPLICE REPAIR BS 850 STRINGER 16L IAW B727 SRM 53May 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01168STSkin · gougedDURING A LTC INSPECTION A GOUGE IN THE SKIN WAS DISCOVERED AT LEFT STATION 277 STRIGNER 26. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 277 AT STRINGER 26L IAW B727 SRM 53-30-3 FIG 3. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA01167STStiffener · crackedDURING A LTC INSPECTION A HORIZONTAL STIFFENER WAS DISCOVERED CRACKED AT BS 178 BULKHEAD, WL 198, RBL 6, OUTBOARD END. ACCOMPLISHED BS 178 BULKHEAD REPAIR BS 178, WL 198, RBL 6 IAW B727 SRM 53-10-2 AND SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01166STStringer · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE LEFT VERTICAL STABILIZER INTERIOR STRINGER 3RD BAY DOWN FROM PANEL 9504 IS CRACKED. ACCOMPLISHED VERTICAL STAB STRINGER REPAIR STRINGER 8L FIN STATION 60 IAW B727 SRM 55-30-4 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Vertical StabilizerSDR GAIA01165STTie · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT AT BS 1183 A VERTICAL BEAM AT LBL 47.03 TENSION TIE IS CRACKED AND CORRODED. ACCOMPLISHED BS 1183 AT LBL 47.03 TENSION TIE REMOVAL AND REPLACEMENT IAW B727 SRM 51-30-2 AND SRM 51-20-1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01164STCargo Track · corrodedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT IN THE AFT MAIN CARGO COMPARTMENT A SEAT TRACK IS CORRODED FROM BS 1110-1136, AT LBL 45. ACCOMPLISHED SEAT TRACK REPAIR BS 1050-1140 LBL 45.5 IAW B727 SRM 53-10-5 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA01163STFloorbeam · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED AT RBL 24.75 A LONGITUDINAL FLOORBEAM UPPER CHORD IS CRACKED AT BS 760, WL 207. ACCOMPLISHED LONGITUDINAL FLOORBEAM UPPER CHORD REPLACEMENT BS 740-848 RBL 24.75 IAW B727 SRM 51-30-2 AND SRM 51-10-1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA01162STSeat Track · corrodedDURING A LTC INSPECTION, IT WAS DISCOVERED AT BS 940-950, LBL 24.75 SEAT TRACK OUTBOARD FLANGE IS CORRODED. ACCOMPLISHED SEAT TRACK REPLACEMENT BS 870-950 PLUS 10 INCHES LBL 24.75 IAW B727 SRM 57-50-3 FIG 9. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA01161STAttach Fitting · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE NR 4 SLAT ACTUATOR ATTACH FITTING PREVIOUS REPAIR IS CRACKED, INSIDE SLAT. ACCOMPLISHED NR 4 SLAT ACTUATOR RIB REPAIR IAW B727 SRM 57-50-3 FIG 9. (M)May 5, 2001 · N6809 · Boeing 727223 · Leading Edge Slat ActuatorSDR GAIA01160STFloorbeam · corrodedDURING A LTC INSPECTION FOUND CORROSION ON A FLOORBEAM WAS DISCOVERED AT BS 1130, BBL 0 AS VIEWED FROM THE AFT PIT. ACCOMPLISHED BS 1130, BBL 0 FLOORBEAM C ANGLE REPAIR IAW B727 SRM 53-10-2 FIG 7 AND SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA01159STCrease Beam · corrodedDURING A LTC INSPECTION, FOUND CORROSOIN WAS DISCOVERD ON LOWER SURFACE OF CREASE BEAM BS 317, RBL 55, WL 208, AND UPPER SURFACE FROM BS 344-380. ACCOMPLISHED CREASE BEAM REPLACEMENT BS 301-360, RBL 55, WL 208 IAW B727 SRM 53-10-2, SRM 51-20-1, AND SRM 51-30-May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, StructureSDR GAIA01158STFrame · crackedDURING A LTC INSPECTION IT WAS DISCOVERED AT BS 520 FRAME DENTED BETWEEN STRINGER 23-24R. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 520 BETWEEN STRINGER 23/24R IAW B727 SRM 53-10-4 FIG 3. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, FrameSDR GAIA01157STDoor Frame · crackedDURING A LTC INSPECTION, A CRACK WAS DISCOVERED ON THE C-1 CARGO DOOR CUTOUT AFT FRAME WEB AT NR 6 STOP. ACCOMPLISHED C-1 DOOR CUTOUT AFT FRAME REPAIR BS 620 BETWEEN STRINGER 26/25R IAW B727 SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, StructureSDR GAIA01151STDoor Frame · crackedDURING A LTC INSPECTION IT WAS DISCOVERED THAT THE E/E COMPARTMENT DOOR INTERIOR HAS A CRACK IN THE RADIUS OF DOOR FRAME. ACCOMPLISHED E/E DOOR FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Electrical/Electronic Compartment DoorsSDR GAIA010150STFloorbeam · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE BS 740 FLOORBEAM UPPER CHORD IS CRACKED IN THE RADIUS UNDER THE RBL 45.5 SEAT TRACK. ACCOMPLISHED FLOORBEAM UPPER CHORD REPAIR BS 740 RBL 45.5 IAW B727 SRM 53-10-4 FIG 4. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA01149STWeb · corrodedDURING A LTC INSPECTION IT WAS DISCOVERED THAT THE LEFT AFT SHEAR WEB IN CABIN IS CORRODED. ACCOMPLISHED SHEAR WEB REMOVAL AND REPLACEMENT BS 1130-1176 LEFT IAW B727 SRM 53-10-2 AND SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01148STSkin · corrodedDURING A LTC INSPECTION, CORROSION AND GOUGES WERE DISCOVERED ON THE FUSELAGE SKIN AT BS 366-370, STRINGER 17-18 LEFT. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 366-370, BETWEEN STRINGER 17-18 LEFT IAW B727 SRM 53-30-3 FIG 3. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA01147STFloorbeam · corrodedDURING A LTC INSPECTION, FOUND CORROSION ON FLOORBEAM WAS DISCOVERED AT BS 1110 BL 30L AS VIEWED FROM LOWER CARGO COMPARTMENT, LOWER SIDE OF UPPER T-CHORD. ACCOMPLISHED FLOORBEAM UPPER CHORD REPAIR BS 1110 LBL 30 IAW B727 SRM 53-10-8 FIG 8. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA01146STFloorbeam · corrodedDURING A LTC INSPECTION, FOUND CORROSION ON FLOORBEAM LOWER SIDE WAS DISCOVERED AT BS 1110, AS VIEWED FROM AFT CARGO. ACCOMPLISHED FLOORBEAM LOWER CHORD REPAIR BS 1110 IAW B727 SRM 53-10-8 FIG 8. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA01145STFlap · corrodedDURING A LTC INSPECTION, PITTING CORROSION AROUND DATA PLATE WAS DISCOVERED ON THE NR 6 KRUGER FLAP, INNER FLAP SURFACE. ACCOMPLISHED NR 6 KRUGER FLAP REPAIR IAW B727 SRM 57-50-3 FIG 2. (M)May 5, 2001 · N6809 · Boeing 727223 · Leading Edge DevicesSDR GAIA01144STFloorbeam · corrodedDURING A LTC INSPECTION, CORROSION ON FLOORBEAM WAS DISCOVERED AT BS 1130R WHERE SHEAR TIE AND FLOORBEAM INTERSECT, AS VIEWED FROM AFT CARGO. ACCOMPLISHED FLOORBEAM STABILIZATION STRAP REPAIR BS 1130 RBL 45.5 IAW B727 SRM 53-10-8 FIG 6. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Floor BeamSDR GAIA01143STSkin · corrodedDURING A LTC INSPECTION, BULGING SKIN WAS DISCOVERED AT BS 350-360, STRINGER 22L, UNDER STRINGER TIE FITTING. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 350-360 STRINGER 22 LEFT IAW B727 SRM 53-30-3 FIG 3A. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Plate/SkinSDR GAIA01142STFrame · crackedDURING A LTC INSPECTION AT IT WAS DISCOVERED AT THE FORWARD ELECTRONIS COMPARTMENT, ZONE 11.2, STATION 196.5, RIGHT FRAME CRACKED WITH A PIECE OF MATERIAL MISSING. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 196.5 RBL 12.0 IAW B727 SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, FrameSDR GAIA01141STStringer · crackedDURING A LTC INSPECTION STRINGER 15 LEFT WAS DISCOVERED CRACKED AT LEFT WING SCANNING LIGHT BS 720B PLUS 5. ACCOMPLISHED STRINGER REPAIR BS 720B PLUS 5 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Longeron/StringerSDR GAIA01140STStringer · crackedDURING A LTC INSPECTION STRINGER 15 LEFT WAS DISCOVERED CRACKED AT LEFT WING SCANNING LIGHT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR BS 720B PLUS 15 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Longeron/StringerSDR GAIA01139STGusset · crackedDURING A LTC INSPECTION IT WAS DISCOVERED AT BS 825.95 THE LEFT LOWER FRAME GUSSET CRACKED AT WL 200, LBL 50. ACCOMPLISHED BS 825.95 FUSELAGE FRAME GUSSET REMOVAL AND REPLACEMENT BS 825-95 WL 200 LBL 50 IAW B727 SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Miscellaneous StructureSDR GAIA01138STFrame · crackedDURING A LTC, INSPECTION A FRAME WAS DISCOVERED CRACKED AT BS 910 STRINGER 14 RT. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 910 AT STRINGER 14 RT IAW B727 SRM 53-10-2 AND SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, FrameSDR GAIA01137STFrame · dentedDURING A LTC INSPECTION, A FRAME WAS DISCOVERED DENTED AT BS 500, BETWEEN STRINGER 24-25 RT. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 500 RT AT STRINGER 24R AND 25R IAW B727 SRM 53-10-4 FIG 2. (M)May 5, 2001 · N6809 · Boeing 727223 · Fuselage Main, Frame
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