Douglas DC-8-73F

Service difficulty reports · 15,471

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'DC873F'
  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 UPS00832708Intercostal · corrodedINSPECTION TYPE:C2, AFT PIT FS 1000 - 1020 INTERCOSTAL AT L35L CORRODED. REMOVED DAMAGED INTERCOSTAL FOR FOM. FABRICATED NEW INTERCOSTAL IAW DOUGLAS DWG NR 5779929, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.May 11, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000295Line · leakingHYDRAULIC FAILURE AND COMPLETE FLUID LOSS DURING APPROACH. SAFETY WIRE BROKEN ON AIR BRAKE HANDLE. FOUND HARD LINE LEAKING AT LT MID FLAP ACTUATOR. INSTALLED FLEX LINE PER EWA ACFT MM CHAP 7. LEAK CK OK. RESAFTIED AIR BRAKE HANDLE.May 11, 2000 · N870TV · Doug DC873F · Hydraulic System, MainSDR UPS00832724Attach Fitting · corrodedINSPECTION TYPE:C2, RIGHT W/W UPPER FWD PRESSURE WEB ATTACH FITTING IS CORRODED AND CRACKED AT HORIZONTAL PRESSURE WEB STA XCW-46-0 AND STA 857. REMOVED FS 857 BULKHEAD RT PRESSURE DOOR DRILLED UP NEW FITTING. REMOVED AND REINSTALLED FUEL DUMP DRUM FOR ACCESMay 10, 2000 · N894UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00832722Door Frame · crackedINSPECTION TYPE:C2, RIGHT MLG W/W DOOR CUTOUT FWD I/B FRAME HAS CRACK STA 886.0 UNDER KEEL BEAM. REMOVED CRACKED FRAME IAW DC8 SRM 51-3-2. MAT ID 7075T6.063 IAW DAC DWG 5616306. FABRICATED FRAME IAW DAC DWG 5616306, HEAT TREATED FRAME FROM 0 TO T6 IAW DAC May 10, 2000 · N894UP · Doug DC873F · Fuselage Main, StructureSDR UPS00832721Door Frame · crackedINSPECTION TYPE:C2, LEFT MLG W/W DOOR CUTOUT FWD I/B FRAME HAS CRACK STA 886.0 UNDER KEEL BEAM. REMOVED CRACKED FRAME IAW DC8 SRM 51-3-2. MAT ID 7075.T6.063 IAW DAC DWG 5616306. FAB FRAME IAW DAC DWG 5616306 & DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRMay 10, 2000 · N894UP · Doug DC873F · Fuselage Main, StructureSDR UPS00832720Intercostal · corrodedINSPECTION TYPE:C2, CORROSION ON INTERCOSTAL FS 1040 AT L35L. REMOVED DAMAGED INTERCOSTAL FOR FOM. FABRICATED NEW INTERCOSTAL IAW DOUGLAS DWG NR 779929, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.May 10, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832719Frame · corrodedINSPECTION TYPE:C2, FWD LWR PIT BETWEEN STA 280 TO 300 BETWEEN LONGERON 35R TO 34R CORRODED AT FRAME 280. REMOVED FASTENERS, FITTING, AND CORROSION. CORROSION ON FITTING OUT OF LIMITS. FAB SPLICE AND DRILLED NEW FITTING IAW DC8 SRM 53-2-0. ALODINED AND PRIMay 10, 2000 · N894UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832707Intercostal · corrodedINSPECTION TYPE:C2, CORROSION ON INTERCOSTAL FS 1040 AT L35L. REMOVED DAMAGED INTERCOSTAL FOR FOM. FABRICATED NEW INTERCOSTAL IAW DOUGLAS DWG NR 5779929, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.May 10, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832705Seat Track · gougedINSPECTION TYPE:C2, SEAT TRACK ''B'' IS WORN AND GOUGED FROM FS 610 - 850; OUT OF LIMITS RT & LT FS 620. ROUTED OUT DAMAGE RT & LT FS 620 WHERE THE TRACK WAS OUT OF LIMITS. INSTALLED 4 HOLE PLUG AND 4 HOLE CHANNEL IAW DC8 SRM 53-2-2, 53-2-3, 51-1-8 & 51-3-0.May 10, 2000 · N894UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832704Seat Track · gougedINSPECTION TYPE:C2, SEAT TRACK ''F'' IS WORN, GOUGED AND HAS BARE METAL STA 810 - 1010. BLENDED GOUGES STA 810 - 920. REMOVED AND REPLACED TRACK STA 970 - 1010 IAW DC8 SRM 53-2-3 & UPS EO DC8 5320-5167C. ALODINED AND PRIMED IAW DC 8 SRM 51-1-8.May 10, 2000 · N894UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832684Seat Track · gougedINSPECTION TYPE:C2, SEAT TRACK G SCALLOPS GOUGED BETWEEN STA 160 & STA 180. BLENDED GOUGES, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED SEAT TRACK STA 130 - 180 IAW DC8 SRM 51-3-0. LOCATED, DRILLED AND DEBURRED SEAT TRACK AND SPLICE FITTING IAW DCMay 10, 2000 · N894UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001760Web · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE MAIN CABIN CUSP WEB AT FS 268 AND RBL 50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0.May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001759Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE MAIN CABIN FLOORBEAM AT FS 1750 AND BL 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FLOORBEAM IAW DC-8 SRM 51-1-20D.May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA001758Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIB AT THE RT STUB WING OVER NR 3 PYLON AT XFS 207.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0.May 9, 2000 · N2674U · Doug DC873F · Wing, Rib/BulkheadSDR RRXA001757Angle · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE MAIN CARGO DOOR THRESHOLD SUPPORT ANGLES AT FS 200 AND 220, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLES IAW DC-8 SRM 51-1-2May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001740Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE MAIN CARGO DOOR SCUFF PLATE AREA BRACKET AT FS 260, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001739Stringer Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN STRINGER TIE END AT FS 1688 TO 1690 AND STR 26L AND 28L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PART IAW DMay 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001738Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE DOUBLER ON LONGERON L28L AT FS 600 , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-3-0.May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001737Stiffener · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE BULKHEAD STIFFENER AT FS 129 AND RBL 40, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED STIFFENER IAW DC-8 SRM 51-1-20D.May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001735Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE UPPER FWD FLANGE FLOORBEAM AT FS 680 AND RBL 52, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor BeamSDR UPS00832718Frame · corrodedINSPECTION TYPE:C2, FRAME FS 80, L36 AFT SIDE CORRODED. REMOVED CORROSION FROM FRAME STA 80, L36 AND FOUND TO BE OUT OF LIMITS . FABRICATED AND INSTALLED REPAIR ANGLE, FILLER, AND DOUBLER IAW STD-53 10-082.May 9, 2000 · N894UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832716Attach Fitting · crackedINSPECTION TYPE:C2, KEEL BEAM RT SIDE, STA 792 FITTING IS GOUGED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0, 51-1-20D & 51-1-16.May 9, 2000 · N894UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00832700Angle · corrodedINSPECTION TYPE:C2, CORROSION ON FLOOR LINER SUPPORT ATTACH ANGLE BETWEEN STA 1400 - 1420 AND L33L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT. REMOVED CORRODED SECTION OF ANGLE, FABRICATED NEW SECTION, ALODINED, PRIMED AND INSTALLED IAW DOUGLAS DRAWING May 9, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832698Angle · corrodedINSPECTION TYPE:C2, CORROSION ON LINER SUPPORT ATTACH ANGLE STA 1440 - 1540 L33L. REMOVED CORRODED SUPPORT ANGLE. FABRICATED NEW ANGLE, ALODINED, PRIMED & INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21 & DOUGLAS DRAWING NR 9 759432.May 9, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832692Angle · corrodedINSPECTION TYPE:C2, CORROSION ON LINER SUPPORT ATTACH ANGLE STA 1440 - 1540 L33L. REMOVED CORRODED SUPPORT ANGLE, FABRICATED NEW ANGLE, ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21 & DOUGLAS DRAWING NR 9 759432.May 9, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832686Frame · crackedINSPECTION TYPE:C2, CRACK IN RADIUS OF PIT FRAME REPAIR AT FS 420 EXTENDING FROM LONG 25 TO 29 RT. FABBED PIT FRAME IAW DC8 DWG NR 3773159. HEAT TREAT IAW DC8 DWG NR 3773159. LOCATED AND DRILLED TRIM TO FIT IAW DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SMay 9, 2000 · N894UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832685Web · corrodedINSPECTION TYPE:C2, CORROSION INSIDE TORQUE BOX FS 280 BETWEEN LONGERONS 32R & 31R. REMOVED FITTING AND WEB AT STA 280. FABBED NEW WEB, FITTING AND WEB SPLICES IAW DC8 SRM 53-2-0 & DAC DWG 5772787. HEAT TREATED WEB IAW TPS-1003. ALODINED AND PRIMED IAW DCMay 9, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832662Pressure Panel · crackedINSPECTION TYPE:C123, STA -12 BL 0 PRESSURE WEB HAS A POPPED RIVET AND A CRACK. REPAIRED IAW SRO8570026.May 9, 2000 · N802UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS00832657Fitting · crackedINSPECTION TYPE:C123, STA 1240 LONG 27L DOOR STOP FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755854 AND SRM 51-1-21.May 9, 2000 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832552Light · inoperativeINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACKS, OPS CHECKS GOOD.May 9, 2000 · N811UP · Doug DC873F · Emergency LightingSDR UPS00832525Switch · failedINSPECTION TYPE:N/A, NOTICED SLIGHT SMOKE COMING FROM PANEL AREA. TURNED LIGHTS TO LOW, NO SMOKE. REMOVED C/P ON WHITE FLOOD LIGHT REOSTAT AND SECURED. DEFERRED PER MEL 33-1, ORDERED REOSTAT.May 9, 2000 · N807UP · Doug DC873F · Flight Compartment LightingSDR RRXA001756Web · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT MLG DOOR UPLOCK TORQUE BOX VERTICALLY IN THE RADIUS OF THE ATTACH FLANGE APPROX. 2 INCHES LONG AT THE FWD WEB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1May 8, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001755Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE UPPER SIDE OF THE RT WING LE SKIN 2 INCHES FWD OF THE WING SPAR AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001754Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE UPPER SIDE 2 INCHES FWD OF THE WING SPAR ON THE RT WING LE SKIN AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001753Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK 2 INCHES FWD OF THE WING SPAR ON THE RT WING LE SKIN ON UPPER SIDE AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001752Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE SKIN ON UPPER SIDE 2 INCHES FWD OF THE WING SPAR AT THE RT WING LEADING EDGE AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001736Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LEFT WHEEL WELL PRESSURE PANEL AT FS 915 TO 925 AND LBL 58 TO 65, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Fuselage Main, BulkheadSDR RRXA001734Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WW PRESSURE PANEL, FS 857 TO 879 AND LBL 58 TO 65, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Fuselage Main, BulkheadSDR UPS00832763Attach Fitting · corrodedINSPECTION TYPE:C123. STA 320 BATH TUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 35L-36. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D.May 8, 2000 · N802UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00832757Fitting · crackedINSPECTION TYPE:C123, STA 798 FLOORBEAM TO WING BOX FITTING IS CRACKED AT RBL 50. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3643112 AND SRM 51-1-20D.May 8, 2000 · N802UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00832756Fitting · crackedINSPECTION TYPE:C123, STA 781 FLOORBEAM ATTACH FITTING IS CRACKED AT LBL 24. REMOVED AND REPLACED FITTING IAW DWG 4751820 AND SRM 51-1-20D.May 8, 2000 · N802UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00832753Frame · crackedINSPECTION TYPE:C123, STA 460 FRAME IS CRACKED AT LONG 9R. REPAIRED IAW SRM 53-2-0 FIG 2.May 8, 2000 · N802UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832731Floorbeam · damagedINSPECTION TYPE:C2, CABIN, ELONGATED HOLE IN FLOORBEAM AT STA 834 RBL 13. ROUTED OUT DAMAGED AREA IAW TIMCO SRM STD 5310-001 PG 6 AND MID FOR 2 REPAIR ANGLES IS 7075-0 .071 PO NR 297242 IAW TIMCO STD REPAIR MANUAL 5310-001 PG 4 & 6. FABBED 2 ANGLES AND FILLMay 8, 2000 · N894UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS00832715Attach Fitting · corrodedINSPECTION TYPE:C2, T-ANGLE ATTACH BRACKET AND RIB AT STA 802 RRL 40 CORRODED. REMOVED 3641315-502 FITTING. REMOVED CORRODED DOUBLER. FAB NEW DOUBLER IAW DAC DWG 5773275. REMOVED CORROSION FROM WEB IAW DC8 SRM 51-1-8, WITHIN LIMITS IAW DC8 SRM 53-2-0. REMay 8, 2000 · N894UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00832714Angle · corrodedINSPECTION TYPE:C2, CORROSION ON L28L STA 1170, LWR AFT PIT. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8. AREA OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 5May 8, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832713Fitting · crackedINSPECTION TYPE:C2, AFT ACCESSORY COMPARTMENT LONGERON 35L END FITTING IS CRACKED STA 1610. REMOVED THE PLACED FITTING (P/N 4646403) IAW DC8 SRM 51-7-20D.May 8, 2000 · N894UP · Doug DC873F · Fuselage Main, StructureSDR UPS00832710Angle · corrodedINSPECTION TYPE:C2, CORROSION ON L28L STA 1170, LWR AFT PIT. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8, AREA OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 53-2-2 & 51-20D. ALODINED ANMay 8, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832702Fitting · crackedINSPECTION TYPE:C2, AFT ACCESSORY COMPARTMENT, LONGERON 35R, END FITTING IS CRACKED, STA 1610. REMOVED AND REPLACED FITTING, (P/N 4646403) IAW DC8 SRM 51-1-20D.May 8, 2000 · N894UP · Doug DC873F · Fuselage Main, StructureSDR UPS00832661Cargo Track · corrodedINSPECTION TYPE:C123, STA 180 LONG 33L CARGO TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED IAW DWG 5759223 AND SRM 51-3-0.May 8, 2000 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832660Seat Track · corrodedINSPECTION TYPE:C123, STA 960 BL 0 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-3 FIG 8A.May 8, 2000 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
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