Boeing 727-2A1

Service difficulty reports · 502

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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 = '7272A1'
  ORDER BY difficulty_date DESC"

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SDR FOTR20006NR5353Seal Depressor · dentedC1 DOOR FWD LOWER CORNER, SEAL DEPRESSOR IS DENTED. REPAIRED ON FASI WO 20006, N/R 05353. REMOVED AND REPLACED SEAL DEPRESSOR AT FORWARD DOOR FWD LOWER CORNER AT STA 560 WITH P/N 65-57146-4 IAW B 727 SRM 51-30-2, REV 102.Jan 30, 2010 · N286SC · Boeing 7272A1 · Cargo/Baggage DoorsSDR FOTR20006NR4915Seal Depressor · crackedC2 DOOR FWD SEAL DEPRESSOR IS CRACKED BETWEEN 1ST DOORSTOP AND LOWER ROLLER. REPAIRED ON FASI WO 20006, N/R 04915. REPAIRED C-2 DOOR FWD SEAL DEPRESSOR BETWEEN 1ST DOOR STOP AND LOWER ROLLER STA 950E IAW B727 SRM 51-10-2, REV 102. MATERIAL USED: FORMED ANGLJan 29, 2010 · N286SC · Boeing 7272A1 · Cargo/Baggage DoorsSDR FOTR20006NR4955Skin · crackedRT WING FIXED L/E NR 4 KREUGER FLAP CUTOUT INBD FWD EDGE DOUBLER IS CRACKED. REPAIRED ON FASI WO 20006, N/R 04955. REPAIRED RT WING FIXED L/E NR 4 KRUEGER FLAP CUTOUT EDGE DOUBLER AT FWD INBD CORNER IAW B727 SRM 51-40-4 FIG 1 AND 57-20-2 FIG 1, REV 102. MATJan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge DevicesSDR FOTR20006NR4962Bracket · crackedRT WING FIXED L/E NR 5 KREUGER FLAP ACTUATOR BRACKET INBD SIDE IS CRACKED. REPAIRED ON FASI WO 20006, N/R 04962. REPAIRED RT WING L/E NR 5 KRUEGER FLAP ACTUATOR ATTACH BRACKET AT INBD SIDE IAW B727 SRM 57-10-2 FIG 3, REV 102 AND BOEING DWG 65-16269 SH 4, REVJan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge DevicesSDR FOTR20006NR4963Bracket · crackedRT WING FIXED L/E NR 5 KREUGER FLAP ACTUAOR BRACKET OTBD SIDE IS CRACKED. REPAIRED ON FASI WO 20006, N/R 04963. REPAIRED RT WING L/E NR 5 KRUEGER FLAP ACTUATOR ATTACH BRACKET AT OTBD SIDE IAW B727 SRM 57-10-2 FIG 3, REV 102 AND BOEING DWG 65-16269 SH 4, REV Jan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge DevicesSDR FOTR20006NR4979Structure · damagedRT WING NR 6 SLAT T/E IS DAMAGED AT SLAT STA 168. REPAIRED ON FASI WO 20006, N/R 04979. INSTALLED DOUBLER REPAIR TO RT WING NR 6 SLAT T/E AT SLAT STA 168.0 IAW B727 SRM 57-50-1 FIG 2, 57-50-3 FIG 10 AND 51-30-8 FIG 4, REV 102. CUTOUT DIM: 7.0 BY 0.50. MATEJan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge DevicesSDR FOTR20006NR4980Skin · tornRT WING FIXED L/E NR 6 SLAT INBD HOOK SEAL CUTOUT AFT SIDE HAS 2 MISSING FASTENERS. REPAIRED ON FASI WO 2000654. N/R 04980- REPAIRED RT WING FIXED L/E AT NR 6 SLAT INBD HOOK SEAL CUTOUT AFT SIDE AT STA 519 IAW SRM 57-30-4 FIG 9, REV 102. MATERIAL USED: DOUJan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge DevicesSDR FOTR20006NR4981Skin · crackedRT WING FIXED L/E NR 6 SLAT OTBD HOOK SEAL CUTOUT AFT SIDE IS CRACKED. REPAIRED ON FASI WO 20006. N/R 04981- REPAIRED RT WING FIXED L/E AT NR 6 SLAT OTBD HOOK SEAL CUT-OUT AFT SIDE AT STA 530.0 IAW SRM 57-30-4 FIG. 9 AND 51-10-1, REV 102. CUT- OUT DIM: 8.50" Jan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge DevicesSDR FOTR20006NR4982Skin · crackedRT WING NR 6 SLAT LOWER SKIN COMMON TO TRACK IS CRACKED IN 2 PLACES SLAT SLAT STA 216. REPAIRED ON FASI WO 20006. N/R 04982- INSTALLED DOUBLER REPAIR TO RT WING NR 6 SLAT LOWER SKIN AT SLAT STA 216.0 IAW SRM 57-50-3 FIG 1, REV 102. MATERIAL USED: 2024-T3, 0.Jan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge DevicesSDR FOTR20006NR5029Skin · crackedRT WING NR 8 SLAT TE HAS 2 CRACKS COMING FROM SCREW HOLE SLAT STA 407.5. REPAIRED ON FASI WO 20006. N/R 05029- INSTALLED DOUBLER REPAIR TO RT WING NR 8 SLAT T/E AT SLAT STA 407.5 IAW SRM 57-50-3 FIG 10, REV 102 MATERIAL USED: DOUBLER- 7075-T6’ 0.125", DIM: 8.Jan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge DevicesSDR FOTR20006NR5044Skin · delaminatedRT WING AILERON OTBD T/E WEDGE IS DELAMINATED AT OTBD END. REPAIRED ON FASI WO 20006. N/R 05044- REPAIRED RT WING OTBD T/E WEDGE BY HOT BONDING REPAIR IAW SRM 51-40-20, REV 102, CUT OUT, AND FILLER DIM: 1.0" X 1.0", 3.0" X 1.0", AND 4.0" X 1.0". MATERIAL USJan 29, 2010 · N286SC · Boeing 7272A1 · AileronsSDR FOTR20006NR5046Skin · delaminatedRT WING OTBD AFT FLAP IS DELAMINATED STA WBL 348. REPAIRED ON FASI WO 20006, N/R 05046. REPAIRED RT WING OTBD AFT FLAP AT WBL 348.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.012, DIM: 2.0 BY 6.0, FILLER; 7075-TJan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge FlapsSDR FOTR20006NR5049Skin · gougedRT WING INBD FORE FLAP OB LOWER SKIN IS GOUGED. REPAIRED ON FASI WO 20006. N/R 05049- REPAIRED RT WING INBD FORE FLAP OTBD LOWER SKIN AT STA 240.0 IAW SRM 57-50-4 FIG 1, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.063", DIM: 5.250" X 4.125".Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge FlapsSDR FOTR20006NR5051Skin · delaminatedRT WING INBD AFT FLAP UPPER SURFACE IS DELAMINATED STA130. REPAIRED ON FASI WO 20006, N/R 05051. REPAIRED RT WING INBD AFT FLAP UPPER SURFACE AT WBL 130.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.016, DIM: 14.Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge FlapsSDR FOTR20006NR5050Skin · damagedRT WING AFT IB FLAP LOWER SURFACE HAS GRAVEL DAMAGE AT INBD END. REPAIRED ON FASI WO 20006. N/R 05050- REPAIRED RT WING AFT INBD FLAP LOWER SURFACE AT WBL 115.0 BY HOT BONDING REPAIR IAW SRM 51-40-20 AND 57-50-2 FIG 3, REV 102. MATERIAL USED: DOUBLER- 7075-T6Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge FlapsSDR FOTR20006NR5222Spar · damagedC/W AD2008-17-14 SB 727-55-0089 ELEVATOR REAR SPAR AT THE TAB HINGE LOC. IAW PARA (A) REPLACEMENT OF THE ELEVATOR REAR SPAR AND SUPPORT FITTING IAW PART 2 OF S/B 727-55-0089 REV 1 (RT). REPAIRED ON FASI WO 20006. N/R 05222- R & R ELEVATOR REAR SPAR AND SUPPJan 29, 2010 · N286SC · Boeing 7272A1 · Elevator, Spar/RibSDR FOTR20006NR5170Angle · crackedLT IB MIDFLAP LOWER AFT CLOSE OUT CHORD ANGLE AT ACTUATOR ROD CUTOUT HAS ONE CORNER CRACKED. REPAIRED ON FASI WO 20006. N/R 05170- R & R LT INBD MID FLAP LOWER AFT CLOSEOUT CHORD ANGLE AT ACTUATOR ROD CUT OUT AT WBL 108 IAW SRM 57-50-2 FIG. 5 AND 51-40-4 FIGJan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge FlapsSDR FOTR20006NR5171Skin · dentedLT INBD AFT FLAP INBD LOWER SURFACE HAS 2 LARGE SHALLOW DENTS. REPAIRED ON FASI WO 20006. N/R 05171- REPAIRED LT WING INBD AFT FLAP LOWER SURFACE AT WBL 86.0 BY HOT BONDING REPAIR IAW SRM 51-40-20, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.020", DIM: 11.50Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge FlapsSDR FOTR20006NR5184Skin · chafedLT OB FORE FLAP UPPER OB LE WBL 485 HAS A DEEP CHAFED AREA ON THE REPAIR DOUBLER. REPAIRED ON FASI WO 20006. N/R 05184- R & R PREVIOUS DOUBLER AT LT WING OTBD FORE FLAP OTBD L/E AT WBL 485.0 IAW SRM 57-50-4 FIG 1, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.0Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge FlapsSDR FOTR20006NR5164Skin · delaminatedNR 5 SPOILER PANEL AFT EDGE SKIN IS DELAMINATED. REPAIRED ON FASI WO 20006, N/R 05164. REPAIRED NR 5 SPOILER PANEL AFT EDGE AT WBL 217.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20 AND 57-50-2 FIG 9, REV 102. MATERIAL USED DOUBLER; 7075-T6, 0.025, DIM: 45.0Jan 29, 2010 · N286SC · Boeing 7272A1 · SpoilersSDR FOTR20006NR5160Skin · debondedNR 6 SPOILER PANEL LOWER IB SKIN DOUBLER & HINGE FITTING IS DISBONDED. REPAIRED ON FASI WO 20006. N/R 05307- INSTALLED BONDED REPAIR DOUBLER TO RT WING NR 9 SPOILER T/E AT WBL 130.0 IAW SRM 51-40-20, REV 102. MATERIAL USED: FILLER; 7075-T6, 0.020", DIM: 2.0" Jan 29, 2010 · N286SC · Boeing 7272A1 · SpoilersSDR FOTR20006NR5211Seal Depressor · dentedC1 DOOR AFT LOWER CORNER OF SEAL DEPRESSOR HAS 2 DENTS. REPAIRED ON FASI WO 20006, N/R 05211. REMOVED AND REPLACED SEAL DEPRESSOR P/N 65-57146-3 AT C1 DOOR AFT LOWER CORNER, STA 620 IAW B727 SRM 51-30-2 AND 51-30-05, REV 102.Jan 29, 2010 · N286SC · Boeing 7272A1 · Cargo/Baggage DoorsSDR FOTR20006NR5059Frame · crackedMAIN CARGO AREA, BS 480, BETWEEN STR 16L-17L, CRACKED FRAME. REPAIRED ON FASI WO 20006, N/R 05059. REPAIRED FRAME AT STA 480 BETWEEN STR 16L AND 17L IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3, REV 102. MATERIAL USED: 7075-T6, 0.050, DIM: 9.0 BY 3. CUT OUJan 29, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, FrameSDR FOTR20006NR4858Support Fitting · damagedVENTRAL STAIRS, TR LOWER TORQUE BOX, BS 1263 UPPER SUPPORT FITTING HAS HOLE DRILLED INTO RADIUS. REPAIRED ON FASI WO 20006, N/R 04858. REMOVED AND REPLACED UPPER SUPPORT FITTING AT RT LOWER TORQUE BOX WEB AT VENTRAL STAIRS STA 1263 WITH P/N 65C27137-1 IAW B7Jan 28, 2010 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR FOTR20006NR4859Web · crackedVENTRAL STAIRS, LT LOWER TORQUE BOX, LIGHTNING HOLE IS CRACKED AT BS 1223. REPAIRED ON FASI WO 20006, N/R 0485. REPAIRED LT LOWER TORQUE BOX WEB AT STA 1223 IAW B727 SRM 53-10-2, FIG 6 AND 51-40-2, FIG 1, REV 102. MATERIAL USED: 7075-T6, 0.032, DIM: 1.50 BYJan 28, 2010 · N286SC · Boeing 7272A1 · Entrance StairsSDR FOTR20006NR4860Web · crackedVENTRAL STAIRS, RT LOWER TORQUE BOX WEB, LIGHTNING HOLE IS CRACKED AT BA 1323. REPAIRED ON FASI WO 20006. 44. N/R 04860. REPAIRED RT LOWER TORQUE BOX WEB AT STA 1323 IAW B727 SRM 53-10-2, FIG 6 AND 51-40-2, FIG 1, REV 102. MATERIAL USED: 7075-T6, 0.032, DIJan 28, 2010 · N286SC · Boeing 7272A1 · Entrance StairsSDR FOTR20006NR4879Nose Cowl · chafedNR 3 ENGINE AFT T/E FROM 2-3 O`CLOCK POSITION CHAFED AND HOLE WORN THRU AS MARKED A NOSE COWL. REPAIRED ON FASI WO 20006, N/R 04879. REPAIRED NR 3 ENGINE NOSE COWL T/E FROM 2 TO 3 O’CLOCK POSITION IAW B727 SRM 54-10-3 FIG 3, REV 102. MATERIAL USED: ANGLE- 2Jan 28, 2010 · N286SC · Boeing 7272A1 · Engine Air Intake SystemSDR FOTR20006NR4888Nose Cowl · gougedNR 3 ENGINE NOSE COWL AT 4 O`CLOCK POSITION T/E GOUGED. REPAIRED ON FASI WO 20006, N/R 04888. REPAIRED NR 3 ENGINE NOSE COWL T/E AT 4 O’CLOCK POSITION IAW B727 SRM 54-10-3 FIG 3, REV 102. MATERIAL USED: ANGLE; 2024-T3, 0.063, DIM: 10.0 BY 2.0, FILLER; 2024-Jan 28, 2010 · N286SC · Boeing 7272A1 · Engine Air Intake SystemSDR FOTR20006NR4905Skin · crackedLT MLG WING DOOR AT AFT HINGE AREA, SKIN IS CRACKED AFT OF SEAL RETAINER. REPAIRED ON FASI WO 20006, N/R 04905. REMOVED AND REPLACED PREVIOUS REPAIR TO LT MLG WING DOOR AT AFT HINGE AREA WBL 124 IAW S/B 727-32-318 FIG 4, REV IR. MATERIAL USED: DOUBLER; 2024Jan 28, 2010 · N286SC · Boeing 7272A1 · Wing Miscellaneous StructureSDR FOTR20006NR4913Depressor · chafedC2 DOOR LOWER SEAL DEPRESSOR IS CHAFED AT FWD END. REPAIRED ON FASI WO 2000, N/R 04913. REMOVED AND REPLACED C-2 DOOR LOWER SEAL DEPRESSOR AT STA 950F WITH P/N 65-60234-501 IAW B727 SRM 51-30-2, REV 102.Jan 28, 2010 · N286SC · Boeing 7272A1 · Cargo/Baggage DoorsSDR FOTR20006NR4771Skin · damagedAFT AIRSTAIR RT T/E PREVIOUS REPAIR BENT AT AFT EDGE. REPAIRED ON FASI W/O NR 20006, N/R 04771. REMOVED AND REPLACED PREVIOUS REPAIR TO AFT AIRSTAIR RT T/E AT STA 1342 IAW B727 SRM 52-10-2 FIG 4, REV 102. MATERIAL USED SKIN; 2024-T3, 0.040, DIM: 42.0 BY 38.Jan 28, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR FOTR20006NR4763Intercostal · crackedAFT PIT INTERCOSTAL IS CRACKED BETWEEN BS 950-950A BETWEEN STR 21R-20R. REPAIRED ON FASI WO 20006, N/R 04763. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 950 AND 950A AND BETWEEN STR 20R AND 21R IAW B727 SRM 53-10-2 FIG 2 AND 53-10-2 FIG 5, REV 102. MATERIJan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR FOTR20006NR4757Angle · corrodedNOSE WHEEL WELL INSIDE WEB BOX AT BOTTOM OF VERTICAL SUPPORT, ANGLE CORRODED AND CRACKED BS 294.5. REPAIRED ON FASI WO 20006, N/R 04757. REMOVED AND REPLACED TEE ANGLE ON BOTTOM OF VERTICAL SUPPORT AT STA 294.5 BETWEEN STR 25L AND 26L WITH P/N 65-16312-145 IJan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR FOTR20006NR4715Skin · dented(FOTR) DENT AT L FUSELAGE SKIN AT BS 356 BELOW STR 24L. REPAIRED ON FASI WO 20006. REPAIRED LT FUSELAGE SKIN AT STA 356.0 BETWEEN STR 24L AND 25L IAW DWG AJ07-53-102 REV. IR. 8110-3 DATED 02/12/2010 ISSUED. REWORKED LOWER SKIN LAP SEAM AND CUT OUT DAMAGED SECTJan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR FOTR20006NR4713Skin · bulgedRT FUSELAGE SKIN HAS SKIN SURFACE BULGE AT BS 350 ABOVE SR 21R. REPAIRED ON FASI WO 20006, N/R 04713. REMOVED AND REPLACED JACK PAD STRAP STIFFENER AT STA 350.0 BETWEEN STR 20R AND 21R WITH P/N 65-22589-8 IAW B727 SRM 51-30-5 AND 51-10-1, REV 102.Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR FOTR20006NR4709Stiffener · corroded(FOTR) CORROSION AT 227.8 BULKHEAD, BL 0 SKIN INTERIOR, JUST AFT OF EQUIPMENT BAY ACCESS DOOR. REPAIRED ON FASI WO 20006. N/R 04709- R & R DAMAGED STIFFENER AT BL 0 STA 227.8 IAW SRM 51-30-2, 53-10-1 FIG. 1, REV 102 AND DWG 69-15768. MATERIAL USED: 7075-T6,Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR FOTR20006NR4685Hinge · crackedEXT FUSELAGE MCD AFT MOST SEGMENT FUSELAGE SIDE HAS 2ND AFT LOBE CRACKED. REPAIRED ON FASI WO 20006. R & R MAIN CARGO DOOR AFT HINGE SECTION WITH PN MS20001-16-7200 AT STA 620 IAW B727 FREIGHTER MM, CH 52, FIG 5201B, REV. G.Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage, Door HingeSDR FOTR20006NR4658Skin · dentedDENT ON LT FUSELAGE SKIN BS 1319 STR 9L. REPAIRED ON FASI WO 20006, N/R 04658. INSTALLED REPAIR DOUBLER AT BS 1319 AND STR 9L IAW B727 SRM 53-30-2 FIG 2, REV 102. MATERIAL USED: 7075-T6, DIM 8.625 BY 9.25 BY 0.063.Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR FOTR20006NR4642Skin · dented(FOTR) DENT ON RT FUSELAGE SKIN AT BS 1100 ABOVE STR 19R. REPAIRED ON FASI WO 20006. N/R 04642 INSTALLED REPAIR DOUBLER AT BS 1100 ABOVE STR 19R, IAW SRM 53-30-3 FIG 3, REV 102 MATERIAL USED: 2024-T3 DIM. 12.25" X 9" X 0.071".Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR FOTR20006NR4712Skin · dentedMULTIPLE DENTS AT RT FUSELAGE SKIN SURFACE, PREVIOUS REPAIR DOUBLER AT BS 345.2 STR 24R. REPAIRED ON FASI WO 20006, N/R 04712. REMOVED PREVIOUS REPAIR DOUBLERS ON RT FUSELAGE SKIN AT STA 345 STR 24R AND INSTALLED ONE REPAIR DOUBLER FROM STA 321 TO 340, STR 2Jan 22, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR C8GA20090183Switch · defectiveDURING CLIMB OPERATION, WHILE RETRACTING THE FLAP FROM FLAPS 5 TO FLAPS 2. THE L/E FLAP AMBER LIGHT ILLUMINATED, FLIGHT ENGINEERS FLAP DISPLAY INDICATED NR 6 FLAP OUT. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMAug 30, 2009 · N286SC · Boeing 7272A1 · Leading Edge Slat Position Indicating SystemSDR C8GA20090179Actuator · leakingDURING CLIMB OPERATION A TOTAL "A" HYD SYS FAILURE OCCURRED. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. THE NR 3 SLAT ACTUATOR INBD FITTING WAS CRACKED. REMOVED AND REPLACED THE NR 3 SLAT ACTUATOR, REMOVEDAug 19, 2009 · N287SC · Boeing 7272A1 · Leading Edge Slat ActuatorSDR C8GA20090133Actuator · leakingFLT 721 FROM TOL TO ROC. AFTER DEPARTING THE RUNWAY THE GEAR WOULD NOT RETRACT, A LOSS OF SYSTEM "A" HYDRAULICS WAS NOTED. THE AIRCRAFT RETURNED TO TOL WHERE AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT Aug 4, 2009 · N287SC · Boeing 7272A1 · Leading Edge Slat ActuatorSDR C8GA20090107Transmitter · unserviceableFLT 740 FROM TOL TO RDU. DURING TAKEOFF ROLL THE # THREE EPR CIRCUIT BREAKER POPPED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE BLOCKS. INSPECTED ENGINE INLET AND EXHAUST, NO DEFECTS WERE NOTED. REMOVED AND REPLACED EPR TRANSMITTER, OPS CHECK GOOJul 7, 2009 · N286SC · Boeing 7272A1 · Engine Pressure Ratio (EPR)SDR C8GA20090076ADoor · unsecureFLT 711 FROM SAN TO PHX. DURING CLIMB OPERATION A LOSS OF CABIN PRESSURE CONTROL WAS EXPERIENCED FOLLOWED BY AN AFT ENTRY DOOR LIGHT. THE AIRCRAFT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT IN PHX. POST FLIGHT INSPECTION WAS PERFORMED. THE AFT ENTRY DOOMay 22, 2009 · N287SC · Boeing 7272A1 · Passenger/Crew DoorsSDR C8GA20090062Latch · dirtyFLT 1738- DURING CRUISE OPERATION THE MAIN CARGO DOOR RED LIGHT ILLUMINATED, ON BULKHEAD BOTH VENT DOOR AND HOOK UNLOCKED LIGHTS WERE ILLUMINATED. POST FLIGHT INSPECTION WAS PERFORMED. CLEANED AND LUBRICATED DOOR LATCHES AND SWITCHES. OPERATIONAL AND PRESSUApr 23, 2009 · N287SC · Boeing 7272A1 · Cargo/Baggage DoorsSDR C8GA20090136Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 11 SPOILER PANEL IS DELAMINATED AT UPPER T/E. REMOVED DAMAGED AREA DIM. 5" X 2", FABRICATED FILLER FROM 2024 T3 .025" DIM 5" X 2" AND FABRICATED DOUBLER FROM 2024 T3 .025" DIM. 9" X 4".Mar 23, 2009 · N287SC · Boeing 7272A1 · SpoilersSDR C8GA20090135Panel · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 9 SPOILER PANEL IS DELAMINATED AT UPPER O/B SURFACE. REMOVED DAMAGED AREA DIM. 5" X 2", FABRICATED FILLER FROM 2024 T3 .025" DIM 5" X 2" AND FABRICATED DOUBLER FROM 2024 T3 .025" DIM. 9Mar 23, 2009 · N287SC · Boeing 7272A1 · SpoilersSDR C8GA20090134ASupport Angle · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE # 6 SLAT I/B & O/B ROD END SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED I/B & O/B RIBS AT # 6 SLAT WS 530. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.Mar 23, 2009 · N287SC · Boeing 7272A1 · Wing Miscellaneous StructureSDR C8GA20090137ASkin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 12 SPOILER PANEL IS DELAMINATED AT I/B UPPER SURFACE. REMOVED DAMAGED AREA DIM. 2" X 2", FABRICATED FILLER FROM 2024 T3 .025" DIM 2" X 2" AND FABRICATED DOUBLER FROM 2024 T3 .025" DIM. Mar 23, 2009 · N287SC · Boeing 7272A1 · Spoilers
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