Boeing 727-30C

Service difficulty reports · 931

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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 = '72730C'
  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 UPS97221814Spar · crackedINSPECTION TYPE-C, NR 4 SLAT AFT SPAR CRACKED AT O/B END. INSTALLED DOUBLERS PER SRM 51-40-4.Jan 9, 1997 · N906UP · Boeing 72730C · Leading Edge DevicesSDR UPS97221800Threshold · corrodedINSPECTION TYPE-C, CORROSION AROUND THE UPPER AND LOWER NUTPLATE AREA ON THE FWD ENTRY DOOR LOWER SILL THRESHOLD ATTACH ANGLES WL 208 LBL 60 TO 67. REMOVED ALL CORROSION TO WITHIN LIMITS. REMOVED AND REPLACED AFFECTED PARTS SRM 53-10-01, 51-30-02.Jan 5, 1997 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS97221801Fitting · corrodedINSPECTION TYPE-C, CARGO NET ATTACH FITTING CORRODED AT BS 364 LBL 5 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED FITTING IAW SRM 51-10-1, 51-10-2, 51-10-6, 51-30-2, 51-30-5.Jan 4, 1997 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS97221802Ribs · crackedINSPECTION TYPE-C, R/W NR 6 SLAT ACTUATOR RIBS CRACKED AT AFT FASTENER HOLE BOTH SIDES OF ACTUATOR. SLAT WAS REPLACED ON NRC 494364 IAW M/M 27-81-11.Jan 3, 1997 · N906UP · Boeing 72730C · Leading Edge DevicesSDR DHL96701010Bulb · failedON APPROACH, BROUGHT GEAR HANDLE TO DOWN POSITION, DID NOT GET GREEN NOSE GEAR INDICATION. WENT TO ALTERNATE PROCEDURE, PUT GEAR HANDLE BACK TO THE DOWN POSITION AND HAD NORMAL INDICATIONS, COMPLETED THE ALTERNATE PROCEDURE. CHECKED NOSE GEAR LOCK AND POSITIDec 11, 1996 · N701DH · Boeing 72730C · Landing Gear Position and WarningSDR UPS96221737Mix Valve · inoperativeINSPECTION TYPE-N/A, FUMES SMELLED IN COCKPIT LIKE BURNING RUBBER. CHECKED CARGO AREA AND NO FUMES DETECTED. *S/D* REMOVED AND REPLACED LEFT PACK MIX VALVE DUCT (P/N 65-23579-2) OPS CHECK LEFT PACK OK. THIS CLEARS M120048 PLACARD REMOVED.Dec 5, 1996 · N919UP · Boeing 72730C · Cabin Cooling SystemSDR DHL96703005Actuator · failedNR 1 L/E WOULD NOT RETRACT WHEN FLAPS SELECTED FROM ZERO. REMOVED AND REPLACED L/E SLAT ACTUATOR OPS AND LEAK CHECK OK.Nov 26, 1996 · N703DH · Boeing 72730C · Leading Edge Slat ActuatorSDR DHL96703004Oilcooler Tube · pulled looseLOST OIL PRESSURE INDICATION ON NR 1 ENGINE FOLLOWED BY QUANTITY DECREASING. ENGINE WINDMILLED FOR 13 TO 14 MINUTES, NO PRESSURE INDICATED. FOUND OIL COOLER IN TUBE ASSY PULLED OUT OF GEARBOX. INSTALLED HELICOILS IN GEARBOX AND INSTALLED LINE, NO LEAKS NOTEOct 30, 1996 · N703DH · Boeing 72730C · Engine Fuel/Oil CoolerSDR UPS96221330Bleed Air So Vlv · inoperativeINSPECTION TYPE-N/A, SMELL/ODOR OF BURNT OIL/RUBBER WHEN USING NR 1 BLEED AIR FOR LEFT PACK SMELL GOES AWAY WHEN AIR SOURCE SWITCHED TO ENG NR 2. NR 1 ENG BLEED AIR S/O VALVE INOP, PER MEL 36-6-1-2 M-116899.Oct 15, 1996 · N919UP · Boeing 72730C · Pneumatic Distribution SystemSDR DHL96701009Container · not sealedNOXIOUS ODOR DETECTED IN FORWARD CONTROL CABIN AND BECAME STRONGER AFTER TAXI IN. WHEN COCKPIT DOOR WAS OPEN, THE ODOR WAS EXTREMELY STRONG. FOUND ODOR TO BE FROM ONE CONTAINER WITH NEOPRENE SOLES FROM GDL PER A/C CREW . SEALED CONTAINER WITH PLASTIC COVERIAug 21, 1996 · N701DH · Boeing 72730C · Cargo CompartmentsSDR UPS96220910Fitting · crackedINSPECTION TYPE: C. 940 FRAME FITTING RT SIDE IS CRACKED IN 3 PLACES, 1 ON FRONT AND 2 ON AFT SIDE. REPAIRED 940 FITTING RT SIDE IAW EO'S B727-5310-3737A, B727-5310-1001A.Aug 4, 1996 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS96220909Clip · corrodedINSPECTION TYPE: C. CORROSION ON FRAME CLIP, NOSE W/W LOWER LOBE, STA 312 RT SIDE ON FLOOR SKIN. REMOVED, FAB'D AND INSTALLED REPLACEMENT ANGLES PER SRM 51-10-01 AND SRM 51-30-02.Aug 3, 1996 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS96220912Skin · corrodedINSPECTION TYPE: C. LOWER RUDDER SKIN AT FRONT SPAR IS CORRODED. REMOVED AND REPLACED RUDDER (LOWER) IAW M/M 27-20-11 AND MM 27-20-20.Aug 1, 1996 · N919UP · Boeing 72730C · Rudder, Plate/SkinSDR DHL96703003Actuator · jammedSTABILIZER TRIM JAMMED FROM TOP OF DESCENT, WOULD NOT STRIM NOSE UP. COMPLIED WITH ALTERNATE PROCEDURE. CLEANED AND LUBED STAB TRIM JACKSCREW DUE TO EXCESSIVE MOISTURE. REPLACED MAIN STAM ACTUATOR, ACTUATED STAB TRIM FULL TRAVEL AND NO DEFECTS NOTED.Aug 1, 1996 · N703DH · Boeing 72730C · Stabilizer ActuatorSDR DHL96701008Oxy Reg Valve · not openAPPROXIMATELY 30 MIN AFTER TAKEOFF, THE O2 QUANITY DROPPED TP 200 PSI. SERVICED O2 PER M/M 12-15-11, FOUND REGULATOR VALVE NOT FULLY OPEN. LEAK CHECK OK.Jul 30, 1996 · N701DH · Boeing 72730C · Crew Oxygen SystemSDR DHL96701007Ind Light · malfunctionedGREEN LIGHT WOULD NOT ILLUMINATE WHEN GEAR SELECTED DOWN, GEAR LIGHT WORKED AFTER CYCLING GEAR. PERFORMED LANDING GEAR LOCK AND POSITION INDICATION TEST PER MM 32-61-21, NO DEFECTS NOTED.Jul 27, 1996 · N701DH · Boeing 72730C · Landing Gear Position and WarningSDR DHL96703002Mod Valve · malfunctionedAIRCRAFT WOULD ONLY PRESSURIZE TO .5 PSI DIFFERENTIAL 8,500 FEET CABIN ALT AT 10,000 AIRCRAFT ALT, NOTED 26 PSI SPLIT ON DUCT PRESSURE GAUGES. REMOVED AND REINSTALLED LEFT OUTFLOW VALVE. REMOVED AND REPLACED NR 1 ENG 13TH STAGE MOD VALVE AND LEFT PACK 35 DEGJul 19, 1996 · N703DH · Boeing 72730C · Pneumatic Distribution SystemSDR UPS96220911Skin · corrodedINSPECTION TYPE: C. UPPER RUDDER SKIN RT SIDE HAS CORROSION AT RUDDER FRONT SPAR. REMOVED AND REPLACED UPPER RUDDER M/M 27-20-01 AND MM 27-20-00.Jul 16, 1996 · N919UP · Boeing 72730C · Rudder, Plate/SkinSDR UPS96220248Water Sep Bag · dirtyDIRTY WATER SEPARATOR BAG CAUSING ODOR IN FLIGHT DECK. REPLACED BAG.May 31, 1996 · N919UP · Boeing 72730C · Humidity Control SystemSDR DHL96702002Directional Gyro · malfunctionedON CRUISE, COMPASS CARD IN HSI PRECESSES. REMOVED AND REPLACED DIRECTIONAL GYRO AND REMOVED WATER FROM E AND E BAY, MM 34-20.Apr 30, 1996 · N702DH · Boeing 72730C · Directional Gyro and Indicating SystemSDR DHL96703001Pitot Heat · inoperativeRIGHT HAND PITOT HEAT INOP LIGHT ON, NO AMP READING. REMOVED AND REPLACED RIGHT HAND PROBE.Feb 1, 1996 · N703DH · Boeing 72730C · Pitot/Static Anti-Ice SystemSDR UPS205187Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 1 BEAM UPPER I/B L-ANGLE IS CRACKED 1 INCH ON FWD END IN RADIUS. FABRICATED BEAM L-ANGLE IAW SRM 51-40-3, 52-30-1 AND INSTALLED REPAIR ANGLE IAW SRM 51-30-2.Jan 1, 1996 · N917UP · Boeing 72730C · Cargo/Baggage DoorsSDR UPS504885Battery · dischargedWHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-101. OPS CHECKED GOOD PER MM 33-50-101.Oct 26, 1995 · N212UP · Boeing 72730C · Emergency LightingSDR UPS504884Pos Switch · failedCREW REPORTED ON FINAL, THE GREEN NOSE GEAR LIGHT SUDDENLY WENT OUT AND THE GEAR HORN CAME ON. GEAR WAS CYCLED AND ALL THREE GEAR LIGHTS ILLUMINATED AGAIN. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR POSITION SWITCH AND THE NOSE GEAR LOCK SWITCH IAW MM 32Oct 26, 1995 · N918UP · Boeing 72730C · Landing Gear Position and WarningSDR UPS204853Pack · failedCREW REPORTED, DURING TAKEOFF THRUST AND CLIMBOUT INCREASINGLY BAD FUMES AND SMELL. TURNED OFF NR 1 BLEED AND NR 1 PACK, SMELL WENT AWAY. LATER USED NR 2 BLEED TO SUPPLY NR 1 PACK AND SMELL AND FUMES WERE NOT EXISTANT. DEFERRED MAINTENANCE ITEM ASSIGNED PEROct 23, 1995 · N906UP · Boeing 72730C · Cabin Cooling SystemSDR UPS204810Acm · malfunctionedCREW REPORTED, BTB DUE TO SMOKE IN FLIGHT DECK. RAN ENG 1 AT A TIME, ISOLATED PROBLEM TO LT PACK AND DEFERRED PACK PER MEL. REMOVED AND REPLACED LT AIR CYCLE MACHINE PER MM 21-51-12 PG 401. OPS CHECK OFF APU AND ALL ENGS DURING TAXI, NO DEFECTS NOTED.Oct 17, 1995 · N906UP · Boeing 72730C · Cabin Cooling SystemSDR UPS204646Te Skin · delaminatedWHILE ON GROUND MAINTENANCE, FOUND LEFT INBD FLAP TRAILING EDGE HAS DELAMINATION. REPAIRED TRAILING EDGE FLAP PER SRM 727-51-40-6.Oct 1, 1995 · N917UP · Boeing 72730C · Trailing Edge FlapsSDR 96ZZZM435Skin · crackedDURING C-CHECK, FOUND LEFT WING UPPER SURFACE, NR 3 SPOILER NR 3 HINGE CUTOUT IS CRACKED. REMOVED NR 3 SPOILER PANEL. STOP DRILLED AS PER SRM 51-10-1. FABRICATED 2024 PLUS 3 .050 4 INCH BY 4 INCH DOUBLER AS PER SRM 57-30-4. INSTALLED FASTENERS ON UPPER SURFSep 6, 1995 · N702DH · Boeing 72730C · Wing, Plate/SkinSDR 96ZZZM434Skin · dentedDURING C-CHECK, FOUND MSI 702-0125-1003, DENT AT RW SLAT STATION 193.5. CUT OUT DENTED (DAMAGED) AREA. INSTALLED FLUSH REPAIR PER SRM 57-50-3 FIG 1 (REPAIR II). INSTALLED DOUBLER .080 2024-0 4.5 INCH BY 7.25 INCH FILLER .063 2024-T3 2.75 INCH BY 5 INCH. FASep 6, 1995 · N702DH · Boeing 72730C · Leading Edge DevicesSDR 96ZZZM433Skin · dentedDURING C-CHECK, FOUND MSI 702-0119-1002 DENT AT STATION 178 RIGHT SIDE FORWARD OF WINDOW POST E-F. REWORKED DENT ON STATION 178 RIGHT SIDE FORWARD WINDOW POST, FOUND OUT OF LIMITS AS PER SRM 51-40-1. FABRICATED DOUBLER AS PER SRM 53-30-3 10 INCHES BY 13 INCHSep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM432Skin · corrosionDURING C-CHECK, FOUND FUSELAGE SKIN BULGED BETWEEN STRINGER 25L AND 26L STATION 141. LFEC INSPECTED C/W PER NDT MANUAL 51-00-00 PART 6 FIG 5 MORE THAN 10 PERCENT NOTED. REMOVED FASTENERS AROUND DAMAGED AREA IAW SRM 51-30-2. CUT OUT DAMAGED AREA 4 INCH BY 4 Sep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM431Skin · crackedDURING C-CHECK, FOUND FUSELAGE SKIN CRACKED AT TAIL SKID CUTOUT STATION 1223. STOP DRILL PER SRM 51-10-1. ZYGLO CHECKED END OF CRACK, FOUND ADDITIONAL CRACK EMMINATING FROM HOLE. CUT OUT AREA DAMAGED PER SRM 51-10-1. FABRICATED DOUBLER AND INSTALLED DOUBLESep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM430Fitting · crackedDURING C-CHECK, FOUND BS 940 FITTING LEFT SIDE CRACK AT REPAIR BETWEEN TWO FASTENERS FWD SIDE UNDER CABIN FLOOR PANEL (VISUAL PER SB 727-53-190 INSP). REMOVED FAST FOR ACCESS FOR HFEC PER SRM 51-30-2. ACCOMPLISHED HFEC INSPECTION OF SUSPECTED CRACK AREA, FOUSep 6, 1995 · N702DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM429Seat Track · corrodedDURING C-CHECK, FOUND FORWARD PIT BULGE RIGHT SEAT TRACK CRACKED AT RADIUS CUT OUTS AT STATION 540, 560, AND 580. REMOVED SECTION OF TRACK PER SRM 51-30-2. CUT OUT DAMAGED AREA OF SEAT TRACK STATION 520 TO STATION 600 AS PER SRM 53-10-5. INSTALLED SEAT TRACSep 6, 1995 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZM428Stringer · corrosionDURING C-CHECK, FOUND FUSELAGE BULGE STATION 740 STRINGER 25L AND CLIP HAVE CORROSION. CLIP WAS REMOVED AND CUT OUT DAMAGED AREA OF STRINGER 25L BS 740 7 INCHES APPROXIMATELY AS PER SRM 53-10-3. REPLACED CLIP PER SRM 51-10-1 PAGE 4. INSTALLED STRINGER REPAISep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, Longeron/StringerSDR 96ZZZM427Frame · corrosionDURING C-CHECK, FOUND FRAME CORROSION ON FORWARD SIDE AT PREVIOUS REPAIR, STATION 304 STRINGER 21-22 LEFT. REMOVED FASTENERS AND OLD REPAIR PER SRM 51-30-2. CUT OUT DAMAGE AREA PER SRM 51-40-4 3 INCHES BY 4 INCHES. CLEANED ALODINED AND PRIMED PER SRM 51-10-Sep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, FrameSDR 96ZZZM426Skin · corrosionDURING C-CHECK, FOUND CABIN FS 760 RIGHT SIDE BETWEEN WING CENTER TANK AND FLOOR LEVEL RBL 67, HEAVY CORROSION ON FRAME AND PRESS PAN WEB. REMOVED OUTSIDE FAIRING FOR S/M ACCESS AND REMOVED FASTENERS PER SRM 51-30-2. REMOVED CORROSION ON FRAME PER SRM 51-10-Sep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM425Frame · crackedDURING C-CHECK, FOUND FS 870 RIGHT FRAME HAS CRACK INDICATION AT ROW 2 BETWEEN 3RD AND 4TH FASTENERS FROM TOP VERIFIED BY EDDY CURRENT AND UT. REMOVED FORWARD SPLICE ANGLE PER SRM 51-30-2. ACCOMPLISHED HFEC AS PER PART G NDT MANUAL 51-00-00 FIG 4. ACCOMPLISSep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, FrameSDR 96ZZZM424Stringer · crackedDURING C-CHECK, FOUND FORWARD E/E COMPARTMENT, STRINGER 22L IS CRACKED IN TWO PLACES JUST AFT OF FUSELAGE FRAME AT FS 312. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF STRINGER 22L AT FS 312 AS PER SRM 53-10-3 16 INCHES APPROXIMATELY. FABRICATED STRINGER 22Sep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, Longeron/StringerSDR 96ZZZM423Skin · crackedDURING C-CHECK, FOUND FUSELAGE SKIN CRACKED STATION 312 STRINGER 23L. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF STRINGER 23L AT FS 312 AS PER SRM 53-10-3. FABRICATED DOUBLER AS PER SRM 53-10-3. FABRICATED DOUBLER AS PER SRM 53-30-3 2024-T-3 15 INCH BY 1Sep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM422Skin · dentDURING C-CHECK, FOUND LARGE DENT ON AFT CARGO DOOR SKIN BS 1090 STRINGER 22R. STRAIGHTEND OUT DENT PER SRM 51-40-1. CUT OUT DAMAGED AREA 3 INCH BY 4 INCH PER SRM 52-00-3 PAGE 6. FABRICATED DOUBLER 2024 T-3 .063 11 INCH BY 9 INCH PER SRM 52-00-3. INSTALLED Sep 6, 1995 · N702DH · Boeing 72730C · Cargo/Baggage DoorsSDR 96ZZZM421Skin · crackDURING C-CHECK, FOUND AFT CARGO DOOR SKIN CRACKED BS 1070 STRINGER 22R. REMOVED AFT CARGO DOOR. CUT OUT CRACKED AREA AS PER SRM 52-00-3 FIG 3 5.25 INCH BY 4 INCH. FABRICATED EXTERNAL DOUBLER 2024 T-3 .063 10.25 INCH BY 11.75 INCH PO 766422. INSTALLED DOUBLSep 6, 1995 · N702DH · Boeing 72730C · Cargo/Baggage DoorsSDR 96ZZZM420Blkhd Beam · crackedDURING C-CHECK, FOUND CABIN FS 1183 LBL 27 VERTICAL BEAM HAS APPROXIMATELY 10 INCH CRACK STARTING APPROXIMATELY 48 INCHES ABOVE FLOOR LEVEL. STOPPED DRILL .25 DIAMETER HOLES STATION 1183 LBL 27 IAW REF SRM 51-10-1 AND S/B 727-53-0182. NDT CHECKED STOP DRILLESep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, BulkheadSDR 96ZZZM419Skin · damagedDURING C-CHECK, FOUND FUSELAGE STATION 178 SKIN DOUBLER BETWEEN WINDSHIELD CENTER POST RADOME DAMAGED AND PULLED LOOSE AT FWD END. REMOVED DAMAGE AREA ON FUS STATION 178 SKIN DOUBLER BETWEEN WINDSHIELD CENTER POST AND RADOME. FABRICATED FILLER 1.5 INCH BY 10Sep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM418Skin · puncturedDURING C-CHECK, FOUND RIGHT ELEVATOR BOTTOM SKIN HAS 1.5 INCH BY .5 INCH HOLE AFT OF NR 4 BALANCE BAY. REMOVED SMALL ACCESS PANEL IAW SRM 51-30-2. ROUNDED OUT HOLE IAW SRM 51-10-1. MADE DOUBLER 2024 T-3 0.032 3.5 INCH BY 2.5 INCH LOT 750761 PO 9319067 PER SSep 6, 1995 · N702DH · Boeing 72730C · Elevator, Plate/SkinSDR 96ZZZM417Blkhd Beam · crackedDURING C-CHECK, FOUND CABIN STATION 1183 BULKHEAD VERTICAL BEAM HAS 4 INCH LONG CRACK COMING FROM FLOOR AT LBL 37. DRILLED .25 IN DIAMETER STOP HOLE AT CRACK END PER SRM 51-10-1 REF S/B 727-53A-0173. INSTALLED REPAIR PER SB 727-53-0173 AND BOEING DRAWING 65CSep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, BulkheadSDR 96ZZZM416Blkhd Beam · crackDURING C-CHECK, FOUND CABIN FS 1183 RBL 37 BULKHEAD VERTICAL BEAM HAS CRACK INDICATION AFT INBOARD FLANGE IN RADIUS 29 INCHES ABOVE FLOOR LEVEL. STOP DRILLED CRACK PER SB 727-53-0192. HFEC INSPECTED STOP DRILL HOLES AND NO FURTHER CRACK PROGRESSION NOTED IAWSep 6, 1995 · N702DH · Boeing 72730C · Fuselage Main, BulkheadSDR 96ZZZM415Floor Support · corrodedDURING C-CHECK, FOUND STATION 760 RBL 65 FRAME AND SUPPORT ANGLE IS CORRODED LOCATED JUST BELOW FLOOR LEVEL. REMOVED AND REPLACED SUPPORT ANGLE STATION 760 RBL 65 7075 T-6 .100 1 INCH BY 1 INCH BY 3.5 INCH AS PER SRM 51-10-1.Sep 6, 1995 · N702DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM414Seat Track · corrodedDURING C-CHECK, FOUND SEAT TRACK CORRODED RBL 62 AT STATION 890 AND STATION 920. REMOVED SECTION OF SEAT TRACK FROM STATION 870 TO STATION 970 RBL 62. INSTALLED NEW TRACK MADE OF BACK 1520 1430 - TMS 60 5030 FROM STATION 870-970.Sep 6, 1995 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZM413'S' Duct · corrosionDURING C-CHECK, FOUND NR 2 ENGINE 'S' DUCT STATION 1332 TO 1342 RIB 35 AT 6 O'CLOCK (BOTTOM) SKIN BULGED AND CRACKED. REMOVED CORROSION AS PER SRM 51-10-6 AND CUT DAMAGED SECTIONS 4 INCHES BY 5 INCHES AND 1 INCH BY 1 INCH TREATED AND PAINTED PER SRM 51-10-2, Sep 6, 1995 · N702DH · Boeing 72730C · Nacelle/Pylon Structure
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