N903TW, cancelled May 10, 2007

Service difficulty reports · 56

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 = 'N903TW' AND deregistration_id = 'N903TW-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 ZW0A0211301Coalescer Bag · contaminatedIRRITATING FUMES WERE OBSERVED IN THE CABIN. REPLACED BOTH WATER SEPARATOR ASSEMBLIES AND PERFORMED PACK BURN OUT. SUSPECT A PREVIOUS APU FUEL LEAK WHICH WAS CORRECTED BY REPLACEMENT OF A CRACKED BURNER CAN. CHECK-C 10-19-2002 MCI. --CLOSED--Nov 13, 2002 · N903TW · Doug DC982 · Humidity Control SystemSDR TWAA0103704Seat Track · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CHAIR TRACK AT STA 1098 TO 1139, SHORT TRACK UNDER FORWARD AFT GALLEY. INSTALLED NEW SECTION OF FLOOR TRACK AT STA 1098 TO 1139 PER SPM 6-70-01, PAGE 3 AND DOUGLAS INSTALLATION DRAWING 5930566.Feb 24, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0103702Seat Track · corrodedDURING CHECK-C MAINT FOUND CORROSION ON NUMBER 2 CABIN TRACK AT LBL 44 INCHES, STA 1155 TO 1308. REMOVED AND REPLACED TRACK STA 1145 TO 1309. INSTALLED WITH HARDWARE PER SRM 51-30-5. INSTALLED TRACK WITH NAS 6203 BOLTS, MS 2104L3 NUTS, MS 250 WASHERS, AND TFeb 24, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0103703Web · misdrilledDURING CHECK-C MAINT FOUND IN FWD CABIN MEMBRANE MISDRILLED AT FASTENER HOLE LBL 56 INCHES OTBD SIDE, STA 200 TO 215. REMOVED MISDRILLED MEMBRANE. INSTALLED REPAIR AND BRACKET THAT WAS REMOVED FOR REPAIR PER SRM 51-70-4. PAINTED AND TREATED PER SRM 51-10-3.Feb 23, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103701Floorbeam · corrodedDURING CHECK-C MAINT FOUND FLOORBEAM/CEILING SUPPORT CORRODED ALONG STA 1308, 20 INCHES INBD OF LONGERON 19L. REPAIRED FLOORBEAM AT STA 1308 PER SRM 53-05 FIG 79 SHEET 8-9-10, ARA 17629 PAGE 1-2-3, SRM 51-60-0, SRM 51-20-0, AND SRM 51-10-3.Feb 23, 2001 · N903TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0103502Web · damagedDURING CHECK-C MAINT FOUND RIVET HOLES ALONG INSIDE EDGE OF MEMBRANE DAMAGED FROM STA 1238 TO 1250, LT SIDE. INSTALLED DOUBLER PER SRM 53-01, PAGE 9 FIG 2 AND SHEET 3. PRIMED AND PAINTED DOUBLER PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-10-05.Feb 22, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103317Intercostal · corrodedDURING CHECK-C MAINT FOUND CORROSION ON TOP OF INTERCOSTAL BETWEEN STA 1322 AND 1338, BELOW LONGERON 21L, AND ON 2 ADJACENT INTERCOSTALS BETWEEN STA 1322 AND 1338 AND LONGERON 21L AND 22L. REMOVED INTERCOSTALS FOR REPLACEMENT. REMOVED CORROSION ON SKIN PER SFeb 18, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103316Cargo Track · corrodedDURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON UNDERSIDE OF RT TIE DOWN TRACK, BETWEEN STA 1309 AND 1320. REPLACED TRACK PER SPM 6-70-01 PAGE 2 AND 3 AND DAC DRAWING 5936663. FABRICATED FROM STOCK AND INSTALLED PER 5936663-505 ASSEMBLY AND SRM 51Feb 18, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0103315Cargo Track · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON RT TIE DOWN TRACK FROM STA 1212 THRU 1320. REPLACED TRACK PER SPM 6-70-01, PAGE 2 AND 3 AND DRAWING 5936663. FABRICATED FROM STOCK AND INSTALLED PER 5936663-505 FOR ASSEMBLY AND SRM 51-30-1 PARAGFeb 17, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0103314Floor Support · corrodedDURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 200, LBL 8 INCHES. INSTALLED NEW FLOOR SUPPORT PER DRAWING 9936534. INSTALLED FASTENERS PER SRM 51-30-1.Feb 16, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103313Cargo Track · corrodedDURING CHECK-C MAINT FOUND HEAVY CORROSION IN FWD CARGO COMPT ON RT TIE DOWN TRACK, STA 332 TO 370. REMOVED CORROSION PER SRM 51-10-3 PAGE 21 PARA 35. FABRICATED NEW TRACK PER SAMPLE AND SPM 6-70-01. PRIMED AND PAINTED PER SRM 51-10-3. INSTALLED WITH FASTEFeb 16, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0103312Intercostal · corrodedDURING CHECK-C MAINT FOUND 4 INTERCOSTALS UNDER THE MEMBRANE AT STA 160 TO 200, LBL 55 INCHES, WERE CORRODED. REMOVED LIGHT CORROSION FROM INTERCOSTAL AT STA 175.688 AND 193.688. REPLACED INTERCOSTALS AT STA 167.688 AND STA 185.688 PER DRAWING 9936534.Feb 16, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103311Web · corrodedDURING CHECK-C MAINT IN THE FWD CABIN, FOUND CORROSION ON FLOOR PAN AT STA 160 TO 169, LBL 9 INCHES. INSTALLED REPAIR PER SRM 51-70-4. INSTALLED FASTENERS PER SRM 51-30-2. TREATED PER SRM 51-10-3.Feb 16, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103310Cargo Track · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT FLOOR TIE DOWN TRACK HAD CORROSION INSIDE OF TRACK FROM STA 1008 TO 1155. REMOVED TRACK AND REPLACED WITH NEW AND INSTALLED PER SPM 6-70-01, SRM 51-30-1, 51-30-2, AND DRAWING 5936660.Feb 16, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0103309Support Bracket · corrodedDURING CHECK-C MAINT IN MID CARGO COMPT, FOUND CORROSION ON TRACK SUPPORT RT SIDE STA 598 TO 642. REMOVED TRACK SUPPORT AND FABRICATED NEW PER SRM 53-24-0, PAGE 19 AND 20. HEAT TREATED PER SRM 51-10-2A. ALODINE PER SRM 51-10-3. PRIMED AND TOP COATED PER SRFeb 16, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103307Floor Support · corrodedDURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION AT STA 180, LBL 13 INCHES TO 38 IN, ON FLOOR SUPPORT TOP AND UNDERSIDE. REPLACED FLOOR SUPPORT. REMOVED RIVETS AND INSTALLED RIVETS PER SRM 51-30-2. TREATED PER SRM 51-10-3.Feb 15, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103306Floor Support · corrodedDURING CHECK-C MAINT A CABIN FLOOR PANEL MOUNT HAD CORROSION ON AFT EDGE OF FLOOR PANEL MOUNT, STA 1174, FLOOR PANEL NUMBER 85. FABRICATED NEW FLOOR SUPPORT PER SPM 6-70-01. PRIMED AND PAINTED NEW SUPPORT PER SRM 51-10-03. INSTALLED NEW SUPPORT AND FASTENERFeb 14, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103103Floor Support · corrodedDURING CHECK-C MAINT, THE RT SIDE FWD CABIN DOOR AREA, FLOOR SUPPORT AT STA 172, 18 INCHES TO RT OF BL 0, WAS CORRODED. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER 51-30-5.Feb 14, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103007Frame · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1309, LONGERON 28R, THE FORMER REPAIR WAS CORRODED. FABRICATED NEW SPLICE PER SPM 6-70-01. INSTALLED REPAIR AND FASTENERS PER SRM 51-10-05.Feb 13, 2001 · N903TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0103006Floor Support · corrodedDURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 160 TO 200, RBL 52 INCHES. REPLACED FLOOR SUPPORT AT STA 160 TO 200 PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-02 AND 51-30-5.Feb 13, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103005Floor Support · corrodedDURING CHECK-C MAINT THE RT SIDE FWD DOOR AREA, FWD GALLEY DRAIN PAN FLOOR SUPPORT HAD CORROSION. REPLACED OUTBOARD FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-02.Feb 13, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103004Pan · corrodedDURING CHECK-C MAINT AT THE RT SIDE FWD CABIN DOOR AREA, THE MEMBRANE AROUND AND UNDER THE FWD GALLEY DRAIN PAN HAD CORROSION. REMOVED CORROSION PER SPM 6-80-01. INSTALLED DOUBLER PER SRM 53-01 FIG 2. INSTALLED FASTENERS PER SRM 51-30-02.Feb 13, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0103308Seat Track · corrodedDURING CHECK-C MAINT IN CABIN FWD END OF TRACK AT RBL 24 INCHES HAD CORROSION GROUND BEYOND LIMITS AT STA 200. REMOVED CORROSION PER SPM 6-80-01. REPAIRED TRACK PER SRM 53-05, PAGE 10G.Feb 12, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0102813Floorbeam · corrodedDURING CHECK-C MAINT IN THE RT SIDE NUMBER 1 CABIN DOOR AREA, FOUND FLOOR SUPPORT AT STA 200 WITH CORROSION, RBL 44 TO 54. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-5.Feb 12, 2001 · N903TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0102812Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 148 TO 200, RBL 5 INCHES. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-1, STA 148 TO 200.Feb 12, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0102811Longeron · corrodedDURING CHECK-C MAINT FOUND CORROSION INSIDE LONGERON 24L, BETWEEN STA 1193 AND 1212. REPLACED LONGERON SPLICE WITH NEW SPLICE. SEALED PART FOR INSTALLING PER SRM 51-20-0. REPLACED RIVETS IN FLANGE WITH HI-LOKS PER SRM 51-60-0.Feb 12, 2001 · N903TW · Doug DC982 · Fuselage Main, Longeron/StringerSDR TWAA0102810Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, RBL 44 INCHES. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-02 AND 51-30-5.Feb 11, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0102809Floorbeam · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 200 FROM BLR AND ON TO APPROX 37 INCHES. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-5.Feb 11, 2001 · N903TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0102808Galley Track · corrodedDURING CHECK-C MAINT FOUND CORROSION AT FWD GALLEY HOLD DOWN SUPPORT AT STA 160, BLR 38 IN. REPLACED GALLEY TIE DOWN PER SRM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-5.Feb 11, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0102807Seat Track · corrodedDURING CHECK-C MAINT FOUND CORROSION IN THE NUMBER 1 CABIN CHAIR TRACK, STA 1118. REPLACED NUMBER 1 CHAIR TRACK FROM STA 1030 TO 1136 PER SPM 6-70-01. REPLACED FASTENERS PER SRM 51-30-0.Feb 8, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0102707Cargo Track · corrodedDURING CHECK-C IN THE FWD CARGO COMPT, THE LT TIE DOWN TRACK AT STA 541 WAS CORRODED. SPLICED IN NEW CARGO TRACK PER SRM 53-05, FIG 4G, PAGE 10R. PAINTED PER SRM 51-10-03.Feb 7, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0102415Flange · damagedDURING CHECK-C MAINT THE FORWARD CARGO DOOR FLANGE AREA UNDER THE CAM LOCK HAD A FIELD REPAIR, ON AFT SIDE. REMOVED OLD REPAIR AND INSTALLED REPAIR PER SRM 52-05, PAGE 110.Feb 6, 2001 · N903TW · Doug DC982 · Cargo/Baggage DoorsSDR TWAA0102412Stop · crackedDURING CHECK-C MAINT FWD CARGO DOOR, TOP AFT EXTERNAL STOP AND LOWER FWD EXTERNAL STOP, HAD CRACKED ATTACH BRACKETS. INSTALLED NEW BRACKETS AND FASTENERS PER SRM 51-30-0.Feb 6, 2001 · N903TW · Doug DC982 · Cargo/Baggage DoorsSDR TWAA0102416Flange · crackedDURING CHECK-C MAINT ON THE AFT CARGO DOOR, THE FLANGE AREA UNDER THE AFT CAMLOCK WAS CRACKED. STOP DRILLED AND INSTALLED REPAIR DOUBLER PER SRM 52-05, FIG 26A. INSTALLED FASTENERS PER SRM 52-05, FIG 26A.Feb 5, 2001 · N903TW · Doug DC982 · Cargo/Baggage DoorsSDR TWAA0102414Seat Track · corrodedDURING CHECK-C MAINT FOUND HEAVY CORROSION ON NUMBER 3 CHAIR TRACK, LBL 22 INCHES, STA 1088 TO 1308. REMOVED AND REPLACED CHAIR TRACK WITH STOCK PART AT STA 1088 TO 1308. SPLICED NEW TRACK AT STA 1088 PER SRM 53-05, FIG 4F.Feb 4, 2001 · N903TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0102413Bracket · corrodedDURING CHECK-C MAINT ON RT WING THE AFT RT END OF KEEL BEAM BOX HAD CORROSION ON DUCT BRACKET. REMOVED AND REPLACED ANGLE PER SPM 6-70-01 USING DRAWING 5936395 CALLING FOR USE OF PART NUMBER 5936395-7 ANGLE. INSTALLED ANGLE USING HI-LOKS. INSTALLED HI-LOKS Feb 4, 2001 · N903TW · Doug DC982 · Wing Miscellaneous StructureSDR TWAA0102411Floor Support · corrodedDURING CHECK-C MAINT FOUND 2 CABIN FLOOR SUPPORTS BETWEEN STA 1182 AND 1250, AND BETWEEN CHAIR TRACKS 2 AND 3, WERE CORRODED. INSTALLED NEW FLOOR SUPPORTS PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-05.Feb 2, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0102305Bracket · crackedDURING CHECK-C MAINT IN THE FWD CARGO COMPT BILGE, STA 237, BETWEEN LONGERON 29R AND 28R, ANGLE BRACKET WAS CRACKED IN RADIUS IN INTERCOSTAL AFT END UNDER TIE DOWN TRACK. INSTALLED NEW BRACKET PER DRAWING 9915554.Jan 30, 2001 · N903TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0102304Frame · damagedDURING CHECK-C MAINT IN THE AFT ACCY COMPT, FORMER RING WAS DAMAGED AT STA 1418, LONGERON 13R. REPAIRED FORMER PER SRM 53-03, FIG 4. INSTALLED FASTENERS PER SRM 51-10-03.Jan 30, 2001 · N903TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0102303Shear Tie · crackedDURING CHECK-C MAINT AT THE AFT ACCY COMPT, STA 1418, BETWEEN LONGERON 13R AND 14R, THE FORMER FOOT WAS CRACKED. REPLACED FORMER FOOT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-10.Jan 30, 2001 · N903TW · Doug DC982 · Fuselage Main, StructureSDR TWAA0102302Skin · misrepairedDURING CHECK-C MAINT, A RT WING L/E BLIND RIVET REPAIR WAS FOUND INSTALLED ON L/E LOWER SURFACE AT INBOARD END OF FUEL SERVICE PANEL, STA X05250. REMOVED OLD REPAIR AND MADE NEW REPAIR DOUBLER AND INSTALLED WITH HI-LOKS PER SRM 57-06B, PAGE 9 FIG 3.Jan 30, 2001 · N903TW · Doug DC982 · Wing, Plate/SkinSDR TWAA0102814Web · corrodedDURING CHECK-C MAINT FOUND THE RT SIDE NUMBER 1 CABIN DOOR AREA, WITH CORROSION ON MEMBRANE AT STA 180 TO 200, BL 0 TO RBL 35 INCHES. SEVERAL PLACES. CORROSION REMOVED PER SPM 6-80-01. TREATED AREA PER SRM 51-10-3. INSTALLED DOUBLER PER SRM 53-01 FIG 2. IJan 12, 2001 · N903TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0008411Slide · deployedDURING OVERNIGHT LAYOVER, THE TAIL SLIDE WAS DEPLOYED. SLIDE NOT DISARMED BY FLIGHT ATTENDANT. REPLACED SLIDE ASSEMBLY. AC02 5-2-00 JFK.May 29, 2000 · N903TW · Doug DC982 · Escape SlideSDR TWAA0003001Connector · disconnectedTHE LEFT AND RIGHT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. RECONNECTED CONNECTOR R5-1314 IN THE FWD CARGO COMPT SIDEWALL. CHECK-C 10-25-99 JFK.Feb 22, 2000 · N903TW · Doug DC982 · Emergency LightingSDR TWAA9916101Sensor · out of adjustAFTER TAKEOFF, NOSE GEAR RED LIGHT WAS ON. CYCLED THE GEAR AND THE LIGHT WENT OUT BRIEFLY THEN CAME BACK ON. WENT OUT AFTER 2 HRS OF FLIGHT AND STAYED OUT. ADJUSTED NOSE GEAR LOCK POSITION SENSOR AND ACCOMPLISHED GEAR SWING. AC-00, NO STATION NO DATE.Nov 23, 1999 · N903TW · Doug DC982 · Landing Gear Position and WarningSDR TWAA9714601Potentiometer · wornJFK - FLT 30 - DURING CRUISE, FIRST OFFICER'S MAP LIGHT SWITCH SHORTED OUT. SLIGHT ODOR AND SMOKE DETECTED. POTENTIOMETER MOUNTING WAS RESECURED. MFG P/N 62412. CHECK-C 01D 11-17-97 LAX. (X)Dec 12, 1997 · N903TW · Doug DC982 · Flight Compartment LightingSDR TWAA9809603Bulkhead · crackedMCI - DUIRNG MAINTENANCE CHECK, FOUND LT BULKHEAD OTBD OF LT TRUNNION, 3 INCHES FORWARD, HAD 3 INCH CRACK. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 53-05, PAGE 85. TOTAL CYCLES: 45,640 HOURS. TOTAL CYCLES: 23,735. (X)Dec 9, 1997 · N903TW · Doug DC982 · Fuselage Main, BulkheadSDR TWAA9809602Skin · gougedMCI - DURING MAINTENANCE CHECK, FOUND FUSELAGE DAMAGE AT STA 204, L22R. GROOVE IN SKIN 2.5 INCHES LONG BY 1.8 INCHES BY .200 INCH DEEP. INSTALLED REPAIR PER SRM 53-04, PAGE 39. TOTAL TIME: 45,640 HOURS. TOTAL CYCLES: 23.735. (X)Dec 9, 1997 · N903TW · Doug DC982 · Fuselage Main, Plate/SkinSDR TWAA9809513Skin · dentedMCI - DURING MAINTENANCE WORK, FOUND DENT IN FUSELAGE SKIN 1.5 INCH IN DIAMETER BY .140 INCH DEEP AT STA 194, L234. INSTALLED REPAIR PER SRM 53-04, PAGE 39. ACFT TC: 45,640 HOURS. ACFT TC: 23,735. (X)Dec 9, 1997 · N903TW · Doug DC982 · Fuselage Main, Plate/SkinSDR TWAA9805803Skin · dentedMCI - DURING MODIFICATION VISIT, FOUND FUSELAGE DAMAGE AT STATION 200 BETWEEN LONGERON 22R AND 23R. TWO DENTS WERE FOUND, AFT DENT 2.5 INCH DIAMETER BY .100 INCH DEEP. FORWARD DENT WAS 2 INCH DIAMETER BY .180 DEEP. INSTALLED REPAIR PER SRM 53-04 PAGE 39. (Dec 9, 1997 · N903TW · Doug DC982 · Fuselage Main, Plate/Skin
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