N625PL

Service difficulty reports not matched to an aircraft · 69

They name N625PL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N625PL' AND registry_match IS NULL
  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 CKSA98384Web · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION FUSELAGE LWR AREA, BS 1200, RBL 58, WEB CORRODED AT O/B FACE LWR AREA. REMOVED CORROSION IAW B747 SRM 51-10-01. FABRICATED REPAIR IAW B747 SRM 51-40-02. INSTALLED REPAIR IAW BOEING 747 SRM 51-40-02. COJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA98383Floorbeam · crackedDURING ROUTINE CPCP INSPECTION, FOUND FS 440 RBL 50 UPPER DECK FLOORBEAM WEB CRACKED. REMOVED DAMAGED WEB IAW B747 SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW SRM 53-10-07 FIG 11. INSTALLED REPAIR IAW SRM 53-10-07 FIG 11. CORROSION TASK CARD NUMBER C53-21Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA98382Intercostal · crackedDURING ROUTINE CPCP INSPECTION, FOUND FS 440 TO FS 460 RBL 50 INTERCOSTAL WEB CRACKED. REMOVED CRACKED WEB IAW B747 SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW B747 SRM 53-10-07 FIG 11. INSTALLED REPAIR IAW B747 SRM 53-10-07 FIG 11. CORROSION TASK CARD NUJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA98381Angle · crackedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS440 RBL50 UPPER DECK FLOORBEAM ATTACH ANGLE CRACKED ON AFT INBD SIDE. REMOVED AND REPLACED ATTACH ANGLE IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-03. NON-ROUTINE TASK CAJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA98380Frame · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND BS 2020 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED AND A FLOOR SUPPORT. PERFORMED HFEC PER NDT MANUAL 51-00-00 PART 6. NO CRACKS NOTED. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05880. INSTALLED REPAIR IAW AIA EDR B4-0Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, FrameSDR CKSA98379Frame · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND BS 2000 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED UNDER FLOOR SUPPORT. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05879. INSTALLED REPAIR IAW AIA EDR NBR B4-05879. NON-ROUTINE TASK CARD NUMBER 26149.Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, FrameSDR CKSA98378Frame · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND BS 1980 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED UNDER FLOOR SUPPORT. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05878. INSTALLED REPAIR IAW AIA EDR B4-05878. NON-ROUTINE TASK CARD NUMBER 26148.Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, FrameSDR CKSA98377Longeron · corrodedDURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON UPPER SURFACE OF LEFT OVERWING LONGERON APPROX STA 1320. REMOVED CORROSION FROM ACCESSABLE AREA IAW SRM 51-10-01. CORROSION RUNNING UNDER LONGERON SPLICE RAISED EDR AS PER AIA ENGINEERING. REPAIRED LT OVERWJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Longeron/StringerSDR CKSA98376Keel Beam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION UPPER WEB OF KEEL BEAM BOX CORRODED AND CRACKED APPROX STA 1265 AT PREVIOUS REPAIR. REMOVED FASTENERS IAW B747 SRM 51-30-2. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, KeelSDR CKSA98375Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND FS2240 RBL75 FLOORBEAM T CHORD HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 51-40-4 FIG 12 AND AIA EDR B4-05887. INSTAJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA98374Spar · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LOWER FWD SPAR LWS1356 EXFOLIATED. REMOVED NR 2 PANEL RT SIDE. HFEC INSPECTED FASTENERS HOLES IN THE HORIZ FLANGE OF THE SPAR CHORD PER NDT MANUAL 51-00-00 PART 6. NO DEFECTS NOTED. PENETRANT INSPECTED CHORD PER STAJun 30, 1998 · N625PL · Boeing 747132 · Wing SparSDR CKSA98373Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS440 RBL50 UPPER DECK FLOORBEAM HAS CORROSION ON FWD SIDE. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. MANF REPAIR PARTS IAW EDR B4-05871. INSTALLED REPJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA98372Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, STA1940-1960 LBL11.33 LONGITUDINAL FLOORBEAM UPPER CHORD CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 53-10-05 Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA98371Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS1100 LBL70 SEAT TRACK UNDERSIDE HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR IAW B747 SRM 53-10-5 FIG 34. INSTALLED SEAT TRACJun 30, 1998 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98370Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, STA 340 FWD SIDE LBL33 SEAT TRACK FLANGE HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 53-10-05 FIG 1A. INSTALLED SEAT Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98369Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION AROUND 2 CLIP NUTS ON RBL 49 SEAT TRACK FWD OF BS 240. REMOVED CORROSION IAW 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED SEAT TRACK SECTION IAW B747 SRM 51-30-02. REJun 30, 1998 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98368Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION AROUND CLIP NUT ON UPPER CHORD OF BS680 FLOORBEAM LBL3. CUTOUT DAMAGE AREA IAW SRM 51-40-04 FIG 1. MADE REPAIR ANGLES AND DRILLED IAW SRM 51-40-04 FIG 1. INSTALLED REPAIR IAW B747 SRM 51-40-4Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA98367Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION STA760 FWD LBL44 FLOORBEAM HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUTOUT CORROSION AND FABRICATED REPAIR IAW B747 SRM 51-40-4 FIG 1. INSTALLED REPAIR IAW B747 SRM 51-40Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA98366Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STA760 FWD LBL72 FLOORBEAM HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUTOUT CORRODED SECTION OF UPPER CHORD AND FABRICATED REPAIR IAW SRM 51-40-4 FIG 1. ALSO AIA EDR NR BJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA98365Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STA 760 AFT, LBL 79 FLOORBEAM ANGLE HAS CORROSION. REMOVED FITTING IAW B747 SRM 51-30-2. REPLACED FITTING IAW 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTINE TASK CARD NUMBER 2Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA98364Floor · corrodedDURING ROUTINE CPCP INSPECTION, FOUND FLOOR HAS CORROSION BETWEEN STA 860 AND STA 880 RBL 98 BOTTOM SIDE. REMOVED FLOOR PANEL CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-20-00 FIG 2. MADE NEW FLOOR PANEL IAW B747 SRM 53-20-01. INSTALLED FLOOR PANEL Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Floor PanelSDR CKSA98363Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND 1 AREA OF CORROSION ON BOTTOM OF RBL11.33 SEAT TRACK FWD OF BS 520. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED SEAT TRACK IAW B747 SRM 51-30-02. INSTALLED NEW SEATJun 30, 1998 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98362Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION 2 AREA OF CORROSION ON BS480 FLOOR BEAM FWD, UPPER, SIDE AT RBL-76. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 51-Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA98361Angle · crackedDURING ROUTINE CPCP INSPECTION, FOUND FS1000 LBL 30 FRONT SPAR FLOOR SUPPORT ATTACH ANGLE CRACKED. REMOVED FLOOR SUPPORT. REWORKED FITTINGS IAW EDR B4-05869 DTD 6-2-98. INSTALLED FITTINGS IAW B747 SRM 51-30-02 AND EDR B4-05885 DTD 6-9-98. CORROSION TASK CAJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA98360Angle · crackedDURING ROUTINE CPCP INSPECTION, FOUND FS1080 LBL90 OUTBD SIDE WEB ATTACH ANGLE CRACKED. FAB NEW ATTACH ANGLE 7075-T6. INSTALLED ATTACH ANGLE IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05. NON-ROUTINE TASK CARD NUMBER 25171.Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA98359Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION BS980, RBL50, PANEL SUPPORT FRAME CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REPAIR FRAME FLANGE IAW B747 SRM 53-50-04. INSTALLED REPAIR IAW B7Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, FrameSDR CKSA98358Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND BS920, FROM BOTTOM CENTERLINE TO BOTH RT AND LEFT BL50, PANEL SUPPORT FRAME CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REPAIR FRAME IAW B747 SRM 53-50-04 AND AIA Jun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, FrameSDR CKSA98357Angle · corrodedDURING ROUTINE CPCP INSPECTION, FOUND AT BS1060, FROM BOTTOM CENTERLINE TO LBL50, PANEL SUPPORT FRAME WITH CORROSION AROUND ANCHOR NUTS AND FASTENERS. REMOVED DAMAGED T-CHORD, FAB NEW PER SRM 51-10-01. FAB REPAIR ANGLES PER SRM 51-40-02. INSTALLED REPAIR ANJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA98356Skin · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: FS1200 RBL95 CNTR WING SKIN HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 57-10-01. INSTALLED REPAIR IAW AIA EA B4-57-051. C/W OPEN HOLE HFEC AND SURFJun 30, 1998 · N625PL · Boeing 747132 · Wing, Plate/SkinSDR CKSA98355Skin · crackedDURING ROUTINE CPCP INSPECTION FOUND: C-2 DOOR OUTER SKIN IS DENTED AND HAS 2 EA 1 CRACKS AT BOTTOM EDGE BETWEEN BS 1840 AND BS 1860. DAMAGED FOUND TO BE OUT OF LIMITS IAW B747 SRM 52-00-2. REPAIR DOOR SKIN IAW B747 SRM 52-00-03 FIG 3. INSTALLED REPAIR IAW Jun 30, 1998 · N625PL · Boeing 747132 · Cargo/Baggage DoorsSDR CKSA98354Skin · gougedDURING ROUTINE C CHECK INSPECTION FOUND: SEVERAL GOUGES IN FUSELAGE SKIN AT AFT LOWER CORNER OF C-2 DOOR CUT-OUT BS1920. REMOVED FASTENERS AND BLENDED AREA IAW B747 SRM 51-30-2. C/W OPEN HOLE HFEC OF 3 FASTENER HOLE AND SURFACE PERIFERY OF BLEND-OUT AREA IAJun 30, 1998 · N625PL · Boeing 747132 · Fuselage Main, Plate/SkinSDR CKSA97458Bleed Air Duct · leakingNUMBER 2 FIRE DETECTION FAULT LIGHT CAME ON IN FLIGHT BLEED VALVE WENT TO CLOSE POSITION AND A AND B INDICATORS SHOW 8.5 AND 7. TEMP WAS NORMAL ON ALL ENGINE PARAMETERS. SUSPECT A BLEED AIR LEAK AROUND B-LOOP. FOUND AIR LEAK AT FIRE LOOP 6 O'CLOCK POSITION Aug 22, 1997 · N625PL · Boeing 747132 · Pneumatic Distribution SystemSDR CKSA97437Door Light · illuminatedDURING DESCENT FL20.0, DOOR OPEN LIGHT ILLUMINATED ALONG WITH PRIMARY NOSE DOOR OPEN LIGHT. PRIMARY NOSE GEAR DOOR IND. TRANSFERRED TO DMI NR 612 IAW MEL 32-12, PLACARDS INSTALLED. DEFECT HAS NOT REOCCURED ON SUBSEQUENT FLIGHTS. CANNOT DUPLICATE ON GROUND,Jul 30, 1997 · N625PL · Boeing 747132 · Landing Gear Position and WarningSDR CKSA96195Drive Unit · wornUHHH-FLT NR 80738: WHEN RETRACTING FLAPS, NR 1 LEADING EDGE FLAP, LEFT SIDE WOULD NOT RETRACT. NR 1 REMAINED INTRANSIT DURING EXTENSION ALSO. REPLACED NR 1 LEFT LEADING EDGE FLAP DRIVE UNIT. OPS CHECKS NORMAL ON GROUND PER MM 27-81-03.Nov 7, 1996 · N625PL · Boeing 747132 · Leading Edge Slat ActuatorSDR CKSA96187Seat Track · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: SEAT TRACK REPAIR BETWEEN STA 1210 AND 1265 LBL 75 CORRODED. REMOVED AND REPLACED IAW SRM 51-30-02 AND AIA/E/2359. C-CHECK CARD NR 7GK0232 TASK CARD NR 87072.Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA96186Angle · corrosionKOSC - DURING C-2 CHECK INSPECTION FOUND: FLOOR BEAM ANGLE AT FS 330 UPPER CABIN HAS CORROSION FROM LBL 6 TO FUSELAGE SKIN. REPAIRED IAW ENGINEERING DOC B405022. C-CHECK TASK CARD NR 7GK0224,TASK CARD NR 76102.Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA96185Stringer · crackedKOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 743R CRACK IN STRINGER 44 AT RIVET. REPAIRED IAW SRM 53-10-3. CORROSION TASK CARD NR C53-110-01, TASK CARD NR 75771.Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage Main, Longeron/StringerSDR CKSA96184Angle · crackedKOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 560 LEFT INNER CORD LOWER SUPPORT ANGLE CRACKED IN RADIUS ABOVE STR 39. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE PER SRM 51-10-21. INSTALLED NEW ANGLE PER SRM'S 51-10-02, 51-21-02 AND MM AND SRM 51-3Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA96183Shear Tie · crackedKOSC - DURING C-2 CHECK INSPECTION FOUND: FORWARD NR 3 PYLON SUPPORT STRUT SHEAR TIE CRACKED AT WS 670 IN NR 3 MAIN FUEL TANK 11 INCHES AFT OF FRONT SPAR WEB. REPAIRED IAW SB 747-57-2273 FIGURES 10 AND 11. AD NR 94-15-18 SID TASK CARD NR W-22C. TASK CARD NROct 18, 1996 · N625PL · Boeing 747132 · Nacelle/Pylon StructureSDR CKSA96182Angle · crackedKOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 680L ABOVE STRINGER 38 INNER CORD REINFORCEMENT ANGLE CRACKED. REMOVED CRACKED ANGLE. VERIFIED AND FABRICATE NEW ANGLE IAW SRM'S 53-10-21, 51-30-02, 51-10-02, AND MM 51-21-02. AD NR 93-08-12 CORROSION TAOct 18, 1996 · N625PL · Boeing 747132 · Fuselage Miscellaneous StructureSDR CKSA96181Frame · corrosionKOSC - DURING C-2 CHECK INSPECTION FOUND: AFT PIT CARGO DOOR AFT FRAME BEHIND LOCK SWITCH SKIN HAS CORROSION. REPAIRED IAW SKETCH AIA/EI2357. CORROSION TASK CARD NR C53-110-01. TASK CARD NR 76020.Oct 18, 1996 · N625PL · Boeing 747132 · Cargo/Baggage DoorsSDR CKSA96180Skin · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: STA 2055 BETWEEN 37R AND 38R SKIN HAS CORROSION. CUT OUT DAMAGED AREA, FABRICATED REPAIR IAW SRM 53-30-03 FIGURE 1. CORROSION TASK CARD NR C53-110-01. TASK CARD NR 86602.Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage Main, Plate/SkinSDR CKSA96179Floor Beam · corroded/splitKOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1820 LBL 67 FLOOR BEAM UPPER CORD SPLIT AND CORRODED. REPAIRED FLOOR BEAM STA 1820 LBL 67 IAW REPORT NR 96AIA-152 AND 8110-3 DATED 10/15/96. CORROSION TASK CARD NR C53-110-01 TASK CARD NR 87061.Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage Main, Floor BeamSDR CKSA96178Seat Track · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1230 RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON INBOARD SIDE. REMOVED DAMAGED SEAT TRACK STA 1230 RIGHT OUTBOARD. REPAIRED IAW EER B4-05046 DATED 10-15-96 AND AIA SKETCH NR AIA/E/2359 DATED 10/4/96 8110-3 AIA EOct 18, 1996 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA96177Spar Cap · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: RIGHT WING LEADING EDGE LOWER SPAR CAP CORRODED AT WS 1300. REMOVED CORRODED SPAR CAP AND REPAIRED IAW B747 SRM 57-30-03. CORROSION CARD NR C57-510-01. TASK CARD NR 85485.Oct 18, 1996 · N625PL · Boeing 747132 · Wing SparSDR CKSA96176Seat Track · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: CABIN: STATION 1242 MAIN CABIN RBL 82 SEAT TRACK FLANGE CORRODED. REMOVED CORRODED SEAT TRACK AND REPAIRED IAW AIA/EA B405042 AND SKETCH AIA/E2359. INSTALLED FASTENERS IAW B747 SRM 51-30-02 ALODINED AND PRIMED IAW Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA96175Skin · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: STATION 2220 STR 35R SKIN HAS CORROSION AT SHEAR TIE AND TEAR STRAP. REMOVED CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-30-01. REPAIRED DAMAGE IAW SRM 53-30-03 FIGURE 1. CORROSION TASK CARD NR C53-110-01 TASKOct 18, 1996 · N625PL · Boeing 747132 · Fuselage Main, Plate/SkinSDR CKSA96174Frame · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: FS 1700 RBL 65 FLOOR FRAME CORRODED. REPAIRED PER AMERICAN INTERNATIONAL AIRWAYS ENGINEERING SKETCH AIA/E/2372. PART FABRICATION DOCUMENTED ON 4 EA M-59 FORMS. CORROSION TASK CARD NR C53-210-01 PART 4 OF 8. TASK COct 18, 1996 · N625PL · Boeing 747132 · Fuselage Main, FrameSDR CKSA96173Seat Track · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1905 MAIN CABIN RBL 34 SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK STA 1905 PER SRM'S 51-10-01 AND 51-30-2, 51-10-2. C-CHECK CARD NR 7GK0232 TASK CARD NR 86824.Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA96172Seat Track · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: SEAT TRACK AT STA 1860 RBL 34 CORRODED. REMOVED AND REPLACED SEAT TRACK STA 1860 AS REQUIRED PER SRM'S 51-10-01 AND 51-30-2 AND 51-10-2. AD NR 94-15-18 SID NR W-44A TASK CARD NR 76194.Oct 18, 1996 · N625PL · Boeing 747132 · Fuselage, Seat/Cargo Attach Fittings
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