Boeing 737-2P6

Service difficulty reports · 200

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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 = '7372P6'
  ORDER BY difficulty_date DESC"

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SDR VJ9800454Floorbeam · corrodedCORROSION UNDER TWO NUT PLATES ON UNDERSIDE OF BS 277 FLOORBEAM UPPER CAP, AFT HORIZ FLANGE LBL 16 AND 23. REMOVED CORROSION OUT OF LIMITS LBL 17 IAW SRM 53-10-9. FABBED FLOORBEAM REPAIR, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 53-10-9 FIG 6, 51-10-2,Sep 4, 1998 · Boeing 7372P6 · Fuselage Main, Floor BeamSDR VJ9800451Strap · corrodedFWD CARGO FLOOR BOARD STRAP AT STA 430 HAS SURFACE CORROSION. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR STRAP, TREATED, PRIMED, AND INSTALLED REPAIR AND NUT PLATES IAW SRM 51-10-6, 51-30-2, AND 51-10-2.Sep 4, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800502Support · corrodedFLOOR SUPPORT AT FS 328 TO 344 RBL 12 CORRODED OUT OF LIMITS. REMOVED FLOOR SUPPORT AND FABRICATED PARTS IAW SRM 51-40-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 51-10-2, MM 51-21-21 AND SRM 51-30-2.Sep 3, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800501Support · corrodedFLOOR SUPPORT AT FS 328 TO 344 LB 12 IS CORRODED OUT OF LIMITS. REMOVED FLOOR SUPPORT AND FABRICATED REPAIR FROM BAC 1505-100604-15.5 IAW SRM 51-30-2 AND SRM 51-40-4. TREATED, PRIMED, AND INSTALLED IAW SRM 51-10-2, 51-20-11, 51-30-2.Sep 3, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800500Support · corrodedFLOOR SUPPORT AT FS 312 TO 328 LBL 12 IS CORRODED OUT OF LIMITS. REMOVED FLOOR SUPPORT AND FABRICATED REPAIR FROM BAC 1505-100604-15.625 IAW SRM 51-30-2 AND 51-40-4. INSTALLED REPAIR IAW B737 SRM 51-30-2.Sep 3, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800496Floor · corrodedCORROSION AROUND FLOOR PANEL FASTENER HOLES ON UNDERSIDE OF CUSP MEMBRANE AT R-2 THRESHOLD, BETWEEN BS 967 TO 986 FLOORBEAMS. CLEANED CORROSION MATERIAL LOSS BETWEEN STA 977.5 TO 982.5 OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR DOUBLER, DRILLED, DEBURRSep 3, 1998 · Boeing 7372P6 · Fuselage Floor PanelSDR VJ9800484Support · corrodedLT FWD LAV; AFT BULKHEAD SUPPORT HAS CORRODED FASTENERS AND IS CORRODED AT FWD EDGE STA 294.5, LBL 29. REMOVED CORROSION IAW SRM 51-10-6. MAT LOSS .019 OUT OF LIMITS IAW SRM 53-10-1. FABRICATED NEW FLOOR SUPPORT REPAIR FROM BAC 1510-335, IAW SRM 51-40-3. ASep 3, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800455Support · corrodedCORROSION ON LONGITUDINAL FLOOR SUPPORT IN FWD LAV DOOR WAY. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR, ALODINED, AND PRIMED AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, MM 51-21-31, AND SRM 51-30-2.Sep 3, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800485Panel · crackedLT AFT VANITY LOWER ACCESS COVER PLATE CORRODED. REMOVED CORROSION FROM THE ACCESS PANEL, OUT OF LIMITS IAW SRM 51-10-1 PG 5. FABRICATED 1 COVER PLATE FROM 6061 T6-.050 IAW SRM 51-10 FIG 7, UPON REMOVAL OF ACCESS PANEL FOUND .75 INCH CRACK IN MATING FLANGE. Sep 2, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800458Support · corrodedLONG FLOOR SUPPORT CORRODED BETWEEN BS 312 AND 328 FLOORBEAMS, RBL 10. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT REPAIR, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, MM 51-21-31 AND SRM 51-30-2.Sep 2, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800494Angle · corrodedCORROSION UNDER NUT PLATES ON UNDERSIDE OF R-1 DOOR THRESHOLD SCUFF PLATE ATTACH ANGLE, BS 297 TO 334. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR STRAP FORM 7075 T6 .100. ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-10-2, MM 51-Sep 1, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800486Doubler · corrodedE/E COMPARTMENT DOOR OPENING IS CORRODED AND HAS BROKEN RIVET AT AFT DOUBLER LT AFT CORNER, FWD OF STA 344 LBL 9.5. REMOVED CORROSION OUT OF LIMITS IAW SRM 51-10-2, 52-01 FIG 1. REMOVED CORRODED DOUBLER AND FABRICATED NEW DOUBLER IAW SRM 51-30-02. ALODINED,Sep 1, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800456Channel · corrodedLOWER END OF FWD DOOR JAM CORRODED BS 283, LBL 11. CUT CORROSION SECTION U CHANNEL, FORMED REPAIR ANGLE 1 EACH, TREATED, PRIMED, AND INSTALLED IAW SRM 51-10-2, 51-40-3.Sep 1, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800450Bracket · corrodedFWD CARGO STA 520 FLOOR SUPPORT L-BRACKET HAS SURFACE CORROSION FROM 27L-27R. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED REPAIR, TREATED, PRIMED, AND INSTALLED REPAIR ANGLE WET WITH SEALANT IAW B 737 51-10-2, MM 51-21-31, SRM 51Sep 1, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800493Bulkhead · corrodedDEEP GOUGE IN FWD SIDE OF BS 294.5 PRESS BULKHEAD AT TOP OF NLG UPLOCK/DOWNLOCK UPLOCK CYCLE, BETWEEN DOWNLOCK LINK ATTACHED FITTINGS. CUT OUT GAUGE AREA IAW RES 981424. FABRICATED 2 DOUBLERS, TREATED, PRIMED, AND INSTALLED IAW SRM 51-10-2, MM 51-21-51, AND Aug 31, 1998 · Boeing 7372P6 · Fuselage Main, BulkheadSDR VJ9800492Bracket · corrodedLOWER FWD I/B OF LT I/B LANDING LIGHT BRACKET 1 HAS CORROSION AT WS 75. REMOVED SUPPORT PLATE DUE TO CORROSION OUT OF LIMITS IAW SRM 51-30-2, 57-10-1. FABRICATED REPAIR SUPPORT PLATE IAW SRM 51-20-1 AND INSTALLED IAW SRM 51-30-2.Aug 31, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800507Seat Track · corrodedCABIN INTERIOR LEFT SEAT TRACK IS CHIPPED AT SEAT ROW 19. REMOVED OUT OF LIMITS SECTION OF SEAT TRACK, DRILLED UP, DEBURRED, TREATED, PRIMED, AND INSTALLED NEW SECTION IAW B737 53-10-5 FIG 1, 51-10-2, ANS 51-30-2.Aug 30, 1998 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800457Support · corrodedLONG FLOOR SUPPORT BETWEEN BS 294 AND 312 FLOORBEAMS CORRODED BEYOND LIMITS. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT REPAIR, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-21-31.Aug 30, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800459Support · corrodedCORROSION AROUND NUT PLATE HOLE, UPPER AND LOWER SIDES OF LATERAL FLOOR SUPPORT FWD FLANGE BS 320, RBL 10 TO 30. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, MM 51-21-31, AND SRAug 29, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ980460Support · corrodedCORROSION AROUND NUT PLATE HOLES ON UPPER AND LOWER SIDES OF FWD FLAGE OF BS 320 LATERAL FLOOR SUPPORT, RBL 30-56. CLEANED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT, ALODINED, PRIMED, AND INSTALLED FLOOR SUPPORT IAW 51-40-3, 51-10-2, Aug 28, 1998 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR VJ9800497Panel · chafedCHAFED AREA IN ACCESS PANEL AFT UNDERSIDE AREA NR 1 ENGINE PYLON. BLENDED CHAFED AREA OUT OF LIMITS IAW SRM 54-10-1. FABRICATED DOUBLER, DRILLED, DEBURRED, ALODINED, AND PRIMED IAW SRM 51-10-2. INSTALLED DOULER IAW SRM 51-30-2.Aug 28, 1998 · Boeing 7372P6 · Fuselage Main, KeelSDR VJ9800284Battery Pack · dischargedFWD EMERGENCY LIGHT BATTERY PACK FAILED DURING LAY OVER CHECK. REPLACED THE FWD BATTERY PACK.Aug 19, 1998 · Boeing 7372P6 · Emergency LightingSDR VJ9800214Battery Pack · dischargedCENTER CABIN CEILING EMERGENCY LIGHT FLASHED WHEN TESTED. REPLACED EMERGENCY LIGHT BATTERY PACK.Jul 2, 1998 · Boeing 7372P6 · Emergency LightingSDR VJ9800186Wire · chafedSECTION 3 OF EMERGENCY FLOOR PATH LIGHTING PULLED UP. REPAIRED CHAFED WIRE BETWEEN SIDEWALL AND LIGHT TRACK AT PASSENGER SEAT ROW 18DEF, OPS CHECKED NORMAL.Jun 6, 1998 · N1PC · Boeing 7372P6 · Light System WiringSDR VJ9800149Light · inoperativeLIGHT RECEPTACLE INOP ON AFT TRACK FOR THE E-PATH LIGHTING. REPLACED 1 LIGHT RECEPTACLE ON AFT TRACK IAW BAC MM 33-21-27. SYSTEM OPS CHECKED GOOD.May 8, 1998 · Boeing 7372P6 · Emergency LightingSDR VJ9800025Light · inoperativeCENTER AISLE, AFT AND OUTSIDE EMERGENCY LIGHTS INOPERATIVE. PERFORMED FUNCTIONAL CHECK OF INTERIOR AND EXTERIOR EMERGENCY LIGHT SYSTEM ON AIRCRAFT AND OPS CHECKED NORMAL IAW MM 33-51-00.Feb 24, 1998 · N1PC · Boeing 7372P6 · Emergency LightingSDR VJ9800024Battery Charger · failedAPPROXIMATELY 10 LIGHTS WERE NOT ILLUMINATED IN FORWARD SECTION OF EMERGENCY PATH LIGHTING. REMOVED AND REPLACED FWD BATTERY CHARGER, OPS CHECKED OK IAW MM 33-51-51.Feb 23, 1998 · N1PC · Boeing 7372P6 · Emergency LightingSDR 98ZZZM161Adc · inoperativeDURING FLT 920 FROM MCO, THE AIRDATA COMPUTER FAILED. THE AIRCRAFT RETURNED TO MCO. REPLACED THE NR 1 AIR DATA COMPUTER. TESTED THE ADC SYSTEM, ALL NORMAL. (M)Jan 9, 1998 · Boeing 7372P6 · Air Data ComputerSDR ZZDA5224597Door · openFLT 680 - DURING TAXI OUT, FLIGHT ATTENDANT IN THE AFT CABIN REPORTED THE R2 DOOR HAD A GAP AT THE BOTTOM AND THEY COULD SEE LIGHT. THE CREW ADVISED THE DOOR LIGHT WAS OUT IN THE COCKPIT. RETURNED TO THE GATE. MAINTENANCE CHECKED OUT THE DOOR AND FOUND IT TOct 28, 1997 · Boeing 7372P6 · Passenger/Crew DoorsSDR 97ZZZX4745Circuit Breaker · trippedFLT 541 - DURING FLIGHT WHEN GEAR LOWERED, GEAR COULD BE FELT EXTENDING, BUT NO INDICATIONS OF GEAR DOWN, LIGHTS TESTED OK. MANUAL EXTENSION ACCOMPLISHED AND GEAR VISUAL CHECK BY THE TOWER. LANDING UNEVENTFUL, MAINTENANCE INSTALLED GEAR PINS AND AIRCRAFT TAXSep 27, 1997 · N1PC · Boeing 7372P6 · Landing Gear Position and WarningSDR ZZDA2718297Circuit Breaker · trippedDURING THE INITIAL TAKEOFF ROLL, WARNING HORN SOUNDED, L/E FLAP EXT LIGHT DID NOT ILLUMINATE GREEN OR MASTER L/E DEVICES PANEL ON OVERHEAD PANEL. VISUAL INSPECTION SHOWED L/E SLATS AND FLAPS HAD BEEN SELECTED TO PROPER POSITION. AIRCRAFT RETURNED TO GATE. FSep 8, 1997 · Boeing 7372P6 · Leading Edge Slat Position Indicating SystemSDR 97ZZZM953Turbine Blade · brokenON SHORT FINAL OMA, APU FIRE WARNING RED LIGHT AND MASTER FIRE WARNING LIGHT ON. APU SHUTDOWN AND APU FIRE SWITCH PULLED AND ROTATED. BOTTLE DISCHARGED NORMALLY. APU FIRE CHECKLIST COMPLETED (M23206). ACCESS APU AREA, OPEN COWL, PULL APU SHROUD AND NOTED NAug 26, 1997 · N1PC · Boeing 7372P6 · APU Core EngineSDR 97ZZZM1055Light · inoperativeDURING THE PREFLIGHT, THE CREW NOTICED THE R-2 EMERGENCY LIGHT INOP. THE R-2 DOOR EMERGENCY LIGHT WAS RELAMPED AND TESTED OK.Aug 22, 1997 · N1PC · Boeing 7372P6 · Emergency LightingSDR 97ZZZM1056Interrogator · inopAFTER TAKEOFF FROM MCO, FLT 920 - THE PILOT CALLED AND REPORTED NR 2 DME INOP. THE NR 1 DME WAS DEFERRED ON AUG 7, 1997 AND WAS STILL DEFERRED AT THIS TIME. AIRCRAFT RETURNED TO MCO, LANDING WEIGHT WAS OK FOR A NORMAL LANDING. THE NR 2 DME INTERROGATOR WAS Aug 20, 1997 · N1PC · Boeing 7372P6 · DME/TACAN SystemSDR 97ZZZM1068Light · looseEMERGENCY TRACK LIGHTING STRIP KICKED LOOSE BY PASSENGER. RE-ALIGNED LIGHT STRIP AND PLACED BACK INTO POSITION. OPS CHECKED OK. (M)Aug 13, 1997 · Boeing 7372P6 · Emergency LightingSDR 97ZZZM936Wire · looseDURING RON, LEFT OVERWING EXIT FWD EMERGENCY LIGHT INOP. ALL BULBS BURNED OUT. RELAMPED THE LIGHT ASSY, NO HELP. CHECKED VOLTAGE AT LIGHT ASSEMBLY 0 VDC FOUND. REMOVED SIDE WALL PANEL, TRACKED WIRES AND FOUND WIRE BEHIND OVERHEAD COMPARTMENT NOT CRIMPED INAug 3, 1997 · Boeing 7372P6 · Light System WiringSDR 97ZZZM937Light · failedDURING THE LAYOVER SERVICE, THE EMERGENCY LIGHTS WERE TESTED. THE R2 LIGHT PACK DID NOT TEST. LIGHT PACK WAS RE-SEATED INTO THE RECEPTACLE AND TESTED OK.Jul 31, 1997 · Boeing 7372P6 · Emergency LightingSDR 97ZZZM882Flap Track · corrodedDURING C-CHECK, FOUND RIGHT WING INBOARD TRAILING EDGE FLAP INBOARD TRACK HAS SURFACE CORROSION AND PITTING. CLEANED OFF AND RE-EVALUATED. RT WING INBOARD FLAP, INBOARD TRACK IS WITHIN LIMITS IAW B737 GMM 57-53-18. NO FURTHER ACTION IS REQUIRED IAW RES NR 0Jul 21, 1997 · Boeing 7372P6 · Trailing Edge FlapsSDR 97ZZZM881Skin · corrodedDURINC C-CHECK, FOUND VERTICAL STABILIZER RIGHT SIDE FIN STATION 86 HAS CORRODED FASTENER HEADS AND BULGE AT THE SEAM. REMOVED CORRODED SKIN FROM STATION 86 CUT ACCESS HOLE BETWEEN STATION 1179-1271. FABRICATED SKIN REPAIR FROM 2024 T3 .40 IAW SRM 55-30 AND EJul 21, 1997 · Boeing 7372P6 · Vertical Stabilizer, Plate/SkinSDR 97ZZZM880Seat Track · corrodedDURING C-CHECK, FOUND SEAT TRACK FROM BS 727B THROUGH 927, RBL 46, IS CORRODED AT THE FASTENERS AND CHIPPED AND GOUGED AT THE SCALLOPS. TRIMMED AND DRILLED NEW SEAT TRACKS 81.5 INCH BY 3.25 INCH BY 142.25 INCH BY 3.25 INCH FROM BAC 1520-792. INSTALLED IAW 53Jul 21, 1997 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach FittingsSDR 97ZZZM879Seat Track · chippedDURING C-CHECK, FOUND SEAT TRACK OF BS 600 LBL 26 IS CHIPPED OUT OF LIMITS. FABRICATED SEAT TRACK FROM BAC 1520-841 24 INCHES BY 1.5 INCH IAW B737 53-10-5. INSTALLED SEAT TRACK IAW B737 53-10-5. (M)Jul 21, 1997 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach FittingsSDR 97ZZZM878Seat Track · chippedDURING C-CHECK, FOUND SEAT TRACK AT BS 500 LBL 28 HAS CHIP OUT OF LIMITS. FABRICATED SEAT TRACK FROM BAC 1520-792 77.5 INCH BY 3.5 INCH. INSTALLED SEAT TRACK IAW B737 SRM 53-10-5. (M)Jul 21, 1997 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach FittingsSDR 97ZZZM877Press Bulkhead · oil cannedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STR BS 1016 HAS OIL CANNING AT THE ONE O'OCLOCK PIE SECTION. FABRICATED CHANNEL AND STRAP FROM 2024-0 15.75 INCH BY 3.25 INCH AND 2024 T3 .032 16.5 INCH BY 2 INCH IAW B737 SRM 53-10-4. INSTALLED IAW B737 SRM 53-10-Jul 21, 1997 · Boeing 7372P6 · Fuselage Main, BulkheadSDR 97ZZZM875Floorbeam · corrodedDURING C-CHECK, FOUND CABIN FLOORBEAM CORRODED AT STATION 986 LBL 28, UPPER CAP IS CORRODED AT LBL 5, RBL 5, AND RBL 15. FABRICATED REPAIR FLOORBEAM CAP FROM BAC 1505-100817 7075 T8 82 INCH IAW B737 SRM 53-10-9. INSTALLED IAW B737 SRM 51-30-2.Jul 21, 1997 · Boeing 7372P6 · Fuselage Main, Floor BeamSDR 97ZZZM935Angle · corrodedDURING C-CHECK AT AERO CORP, BS 1138 RBL 25 HORIZONTAL CROSSBEAMS 'L' ANGLE CORRODED BEYOND LIMITS. REMOVED ANGLE, FABRICATED THE ANGLE, DRILLED AND INSTALLED.Jul 16, 1997 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR 97ZZZM934Floorbeam · crackedDURING C-CHECK AT AERO CORP, FOUND FLOORBEAM CRACKED IN TWO PIECES, BS 454 AND 482 IN WEB AND ACROSS LOWER FLANGE. ALSO, CRACKED BETWEEN BS 475 AND 484 IN WEB AREA. REPLACED STATION SUPPORT RAIL IAW SRM 51-30-8.Jul 16, 1997 · Boeing 7372P6 · Fuselage Main, Floor BeamSDR 97ZZZM933Angle · corrodedDURING C-CHECK AT AERO CORP, FOUND BS 1138 48 RT LOWER HORIZONTAL CROSS BEAM 'T' ANGLE HAS HEAVY CORROSION OUT OF LIMITS RB 20 AT WEB. REMOVED 'T' ANGLE, FABRICATED, DRILLED AND INSTALLED THE ANGLE. (M)Jul 16, 1997 · Boeing 7372P6 · Fuselage Miscellaneous StructureSDR 97ZZZM931Seat Track · corrodedDURING C-CHECK, FOUND CABIN SEAT TRACK AND FLOOR SUPPORT CORRODED AT FASTENER HOLES BS 947-967 RBL 0-20. REMOVED CORROSION OF FLOOR SUPPORT AND SEAT TRACK LOSS MATERIAL 20 PERCENT OUT OF LIMITS. FABRICATED SUPPORT AND TRACK MATERIAL FOR THE TRACK, BAC 1520-8Jul 8, 1997 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach FittingsSDR 97ZZZM930Floorbeam · corrodedDURING C-CHECK, FOUND AFT CARGO CABIN FLOORBEAM HAS CORROSION BULGE AT BS 967 BL0 TO RBL. REMOVED CORROSION LOSS MATERIAL MORE THAN 20 PERCENT. FABRICATED NEW FLOORBEAM LBL 6 INCH TO RBL 57. MATERIAL T-CHORD 7075 T-6 DIMENSIONS 11.75 BY 1.125 INCH BY 1 INCHJul 8, 1997 · Boeing 7372P6 · Fuselage Main, Floor BeamSDR 97ZZZM932Frame · elongated holesDURING C-CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FS 807 STRINGER 29R VERTICAL FLOOR SUPPORT AT FRAME HAS ELONGATED HOLES. FOUND FRAME DOUBLE DRILLED HOLE OUT OF LIMITS IAW SRM 51-10-1, FABRICATED FORMED CHANNEL REPAIR 7075-T6-40. TREATED AND PRIMED IAWJul 3, 1997 · Boeing 7372P6 · Fuselage Main, Frame
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