Boeing 727-228

Service difficulty reports · 1,323

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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 aircraft_model_key = '727228'
  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 96ZZZM598Floor Support · corrodedDURING D-CHECK, FOUND BETWEEN STATION 460 AND 420 FLOOR SUPPORT ANGLE RBL 10 HAS CORROSION. REMOVED FLOOR SUPPORT 400 TO 420 CORROSION EXCEED SRM LIMITS 51-10-6. FABRICATED NEW FLOOR SUPPORT ANGLE 20 INCH BY 2 INCH BY 2.5 INCH 7075 T-6 .125 PER SRM 51-40-3. Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM597S-Duct · corrosionDURING D-CHECK, FOUND NR 2 ENGINE INLET 'S' DUCT HAS INNER SKIN BULGE AT 6 O'CLOCK BETWEEN 10-21 INCH FORWARD OF LOWER AFT EDGE. REMOVED FASTENERS PER SRM 51-30-2. CLEANED CORROSION INNER SKIN PER SRM 51-10-6 MATERIAL LOSS .003. FOUND CRACK AT BETWEEN 10-21Jul 9, 1995 · N727DH · Boeing 727228 · Nacelle/Pylon StructureSDR 96ZZZM596Skin · corrodedDURING D-CHECK, NR 2 ENGINE INLET INNER SKIN BULGE AND CRACKED JUST BELOW PRODUCTION JOINT 7 O'CLOCK. REMOVED FASTENERS PER SRM 51-30-2. REMOVED ALL DAMAGED AREA PER SRM 54-10-3. FABRICATED DOUBLER AND FILLER AS 7075-T6 (DOUBLER .050 AND FILLER .040) PER SRJul 9, 1995 · N727DH · Boeing 727228 · Engine Cowling SystemSDR 96ZZZM595Floor Beam · corrodedDURING D-CHECK, FOUND FLOOR BEAM STATION 400 TOP FLANGE BL 0 TO LBL 25 CORROSION. REMOVED CORROSION AS PER 51-10-6. OUT OF LIMITS SEVERAL SPOTS BETWEEN RBL 3 THROUGH LBL 33. ALODINE AND PRIME PER SRM 51-10-2. CUT UPPER CHORD OF FLOOR BEAM FROM RBL 5 THROUGJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Floor BeamSDR 96ZZZM594Floor Support · corrosionDURING D-CHECK, FOUND NR 2 SEAT TRACK CHANNEL SUPPORT HAS BARE METAL AND SURFACE CORROSION AT STATION 950A-950B AND LCL 25. FABRICATED AND INSTALLED NEW SEAT TRACK ANGLE SUPPORT PER SRM 51-10-1 PAR 4 19.75 INCH BY .75 INCH BY .75 INCH 2024T-3 .040 ANGLE.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM593Floor Support · corrodedDURING D-CHECK, FOUND FLOOR SUPPORT BEAM HAS CORROSION AT STATION 1130 RCL 31-45. REMOVED CORROSION PER SRM 51-10-6. MATERIAL LOST .100 BEYOND LIMITS. FABRICATED ANGLES 7075-T6 .100 1 INCH BY 2O INCH. INSTALLED ANGLE REPAIR PER SRM 51-40-4.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM592Floor Support · corrosionDURING D-CHECK, FOUND CRACK AND CORROSION BY NR 2 RIGHT SERVICE DOOR FLOOR SUPPORT BEAM STATION 1070 RRBL 57 TO 64. CRACK IS BOTTOM SIDE OF BEAM SUPPORT. CUT OUT CORRODED AREA AND STARTED FABRICATING REPAIR AS PER SRM 53-10-8. FABRICATED T-ANGLE OUT OF 7075Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM591Floor Support · corrodedDURING D-CHECK, FOUND COCKPIT FLOOR SUPPORT IS CRACKED FS 283 RBL 7. STOP DRILLED CRACK .25 INCH PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 FIG 1 8 INCHES 2024-T3 .050.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM590Floor · corrodedDURING D-CHECK, MAIN CABIN FLOOR, CORROSION UNDER REINFORCEMENT CHORD AT FS 1176 RBL 20 BETWEEN SUB FLOOR AND CHORD. REMOVED FASTENERS AND REMOVED CHORD ANGLE AT STATION 1176.9 PER SRM 51-30-2. CUT OUT DAMAGED AREA OF SUB FLOOR 15 INCHES BY 20 INCHES AND CLEJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Floor PanelSDR 96ZZZM589Skin · corrodedDURING D-CHECK, FUSELAGE EXTERIOR SKIN DOUBLER REPAIR FS 1152 STRINGER 27L UPGRADE PER SRM. REMOVED DOUBLER. REMOVED CORROSION, FOUND GRINDOUT TO BE BEYOND LIMITS AS PER SRM 51-10-6. FILLED GRINDOUT PER SRM 51-40-1. FABRICATED .125 2024-T3 8 INCH BY 11 INCJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM588Frame · crackDURING D-CHECK, MAIN CARGO LEFT FRAME CRACKED STATION 930 STRINGER 14-15L AT STUB FRAME ATTACHMENT FITTING. STOP DRILLED CRACK AS PER SRM 51-10-1. FABRICATED PARTS PER STEP ON OF DHL/BOEING FAX 95 14TR DATED MAY 26, 1995. INSTALLED REPAIR PARTS PER DHL FAC Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, FrameSDR 96ZZZM587Frame · crackedDURING D-CHECK, MAIN CABIN FRAME CRACKED STATION 930 STRINGER 14R UNDER STUB FRAME SUPPORT FITTING. CRACK GOES FROM HOLE TO HOLE. FABRICATED PARTS PER STEP ONE ON DHL/BOEING FAX 95-14TR DATED MAY 26, 1995. OVERSIZE HOLES.03125 FRAME ONLY PER STEP TWO OF DHL/Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, FrameSDR 96ZZZM586Ditching Web · crackedDURING D-CHECK, AFT BAGGAGE DITCHING WEB IS TORN AND CRACKED FS 1180 RBL 55. STOP DRILLED AT END OF CRACK AS PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .025 6 INCH BY 3 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM585Stringer · corrodedDURING D-CHECK, JUST FORWARD OF STATION 460 STRINGER 3R HAS HEAVY CORROSION. REMOVED CORROSION FORWARD STATION 460 STRINGER 3R PER SRM 51-10-6, OUT OF LIMITS. INSTALLED STRINGER REPAIR PER SRM 53-10-3 7075-T6 .040 10 INCH BY 1 INCH BY 1 INCH. ALODINED AND Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR 96ZZZM584Stringer · corrodedDURING D-CHECK, STATION 420 AFT SIDE OF RIB STRINGER 3L HAS CORROSION THROUGH STRINGER TOP FLANGE. CUT OUT DAMAGED SECTION AS PER SRM 53-10-3. INSTALLED 1 INCH BY .5 INCH REPAIR AS PER SRM 53-10-3 FIG 2 PART 1 10 INCH J-ANGLE BAC 1493-508.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR 96ZZZM583Angle · corrodedDURING D-CHECK, MAIN CABIN FLOOR HAS CORROSION AN ANGLE AT STATION 1176.9 RBL 61-66. REMOVED FASTENERS AND CHORD ANGLE AT STATION 1176.9. FOUND CORROSION BEYOND LIMITS. CLEANED AREA AND PRIMED PER SRM 51-10-2. REPLACED CHORD ANGLE PER SRM 51-10-1 PAR 4.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM582Chord · corrodedDURING D-CHECK, CORROSION ON FLOOR REINFORCEMENT CHORD BOTTOM SIDE AT STATION 1176.9 LBL 37 INCH AND 48 INCH. REMOVED FASTENERS AND CHORD ANGLE AT STATION 1176.9 PER SRM 51-30-2. CUT OUT FLOOR LBL 26 INCH, CORROSION BEYOND LIMITS 20 INCH BY 15 INCH APPROX CLJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM581Floor Support · corrodedDURING D-CHECK, MAIN CABIN FLOOR SUPPORT ANGLE IS CORRODED AT SPLICE AT STATION 923 RBL 65 INCHES. REPLACED ANGLE SPLICE PER SRM 51-10-1 AND SRM 51-30-2 AT STATION 923 RBL 65 INCHES.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM580Floor Support · corrodedDURING D-CHECK, MAIN CABIN FLOOR SUPPORT ANGLE IS CORRODED AT SEVERAL AREAS AT STATION 760-849 LBL 65 INCHES. REMOVED FLOOR SUPPORT ANGLE AS PER SRM 51-30-2. INSTALLED NEW FLOOR SUPPORT ANGLE AS PER SRM 51-10-1 PAGE 4 AND SRM 51-30-2. SIZE 107 INCH BY 1.25 Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM579Floor Support · corrodedDURING D-CHECK, MAIN CABIN FLOOR SUPPORT ANGLE IS CORRODED AT STATION 745 LBL 65 INCHES. REMOVED FLOOR SUPPORT ANGLE PER SRM 51-30-2. INSTALLED NEW FLOOR ANGLE SUPPORT PER SRM 51-10-1 PAGE 4 AND SRM 51-30-2, SIZE 107 INCHES BY 1.5 INCH BY 1.25 INCH BAC 1515-Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM578Web · corrodedDURING D-CHECK, MAIN CABIN WEB IS CORRODED AT UNDER SIDE STATION 760-783 LBL 68 INCHES. REPLACEMENT OF WEB AT STATION 760-783 LBL 68 INCHES 7075-T6 .071 AS PER SRM 51-10-1 PAR 4.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM577Rib · corrodedDURING D-CHECK, RIB LEFT SIDE STATION 1354 INSIDE TORQUE BOX LOWER SURFACE OF LOWER ANGLE HAS CORROSION ON HORIZ STAB. REMOVED CORROSION AS PER SRM 51-10-6 MATERIAL LOSS .005. INSTALLED ANGLE REPAIR 2024-T3 .063 2 INCH BY 10 INCH AS PER SRM 51-40-3.Jul 9, 1995 · N727DH · Boeing 727228 · Horizontal Stabilizer StructureSDR 96ZZZM576Skin · corrodedDURING D-CHECK, LEFT HORIZONTAL RIB INNER CHORD AND ADJACENT SKIN IS CORRODED FROM BS 1342.4 TO BS 1345. CUT OUT DAMAGED AREA OF SKIN 8 INCH BY 7 INCH .063, REMOVED FASTENERS, REMOVED CORROSION ON CHORD ANGLE, MATERIAL LOSS .004 AS PER SRM 51-10-6. ALODINED Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM575Skin · corrodedDURING D-CHECK, LEFT VERTICAL EXTERNAL SKIN AT LBL 19 INSIDE TORQUE BOX IS HEAVILY CORRODED FROM BS 1334 TO BS 1346 AND S-10 TO LOWER TORQUE BOX CHORD ANGLE. REMOVED SURFACE CORROSION PER SRM 51-10-6. CUT OUT DAMAGED AREA PER SRM 55-30-3 AND ALODINE AND PRIMJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM574Angle · crackedDURING D-CHECK, EMPANNAGE, LEADING PANEL NR 9707 FOR VERTICAL STABILIZER, HAS CRACKED ATTACHING ANGLE ON RIGHT SIDE OF VERTICAL STABILIZER FORWARD SPAR JUST OUTBOARD OF RIGHT VERTICAL FIN UPPER TERMINAL FITTING, AT UPPER END OF ANGLE. REMOVED T-ANGLE FOR REPAJul 9, 1995 · N727DH · Boeing 727228 · Vertical StabilizerSDR 96ZZZM573T-Angle · crackedDURING D-CHECK, EMPANNAGE, T-ANGLE CRACKED AT FORWARD SIDE OF VERTICAL STABILIZER FORWARD SPAR (L/E PANEL NR 9707 ATTACH ANGLE) AT LEFT SIDE UPPER END, JUST OUTBOARD OF LEFT VERTICAL FIN UPPER TERMINAL FITTING. REMOVED T-ANGLE FOR REPAIR. STOPPED DRILLED CRAJul 9, 1995 · N727DH · Boeing 727228 · Vertical StabilizerSDR 96ZZZM572Plate · crackedDURING D-CHECK, MAIN CABIN STATION 1180 LBL 27, DITCHING PLATE CRACKED. STOP DRILLED AT THE END OF CRACK PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .025 6 INCH BY 4 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM571Plate · crackedDURING D-CHECK, MAIN CABIN STATION 1180 LBL 30, DITCHING PLATE IS CRACKED. STOP DRILLED AT THE END OF CRACK PER SRM 51-10-1. FABRICATED DOUBLER REPAIR 2024-T3 .025 6 INCH BY 4 INCH. INSTALLED DOUBLER AS PER SRM 51-40-2.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM570Bracket · corrodedDURING D-CHECK, LOWER CARGO DOOR NR 2 AFT VERTICAL SUPPORT BRACKET FOR EXTERNAL DOOR HANDLE IS CORRODED AT BOTTOM. REMOVED FASTENERS ON VERTICAL SUPPORT BRACKET PER SRM 51-30-2. REMOVED CORRODED VERTICAL SPACER AND FABRICATED 2024-T3 .050 5 INCH BY 5 INCH PEJul 9, 1995 · N727DH · Boeing 727228 · Cargo/Baggage DoorsSDR 96ZZZM569Frame · corrodedDURING D-CHECK, FUSELAGE FRAME 1166 STRINGER 17R HEAVY CORROSION. REMOVED FASTENERS AS PER SRM 51-30-2. CUT OUT DAMAGE AREA AS PER SRM 51-40-3. FABRICATED FRAME REPAIR AS PER SRM 51-40-3 MATERIAL 7075-T6 ,090 11 INCH BY 1 INCH BY 9 INCH FILLER 7075-T6 .100 Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, FrameSDR 96ZZZM568Intercostal · cracksDURING D-CHECK, FUSELAGE STATION 1070-1077 TWO EACH CRACKS AT INTERCOSTAL FASTENER STRINGER 6R. REMOVED INTERCOSTAL STATION 1070-1077 STRINGER 6R PER SRM 51-10-1 PAR 4 AND 51-30-2. FABRICATED INTERCOSTAL PER SRM 51-10-1 PAR 4. INSTALLED INTERCOSTAL PER SRM Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM567Intercostal · crackedDURING D-CHECK, NLG W/W LT SIDE FS 290 INTERCOSTAL WEB CRACKED TWO PLACES AROUND LIGHTENING HOLES. FABRICATED WEB LEFT SIDE FS 290 NLG W/W AS PER SRM 51-10-1 PAR 4.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM566Bulkhead · corrosionDURING D-CHECK, CORROSION AFT SIDE OF BS 1183 ABOVE NR 1 PYLON (2 INCH). REMOVED DOUBLER AND REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED PER SRM 51-10-2. FABRICATED NEW DOUBLER AND INSTALLED PER SRM 51-30-2 (2024-T3 .040 2.5 INCH BY 3 INCH).Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, BulkheadSDR 96ZZZM565Sill · corrosionDURING D-CHECK, CORROSION UNDER FORWARD TO CENTER NUT PLATES OF INBOARD LOWER SILL ATTACH FLANGE AT RIGHT AFT GALLEY DOOR. REMOVED CORROSION, CORROSION BEYOND LIMIT, MADE TYPICAL ANGLE REPAIR PER SRM 51-40-3. CUT OUT DAMAGED AREA PER SRM 51-40-3. REPAIRED AJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM564Stringer · crackDURING D-CHECK, MAIN CABIN AT STATION 852 STRINGER 16L HAS CRACK IN STRINGER. INSTALLED NEW STRINGER PER SRM 51-10-1.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR 96ZZZM563Skin · dentedDURING D-CHECK, STATION 1183 TO 1203 BETWEEN STRINGER 25R AND 24R, HAS DENT FILLED WITH BONDO AND HAS A GOUGE JUST AFT OF 1183 BUTT SEAM. REMOVED FILLER MATERIAL PER SRM 51-40-1. FOUND DENT TO BE BEYOND LIMITS PER SRM 53-30-1. CUT OUT DAMAGED AREA AS PER SRJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM562Wing Tip Web · corrosionDURING D-CHECK, HEAVY CORROSION ON WEB INTERIOR OF WING TIP. CUT OUT DAMAGED AREAS WITH CORROSION OUT OF LIMITS PER SRM 51-40-2. CLEANED AREA PER SRM 51-10-6. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED DOUBLER 2024-T3 .040 7.5 INCH BY 4 INCH. INSTALLJul 9, 1995 · N727DH · Boeing 727228 · Wing Miscellaneous StructureSDR 96ZZZM561Bulkhead · crackDURING D-CHECK, BULKHEAD HAS TWO CRACKS AT STATION 126.3 RIGHT JUST UNDER AFT STAIR ACTUATOR ATTACH FITTING. REMOVED FASTENERS FROM INBOARD VERTICAL WEB ON RIGHT SIDE TORQUE BOX. REMOVED FASTENERS AND VERTICAL STIFFENER, CUT OUT CRACKED AREA OF WEB STATION 1Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, BulkheadSDR 96ZZZM560Plate · crackedDURING D-CHECK, FOUND MAIN CABIN STATION 1180 LBL 60, DITCHING PLATE HAS 1 INCH HOLE THAT IS NOT COVERED. STOP DRILLED AT THE END OF CRACK AS PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .025 6 INCH BY 4 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM558Skin · corrosionDURING D-CHECK, FOUND FORWARD LOWER C/C AND AIR COND BAY INT'R BS 723E STRINGER 26R LAP SEAM UPPER SIDE CORROSION LEVEL 1. REMOVED RIGHT RAM AIR DUCT FOR S/M ACCESS. REMOVE HI-LOKS PER SRM 51-30-2. CUT OUT DAMAGED SKIN CORROSION OUT OF LIMITS AS PER SRM 53-Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM557Stringer · corrosionDURING D-CHECK, LOWER FORWARD AIR COND BAY INT'R BS 736F STRINGER 26R CENTER BOTTOM STRINGER TO TIE CLIP CORROSION LEVEL 1. REMOVED FASTENERS BS 725F TO 740 STR 26R AS PER SRM 51-30-2. CUT OUT 9 INCHES OF STRINGER 26R BS 729F TO 738F. REMOVED TIE CLIP FOR CJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR 96ZZZM556Skin · crackedDURING D-CHECK, FOUND AFT AIR STAIR COMPARTMENT WEB CRACKED AT LIGHTENING HOLE STATION 1260 LEFT. INSTALLED REPAIR ON WEB AT LIGHTENING HOLE STATION 1260 LEFT. REPAIR DIMENSIONS 3 INCH BY 4 INCH 2024-T3 AS PER SRM 51-40-2.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM555Ditching Plate · crackedDURING D-CHECK, FOUND MAIN CABIN STATION 1180 RBL 28, DITCHING PLATE IS CRACKED. FABRICATED NEW DITCHING PLATE PER SRM 51-10-1. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER 2024-T3 .025 6 INCH BY 3 INCH PER SRM 51-10-1.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM554Angle · crackedDURING D-CHECK, EXTERIOR FUSELAGE VERTICAL STIFFENER ANGLE CRACKED AT LOWER END STATION 950 AFT SIDE OF RIGHT WHEEL WELL AFT BULKHEAD RBL 54 INCHES. STOP DRILLED AS PER SRM 51-10-1. INSTALLED TYPICAL WEB REPAIR AS PER SRM 51-40-2 AT STATION 950 AFT SIDE OF RJul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM553Skin · corrosionDURING D-CHECK, FOUND CORROSION ON UPPER SURFACE OF RIGHT RAM AIR PLENUM ABOVE RIGHT SECONDARY HEAT EXCHANGER. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT 'L' ANGLE SUPPORT FOR ACCESS. REMOVED CORROSION PER SRM 51-10-6. ALODINED AND PRIMED PER SRM 51-10-2. Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM552Skin · corrosionDURING D-CHECK, FOUND CORROSION ON UPPER SURFACE OF LEFT RAM AIR PLENUM ABOVE SECONDARY HEAT EXCHANGER. REMOVED CORROSION AS PER SRM 51-10-6. REMOVED FASTENERS PER SRM 51-30-2. NDT CHECK LOSS MATERIAL .090. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96ZZZM551Track · damagedDURING D-CHECK, FOUND NR 4 CABIN FLOOR TRACK UPPER SURFACE AND LIPS DAMAGED AND WORN AT APPROX STATION 764. REPLACED UPPER SURFACE DAMAGED LIPS WITH SEAT TRACK REPAIR AS PER SRM 53-10-5 APPROX 6 INCHES FROM STATION 760 TO 754. TREATED AND ALODINED AND PRIMERJul 9, 1995 · N727DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZM550Web · crackedDURING D-CHECK, FOUND AFT CARGO, CRACK AND BULGE IN WEB FS 990-1010 STRINGER 30. CUT OUT DAMAGED AREA. ALODINED AND PRIMED AREA. INSTALLED FILLER 2024-T3. INSTALL DOUBLER AS PER SRM 51-40-2, SIZE 5 INCH BY 4 INCH AND 5 INCH BY 3 INCH .050 2024-T3.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM549Seat Track · damagedDURING D-CHECK, FOUND NR 6 CABIN FLOOR TRACK LIP DAMAGED BETWEEN STATION 1164 AND STATION 1173 RBL 45.50. REMOVED SLAT TRACK NR 6 FROM STATION 1164 TO 1178 PER SRM 53-10-5. INSTALLED SEAT TRACK NR 6 FROM STATION 1164 TO 1173 PER SRM 53-10-5.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZM548Seat Track · corrodedDURING D-CHECK, NR 5 TRACK LOWER SURFACE CORRODED AROUND FASTENERS BETWEEN STATION 1130 AND STATION 1136 RBL 24.75. REMOVED FASTENERS AS PER SRM 51-30-2. REMOVED CORROSION FOUND OUT OF LIMIT. CUT OUT DAMAGE SECTION SEAT TRACK FOR REPAIR. FABRICATED SEAT TRJul 9, 1995 · N727DH · Boeing 727228 · Fuselage, Seat/Cargo Attach Fittings
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