Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  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 07FDEA02353Stringer Clip · crackedAFT PIT STRINGER CLIP CRACKED STA 950E STR 28L REMOVED CRACKED STRINGER CLIP REPLACED WITH NEW CLIP PART NR 6611809-2 IAW SRM 51-30-2 PG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 2, 2007 · N286FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02352Floorbeam · corrodedAFT UPPER MAIN DECK, CORROSION AROUND NUT PLATE HOLE ON UPPER SURFACE OF UPPER T-CAP STA 950C LBL27.5". REMOVED CORROSION FROM AFT MAIN DECK UPPER SURFACE NUTPLATE HOLE ON T-CAP STA 950C LBL 27.5. HFEC AREA, NO DEFECTS NOTED. SHOT PEEN AREA, TREAT PRIMED, Jul 2, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02351Shear Tie · corrodedAFT PIT STA 990 STR 26-27 L SHEAR TIE CORRODED STR 26-27 L. REMOVED 2 EA FASTENERS REF 51-30-2. REMOVED CORROSION REF SRM 51-10-1 NDT'D IAW B727 NDT MAN PART 4 51-00-00 FIG 2 ORIGINAL THICKNESS .063. REMOVED .003 ;.060 MATERIAL REMAINING WITHIN LIMITS REF SJul 2, 2007 · N286FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA02347Floorbeam · failedON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 460 FLOORBEAM UPPER CHORD RBL 33" TO 49" DOES NOT CONFORM TO SRM. REMOVED EXISTING REPAIR ANGLES IAW SRM 51-30-2 FABRICATED NEW REPAIR ANGLE FOR BS 460 FLOORBEAM UPPER CHORD RBL 33" TO 48", IAW FED EX Jun 30, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02313Floorbeam · gougedCABIN BS 500 FLOORBEAM UPPER CHORD HAS SCRATCHES ON UPPER SURFACE BETWEEN BL 0 AND RBL 25 BLENDED AREA, VERIFIED MATERIAL LOSS, AND NO CRACK BY NDT, FLAP PEENED REF EA 7-5310-113039, TREATED AND PRIMED AREA. APPLIED CORROSION RESISTANT COMPOUND THIS IS CLASSIJun 28, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02312Floorbeam · corrodedCABIN STA 940 FLOORBEAM HAS CORROSION BETWEEN BEAM UPPER FLANGE AND SEAT TRACK AT BL 0 REMOVED CORROSION FROM FLOORBEAM AT STA 940 BL 0 IAW B727 SRM 51-10-1, ORIGINAL .125 REMAINING .123. HFEC NO DEFECTS NOTED ROTO PEENED FLOORBEAM. TREATED AND PRIMED REWORKJun 28, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02311Floorbeam · damagedCABIN BS 540 FLOORBEAM UPPER CHORD HAS SCRATCHES ON UPPER SURFACE BETWEEN RBL2 AND RBL 10 BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS ORIGINAL .125 REMOVAL .005, SELF CONTAINED SHOT PEEN AREA. APPLIED ALODINE AND PRIME, APPLIED CORROSION INHIBITING COMPOUND, Jun 28, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02310Floorbeam · damagedCABIN BS 480 FLOORBEAM UPPER CHORD HAS SCRATCHES BETWEEN RBL 48 AND RBL 60 BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS ORIGINAL .130 REMOVAL .002, SELF CONTAINED SHOT PEEN AREA, APPLIED ALODINE AND PRIMED. APPLIED CORROSION INHIBITING COMPOUND, REF SRM 51-1Jun 28, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02309Floorbeam · damagedCABIN FLOORBEAM AT BS 480 HAS SCRATCHES ON UPPER SURFACE OF UPPER TEE BETWEEN RBL 27 AND RBL 40 BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS ORIGINAL .130 REMOVAL .008, SELF CONTAINED SHOT PEEN AREA, APPLIED ALODINE AND PRIMED. APPLIED CORROSION INHIBITING COMJun 28, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02307Skin · crackedPNEU GROUND CONNECTION SERVICE DOOR (#3903) CUTOUT HAS CRACK AT I/B AFT CORNER. FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED. REF EA 7-53330-10732, SRM 51-10-2, 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR STOP DRILLED CRACK REF BOEING 727 SRM 51-10-1Jun 28, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02306Shear Tie · corrodedAFT PIT SHEAR TIE CORRODED STA 950D BETWEEN STR 28-29L CUT OUT DAMAGE AREA OF SHEAR TIE AT STA 950D, BETWEEN STRINGER 28-29 L IAW BOEING SRM 53-10-4, REPAIR 3. FABRICATED REPAIR BRACKET AND FILLER IAW BOEING SRM 53-10-4. REPAIR 3. HEAT TREATED REPAIR BRACKEJun 28, 2007 · N286FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA02305Shear Tie · corrodedAFT PIT SHEAR TIE CORRODED STA 990 STR 28-29L FAB SHEAR TIE AND SHIM REF SRM 53-10-4. TREATED AND PRIMED REPAIR MATERIAL FOR SHEAR TIE 7075-O-071. HEAT TREATED TO T6, CUT OUT DAMAGED AREA, INSTALLED REPAIR PART REF SRM 53-10-3. THIS REPAIR CLASSIFIED AS MAJJun 28, 2007 · N286FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA02304Stringer · unknownFOUND REPAIR LOCATED AT STR S-27R FROM BS 674 TO 700 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR IAW BOEING 727 SRM 51-10-2. REPAIRED STRINGER USING NEW STRINGERJun 28, 2007 · N286FE · Boeing 727233 · Standard Practices/StructuresSDR 07FDEA02295Frame · corrodedFWD PIT BILGE, BODY FRAME SHEAR TIE IS CORRODED, BS 72OF STR 28L- 28R, WL148. REMOVED CORROSION, REFERENCING SRM 51-10-1, ORIGINAL THICKNESS .072", BLENDED TO .067" MATERIAL LOSS .005" WITHIN LIMITS, REFERENCING SRM MEASURED WITH TOOL NR IN17-9593 CAL DUE Jun 27, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02294Seat Track · corrodedCABIN, LBL 25 SEAT TRACK IB FLANGE HAS CORROSION ON UPPER SURFACE BETWEEN BS 400 AND BS 460. REMOVED CORROSION IAW B727 SRM 51-10-1, ORIGINAL .080", REMAINING .059" REF EA NR 7- 5310-113056, ROTO PEENED SEAT TRACK FLANGE AT STA 400-460 LBL 25. TREATED AND PJun 27, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02293Panel · crackedLT WING OB TE FLAP WELL LWR FIXED PANEL CORRUGATED SUPPORT PLATE IS CRACKED RSS 516-523. REPLACED CORRUGATED SPLICE IAW SRM 51-30-02.Jun 27, 2007 · N286FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA02292Frame · corrodedFWD PIT BILGE BODY FRAME, SHEAR TIE IS CORRODED, BS 720A, 2" OB OF STR 28R, WL 148. REMOVED CORROSION. ORIGINAL - .050", REMAINING - .046", MATERIAL LOSS - .004", WITHIN LIMITS REF SRM 53-10-1, TOOL NR 18172, CAL DUE 1-19-08. TREATED AND PRIMED REF 51-10-6 Jun 27, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02291Frame · corrodedFWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CORRODED BS 720A, STR 27L-28L, WL 148. REMOVED CORROSION, ORIGINAL .050", REMAINING- .045", MATERIAL LOSS- .005", WITHIN LIMITS REF SRM 51-10-1 AND 53-10-1, TOOL NR 2221 CAL DUE 4-24-08, STRAIGHTENED SHEAR TIE REFJun 27, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02289Frame · corrodedFWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CORRODED BS 720B, STR 28L-28R, WL 148. REMOVED CORROSION, ORIGINAL THICKNESS- .063", REMAINING- .058", MATERIAL LOSS- .005". WITHIN LIMITS REFERENCING SRM 51-10-6 AND 53-10-1 USING NR 2221 CAL DUE 4-24-08. STRAJun 27, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02284Floorbeam · corrodedAFT UPPER MAIN DECK , FLOORBEAM TOP CAP HAS CORROSION AND A DRILL START ON UPPER SURFACE, STA 950E, LBL 35. REMOVED DAMAGE AREA OF FLOORBEAM AT STA 950E LBL 35 IAW B727 SRM 53-10-8. FABRICATED REPAIR ANGLES (2 EA) AND FILLER FROM BAC1490-2888 PO NR 10156633 Jun 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02283Shear Tie · crackedFWD PIT BILGE, BODY FRAME SHEAR TIE, IS BUCKLED/CRACKED BS 720B, STR 25L - 26L, WL 152. REPLACED DAMAGED SHEAR TIE AT FWD PIT STA 720B, BETWEEN STR 25L AND 26L, REF SRM 51-30-2 PG 1-12.Jun 26, 2007 · N286FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA02279Frame · misrepairedON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 560 ON FRAME BETWEEN STR S-22L AND S-26, DID NOT COMFORM TO SRM 51-40-3 PG 1-6. REMOVED OLD DOUBLER AND FILLER, FABRICATED NEW DOUBLER AND FILLER, HEAT TREATED, ALODINED AND PRIMED REF SRM 51-40-3 PG 1-6.Jun 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02278Skin · misrepairedON AGING A/C INSP, FOUND EXTERNAL REPAIR LOCATED AT BS 1120 TO 1130, STR S-18L TO S-19L, DID NOT CONFORM TO SRM 53-30-1. REMOVED EXISTING DOUBLER PER SRM 51-30-2. BLENDED OUT DAMAGE, EXTENDED CUT OUT TO REMOVE FASTENER HOLES WITH NO EDGE DISTANCE, REF 53-30-Jun 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02277Frame · misrepairedON AGING A/C INSP, FOUND REPAIR LOCATED AT BS 1050 FRAME BETWEEN STR S-26R AND S-28R DID NOT CONFORM TO SRM 51-40-3. REMOVED EXISTING REPAIR, REMOVED Z-ANGLE, GUSSET, TIE DOWN BRACKET FOR ACCESS. FABRICATED NEW REPAIR PARTS, REF SRM 51-4O-3 FIG 1. HEAT TREAJun 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02276Skin · corrodedFUSELAGE BS 720 TO BS 740, S-27L TO S-26L EXTERNAL DOUBLER CORRODED ON BOTH SIDES AROUND DUCT CUTOUT. REMOVED CORROSION REFERENCING SRM 51-10-1 VERIFIED MATERIAL TO BE .125". REMOVED .OO6". REMAINING MATERIAL .119" FOUND TO BE WITH IN LIMITS REFERENCING SJun 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02265Shear Tie · corrodedFWD PIT BILGE BODY FRAME, SHEAR TIE, IS CORRODED, BS 720, STR 27L-28L, WL 148. LEVEL 1 CORROSION. REMOVED CORROSION, TREATED AND PRIMED REF SRM 51-10-6 AND 51-10-2. ORIGINAL THICKNESS .050". REMAINING .047" MATERIAL LOSS IS .003" WITHIN LIMITS REF SRM 53Jun 23, 2007 · N286FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA02261Door Frame · corrodedHIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, BOTTOM FRAME, INNER SURFACE IS CORRODED UNDER LEVELING COMPOUND FROM FWD TO AFT END OF FRAME. [07-06-07] DRILLED UP NEW BEAM PER SRM 51-30-5 PG.1, INSTALLED LOWER BEAM ON AFT SERVICE DOOR, PER SRM 51-10-1 PG.10Jun 22, 2007 · N286FE · Boeing 727233 · Service DoorsSDR 07FDEA02260Door Frame · corrodedHIDDEN DAMAGE INSP LT AFT SERVICE DOOR LOWER AFT STOP FITTING HAS CORROSION. [07-06-07] DRILLED UP NEW STOP FITTING PER. SRM 51-30-5 PG 1, INSTALLED IT, PER SRM 51-10-1 PG. 10 AND 51-30-2 PG. 2-5. INSTALLED CORROSION INHIBITING COMPOUND TO THE LOWER PART OFJun 22, 2007 · N286FE · Boeing 727233 · Service DoorsSDR 07FDEA02259Door Frame · corrodedHIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR 2ND FRAME, 4" FROM FWD EDGE, UPPER SURFACE OF LOWER FRAME SHEAR TIE IS CORRODED. [07-26-07] BLENDED OUT DAMAGE, ORIGINAL MATERIAL IS .050", MATERIAL LOSS OF .001", REMANING MATERIAL IS .049", WITHIN LIMITS. TJun 22, 2007 · N286FE · Boeing 727233 · Service DoorsSDR 07FDEA02258Door Frame · noneFOUND ON HIDDEN INSPECTION LT AFT SERVICE DOOR, 3RD FRAME, 9" FROM FWD EDGE, LOWER SHEAR TIE, LOWER SURFACE IS CORRODED. [07-26-07] BLENDED OUT DAMAGE, ORIGINAL MATERIAL IS .045", MATERIAL LOSS OF .001, REMAINING MATERIAL IS .044" TOOL USED IN17-0458 CJun 22, 2007 · N286FE · Boeing 727233 · Fuselage Main, StructureSDR 07FDEA02257Door Frame · corrodedHIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, 2ND FRAME, 4" FROM AFT EDGE UPPER SURFACE OF LOWER FRAME, SHEAR TIE IS CORRODED. [07-26-07] BLENDED OUT DAMAGE. ORIGINAL MATERIAL IS .050", REMOVED .005", REMAINING MATERIAL IS .045". CHECKED MATERIAL LOSS Jun 22, 2007 · N286FE · Boeing 727233 · Service DoorsSDR 07FDEA02256Door Frame · corrodedHIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, 2ND FRAME, 4" FROM FWD EDGE UPPER SURFACE OF LOWER SHEAR TIE IS CORRODED. THIS SDR IS A DUPLICATE OF SDR NR 07-2257 AND INADVERTENTLY ENTERED IN ERROR. SDR SUBMITTED IN ERROR- ADMINISTRATOR.Jun 22, 2007 · N286FE · Boeing 727233 · Fuselage Main, StructureSDR 07FDEA02253Floorbeam · corrodedCABIN FLOOR PANEL SUPPORT AT BS 418 HAS CORROSION ON UPPER SURFACE BETWEEN RBL 13 AND RBL 23. REMOVED AND REPLACED SUPPORT REF SRM 51-30-02.Jun 22, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02252Skin · corrodedFWD LOWER FUSELAGE BELLY SKIN, BS 680 TO 740 STR 26L TO S-26R NEEDS TO BE REPLACED DUE TO MULTIPLE AREAS OF CORROSION AND DAMAGES. [08-29-07] BELLY SKIN AT STA. 680 TO 740, BETWEEN STR 26L TO 26R, WAS REMOVED. NEW SKIN WAS DRILLED UP TO MATCH EXISTING STJun 21, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02251Floor Support · corrodedAFT PIT STR CLIP FLOOR SUPPORT ANGLE CORRODED STR 29L, STA 970 REMOVED FLOOR SUPPORT, ORDERED NEW FLOOR SUPPORT, FABRICATED SHIM AND DRILLED UP NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT AND SHIM REF SRM 51-30-2 PG 3, 5-7, SRM 51-10-2 PG 1, SRM 51-20-1 FIG 10Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02248Frame · corrodedAFT PIT SHEAR TIE CORRODED STA 970 BETWEEN STRINGER 28-29L REMOVED SHEAR TIE, REMOVED CORROSION ON SIDE OF FRAME. CUT SHEAR TIE FROM FRAME. FABRICATED SHEAR TIE REPAIR FROM 7075-0 .071, HEAT TREATED TO T-6 CONDITION ON SNRM NR N01032, 8130 TRACKING NR 2007-Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02245Shear Tie · corrodedAFT PIT SHEAR TIE CORRODED STA 950F STR 25L-29L. REMOVED SHEAR TIE, REMOVED CORROSION ON SIDE OF FRAME. CUT SHEAR TIE FROM FRAME. FABRICATED SHEAR TIE REPAIR FROM 7075-0 .071" SENT TO HEAT TREAT ON SNRM NR N00976 FORM 8130 TRACKING NR 2007-05-157 TO T-6. DJun 21, 2007 · N286FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA02244Floor Support · corrodedUPPER MAIN DECK FLOOR SUPPORT STRUCTURE, INTERCOSTAL LWR STRAP HAS CORROSION (VIEW FROM PIT) FROM STA 1115 TO 1130, RBL 46. REMOVED CORROSION AT STA 1115 TO 1130 RBL 46, IAW B727 SRM 51-10-6. 100 PERCENT MATERIAL LOSS, OUT OF LIMITS. REMOVED DAMAGED SECTIOJun 21, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02243Floor Support · corrodedAFT PIT STRINGER CLIP FLOOR SUPPORT ANGLE CORRODED STA 950F, STR 29L REMOVED FLOOR SUPPORT, ORDERED NEW FLOOR SUPPORT. FABRICATED SHIM AND DRILLED UP. INSTALLED NEW FLOOR SUPPORT AND SHIM REF SRM 51-30-2 PG 3, 5-7, SRM 51-10--2 PG 1, SRM 51-20-1, FIG 10.Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02242Floor Support · corrodedAFT PIT STR CLIP/FLOOR SUPPORT ANGLE CORRODED AT STA 990 STR 29L REMOVED CORRODED STIFFENER REF SRM 51-30-2. REMOVED CORROSION FROM STIFFENER REF SRM 51-10-01 PG 14-16. FABED FILLER FROM 7075-T6- .071. TREATED AND PRIMED STIFFENER AND FILLLER REF MM 51-2Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02241Seat Track · corrodedAFT UPPER MAIN DECK, CORROSION ON SEAT TRACK LWR O/B UPPER SURFACE STA 950 LBL 26K. REMOVED CORROSION REF SRM 51-10-1, VERIFIED REMAINING MATERIAL WITHIN LIMITS REF SRM 53-10-1 FIG 3. TREATED AND PRIMED REF MM 51-20-002-7.Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02240Seat Track · corrodedAFT UPPER MAIN DECK, SEAT TRACK HAS CORROSION, ON UPPER INBD FLANGE, STA 1070 2 LBL 45. REMOVED CORROSION ORIG THICKNESS .530. REMOVED .036, REMAINING .494" MATERIAL. REMOVED IS WITHIN LIMITS. TREATED AND APPLIED PRIMER REF SRM 53-10-1 PG 13-17.Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02239Stringer Clip · gougedMAIN CABIN, STRINGER CLIP GOUGED IN RADIUS AT STA 680 AT STR 7L REPLACED DAMAGED STRINGER CLIP AT BS 680 STR 7L REF SRM 51-30-2 PG 1&2.Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02238Attach Angle · crackedRT WING O/B T/E UPPER SURFACE PANEL JUST INBD OF AILERON, JACKSCREW FAIRING ATTACH ANGLE CRACKED INSIDE FAIRING. REMOVED DAMAGED ANGLE, DRILLED UP, PRIMED AND PAINTED NEW ANGLE ON PANEL INBD OF AILERON, REF SRM 51-30-2.Jun 21, 2007 · N286FE · Boeing 727233 · Wing, Attach FittingsSDR 07FDEA02237Seat Track · corrodedRBL SEAT TRACK HAS CORROSION BETWEEN UPPER CHANNEL AND LWR MOUNT FLANGE STA 783-849. REMOVED CORROSION REF SRM 53-10-1 FIG 3 SHT 5. .015" MAT. REMOVED. OUT OF LIMITS REF SRM 53-10-1 FIG 3. REMOVED FLOORBEAM AND SEAT TRACK BS 740 TO 850 RBL 45. FABRICATED NJun 21, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02236Structure · corrodedLWR FWD CARGO PIT, CORROSION ON LT AND RT SIDES AT MOUNTING HOLES, FWD OF WORK PLATFORM THATS AT STA 720D TO 720E. ACCOMPLISHED 2 TYPICAL FORMED REPAIRS AT STA 720D AND STA 720E LOWER CARGO PIT WORK PLATFORM PANEL REF SRM 51-40-3 PG 1-6.Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02235Floorbeam · crackedFWD PIT FLOOR SUPPORT STIFFENER STA 580, RBL 9, IS CRACKED REMOVED AND REPLACED STIFFENER AT STA 580 RBL 9, IAW B727 SRM 51-30-2.Jun 21, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02228Skin · misrepairedON AGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT LT WING I/B AFT FLAP UPPER SURFACE 30" FROM O/B END, 9" FROM T/E DID NOT CONFORM TO SRM 51-40-20. REMOVED PREVIOUS REPAIR AND BONDED ON REPAIR REF SRM 51-40-20 PARAGRAPHS, 7, 14, 18, 20, 21, AND 22. TJun 20, 2007 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA02227Flap Track · crackedNR 5 FLAP TRACK FAIRING INBD MIDDLE ATTACH BRACKET IS CRACKED. THIS SDR WAS ENTERED IN ERROR. THIS IS A DUPLICATE OF TRACKING NR 07-2224 KEEP NR 07-2224 AS ORIGINAL AND ACTIVE. THIS SDR WAS SUBMITTED IN ERROR- ADMINISTRATOR.Jun 20, 2007 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA02226Skin · misrepairedAGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT LT WING AFT FLAP UPPER SURFACE 18" FROM I/B END 12" FROM T/E DID NOT CONFORM TO SRM 51-40-20 PARA 7. REMOVED PREVIOUS REPAIR AND BONDED ON NEW REPAIR REF SRM 51-40-20 PARAGRAGHS 7, 14, 15, 18, 20, 21, ANDJun 20, 2007 · N286FE · Boeing 727233 · Trailing Edge Flaps
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