Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  ORDER BY difficulty_date DESC"

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SDR 04FDEA01059Beam · corrodedCORROSION STA 760 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS BS 760 DELTA BEAM LWR ANGLE. REMOVED AND INSTALLED NEW BS 760 DELTA BEAM LWR ANGLE IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5.Apr 22, 2004 · N243FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA01058Beam · corrodedCORROSION STA 780 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS BS 780 DELTA BEAM LWR ANGLE. ACCESS LWR WEB. REMOVED, INSTALLED NEW BS 780 DELTA BEAM LWR ANGLE AND INSTALLED LWR WEB SUPPORT BEACON PANEL IAW SRM 51-30-2, 51Apr 22, 2004 · N243FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA01057Skin · chafedEXTERNAL FUSELAGE SKIN CHAFE DAMAGED UNDER FAIRING CONTACT AREA, BS 950D 15 - 990, STR 23L - 26L. SKIN CHAFE FOUND OUT OF LIMITS BS 973-989 IAW SRM 53-30-1. REPAIRED SKIN IAW SRM 53-30-3 FIG 3. BLEND OUT FROM 950D 15 - 950E 12, AND 950E 18 TO 973 FOUND TO BApr 22, 2004 · N243FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA01056Skin · dentedLWR FUSELAGE SKIN DENTED BS 1125 BELOW LAP AT STR 20L. DENT ON SKIN AT BS 1125 BELOW LAP AT STR 20L WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER SRM 53-30-3 FIG 5.Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA01055Frame · gougedFRAME GOUGED AT STR 22L BS 520. FOUND GOUGE ON FRAME AT BS 520 STR 22 LT TO .023 INCH DEEP. FRAME THICKNESS IS .050 OUT OF LIMITS. REMOVED FRAME SECTION FROM STR 21L - 25L, BS 520. INSTALLED NEW FRAME IAW SRM 53-10-1/SRM 51-30-2/SRM 51-30-5.Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01054Skin · dentedFUSELAGE SKIN DENTED AT BS 1080 STR 7R. FUSELAGE SKIN DENT AT BS 1080 STR 7R FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3.Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA001059Beam · corrodedCORROSION STA 760 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS BS 760 DELTA BEAM LWR ANGLE. REMOVED AND INSTALLED NEW B S760 DELTA BEAM LWR ANGLE IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5.Apr 22, 2004 · N243FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA001058Beam · corrodedCORROSION STA 780 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS BS 780 DELTA BEAM LWR ANGLE. ACCESS LWR WEB. REMOVED, INSTALLED NEW BS 780 DELTA BEAM LWR ANGLE AND INSTALLED LWR WEB SUPPORT BEACON PANEL IAW SRM 51-30-2, 51Apr 22, 2004 · N243FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA001057Skin · damagedEXTERNAL FUSELAGE SKIN CHAFE DAMAGED UNDER FAIRING CONTACT AREA, BS 950D 15 - 990, STR 23L - 26L. SKIN CHAFE FOUND OUT OF LIMITS BS 973-989 IAW SRM 53-30-1. REPAIRED SKIN IAW SRM 53- 30-3 FIG 3. BLEND OUT FROM 950D 15 - 950E 12, AND 950E 18 TO 973 FOUApr 22, 2004 · N243FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA001056Skin · dentedLWR FUSELAGE SKIN DENTED BS 1125 BELOW LAP AT STR 20L. DENT ON SKIN AT BS 1125 BELOW LAP AT STR 20L WAS FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE & REPAIRED SKIN PER SRM 53-30-3 FIG 5.Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA001055Frame · gougedFRAME GOUGED AT STR 22L BS 520. FOUND GOUGE ON FRAME AT BS 520 STR 22 LT TO .023 INCHES DEEP. FRAME THICKNESS IS .050 OUT OF LIMITS. REMOVED FRAME SECTION FROM STR 21L - 25L, BS 520. ISNTALLED NEW FRAME IAW SRM 53-10-1/SRM 51-30-2/SRM 51-30-5.Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA001054Skin · dentedFUSELAGE SKIN DENTED AT BS 1080 STR 7R. FUSELAGE SKIN DENT AT BS 1080 STR 7R FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3.Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA01013Skin · chafedSKIN CHAFE DAMAGE FOUND AT BS 950E 12 TO 950E 19 BETWEEN STR 25L TO STR 26L. SKIN CHAFE FOUND TO BE OUT OF LIMITS FROM BS 950E 12 - 950E 19. REPAIRED DAMAGED SKIN FROM 950E 12 TO 950E 19 BETWEEN STR 25L TO 26L PER SRM 53-30-3 FIG 1.Apr 21, 2004 · N243FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA01016Seat Track · gougedMAIN CARGO COMPT. SEAT TRACK HAS GOUGED SCALLOPS AT FS 755 - 765, LBL 63. REMOVED AND REPLACED SEAT TRACK SECTION AT F/S 755-765, LBL 63, IAW SRM 51-30-2.Apr 21, 2004 · N206FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA001016Cargo Track · gougedMAIN CARGO COMPT CARGO TRACK HAS GOUGED SCALLOPS AT FS 755 - 765 LBL 63. REMOVED AND REPLACED CARGO TRACK SECTION AT FS 755 - 765 LBL 63, IAW SRM 51-30-2 AT MAE.Apr 21, 2004 · N206FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA001013Skin · chafedSKIN CHAFE DAMAGE FOUND AT BS 950E 12 TO 950E 19 BETWEEN STR 25L TO STR 26L. SKIN CHAFE FOUND TO BE OUT OF LIMITS FROM BS 950E 12 - 950E 19. REPAIRED DAMAGED SKIN FROM 950E 12 TO 950E 19 BETWEEN STR 25L TO 26L PER SRM 53-30-3 FIG 1.Apr 21, 2004 · N243FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA01001Web · corrodedCENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE.Apr 17, 2004 · N279FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA001000Bracket · crackedNR 8 SPOILER INBOARD STOP BRACKET LWR MOUNTING CRACKED. REMOVED AND REPLACED STOP BRACKET IAW SRM 51-30-2 AT MAE.Apr 17, 2004 · N279FE · Boeing 727200 · SpoilersSDR 04FDEA001003Frame · damagedCOMPLY WITH EA 7-5310-77343; FUSELAGE MAIN FRAME MISDRILLED HOLE REPAIR BS 336.0, RBL 6.5 WL 153. COMPLIED WITH EA 7-5310-77343 FUSELAGE MAIN FRAME MISDRILLED HOLE REPAIR BS 336.0 RBL 6.5 WL 153 AT MAE.Apr 17, 2004 · N206FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA001001Floor Panel · corrodedCENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE.Apr 17, 2004 · N279FE · Boeing 727200 · Fuselage Floor PanelSDR 04FDEA00986Support · crackedNR 2 RIGHT AFT COWL ENGINE DRAIN LINE SUPPORT CRACKED. FABRICATED DRAIN LINE SUPPORT FROM 2024-T3 .032C BATCH 715298 AND INSTALLED IAW SRM 51-30-2 AT MAE.Apr 17, 2004 · N206FE · Boeing 727200 · Nacelle/Pylon, Main FrameSDR 04FDEA00985Bracket · chafedNR 2 ENG RIGHT AFT COWL OVERBOARD DRAIN SUPPORT BRACKET & RIVET CHAFED. FABRICATED NEW SUPPORT BRACKET USING 2024-T3 .050C BATCH 742514 AND INSTALLED IAW SRM 51-30-2 AT MAE.Apr 16, 2004 · N206FE · Boeing 727200 · Nacelle/Pylon Miscellaneous StructureSDR 04FDEA00984Strip · tornPANEL 5531 CHAFE STRIP IS TORN. REMOVED AND REPLACED STRIP IAW SRM 51-30-2 AT MAE. FABBED FROM 301-25 .012SS BATCH 000705488.Apr 16, 2004 · N206FE · Boeing 727200 · Nacelle/Pylon, Main FrameSDR 04FDEA00981Skin · bulgedUPPER FUSELAGE SKIN BULGE AT BS 380 BETWEEN STR 17L AND STR 18L. FOUND BULGE IN SKIN, BS 380 BETWEEN STR 17L & 18L, TO BE CREASED AND OUT OF LIMITS IAW SRM 53-30-1.CUT OUT DAMAGED SKIN 2 X 6 AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3.Apr 16, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00980Web · crackedSHEAR WEB CRACKED, AT BS 380-400, LBL 65, WL 208. REMOVED CRACKED SHEAR WEB BS 380-400, LBL 65, WL 208. FABRICATED NEW WEB AND INSTALLED IAW SRM 51-30-5, SRM 51-30-2 AND FED EX MM 51-20-151.Apr 16, 2004 · N283FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA00979Stringer · crackedSTR 17L IS CRACKED AT BS 385 LBL 65 WL 208. CUT AND REMOVED STR AND INSTALLED REPAIR AT BS 370 TO BS 407, STR 17L, WL 208 IAW SRM 51-40-4.Apr 16, 2004 · N283FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA00967Floorbeam · corrodedMAIN CARGO COMPARTMENT CORROSION ON FLOORBEAM BS 344 WL 208 BL 0 TO LBL 45. REMOVED CORROSION ON FLOORBEAM STA 344, LBL 38, 2 X 8 X .020 FOUND OUT OF LIMITS IAW SRM 51-10-1. REMOVED AND FABRICATED NEW FLOOR BEAM BS 344, WL 208, RBL 6 TO LBL 65 (SKIN) BAC 1505Apr 15, 2004 · N243FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00966Shear Tie · corrodedCORROSION (C53-111-01, 3) ON SHEAR TIE BS 950E LBL 18 WL 141. CORROSION OUT OF LIMITS. REPAIRED SHEAR TIE BS 950E, LBL 18, WL 141 PER SRM 53-10-4 FIG 15 AND EA 7-5310-55285.Apr 15, 2004 · N243FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00959Floorbeam · corrodedCORROSION (C53-111-01) AFT CARGO BAY, FLOORBEAM HAS CORROSION LWR FLANGE BS 1148, WL 200, LBL 20 TO LBL 29. *S/D* CORROSION ON AFT CARGO BAY FLOORBEAM LWR FLANGE BS 1148, WL 200, LBL 20 TO LBL 29 FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR ANGLES AND FILLERApr 14, 2004 · N243FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00958Trunnion · corrodedCORROSION ON RIGHT TRUNNION UPPER TEE CHORD FWD UNDERSIDE, STA 295 WL 169 RBL 15. CORROSON ON NLG RT TRUNNION UPPER TEE CHORD STA 295, WL 169, RBL 15 FOUND TO BE OUT OF LIMITS. REPLACED CORRODED TEE CHORD AND INSTALLED NEW TEE CHORD PER 727 SRM 53-10-1, 51-30Apr 14, 2004 · N243FE · Boeing 727200 · Fuselage Main, StructureSDR P9RA20040012Slide · leakingSLIDE REMOVED FOR SCHEDULED CHANGE. REPAIR STATION TEARDOWN INDICATED THE INFLATABLE TUBE IS POROUS AND WILL NOT PASS TEST. UNIT IS NOT REPAIRABLE. LAST OVERHAUL WAS MAY 31 2001.Apr 13, 2004 · N288SC · Boeing 727200 · Escape SlideSDR 04FDEA00885Charger · overheatedTHE BATTERY CHARGER STARTED TO SMOKE AND THE BATTERY GOT VERY HOT 170 DEGREES. THE AIRCRAFT WAS IN THE HANGAR HAVING AN ALL LANDING GEAR CHANGE AND ON JACKS.Apr 8, 2004 · N236FE · Boeing 727200 · Battery/Charger SystemSDR 04FDEA00849Duct · crackedCOMPLY WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR. COMPLIED WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR AT MAE.Apr 7, 2004 · N279FE · Boeing 727200 · Engine Exhaust SystemSDR 04FDEA00822Flap Track · brokenOUTBOARD FLAPS STAYED AT 2 DEG WHEN FLAP HANDLE PUT TO 5 DEG. RAN QRH. LANDED UNEVENTFULLY. DECLARED AN EMERGENCY. IN WORK. RAN FLAPS TO 25 DEG. UPON VISUAL INSPECTION FOUND RIGHT OUTBD FOREFLAP BROKEN OFF OF FLAP TRACKS. EVALUATING DAMAGE AND PARTS ATApr 3, 2004 · N211FE · Boeing 727200 · Trailing Edge FlapsSDR 04FDEA00817Skin · crackedFUSELAGE SKIN IS CRACKED AND EXFOLIATED AT BS 1060, STR 30. COMPLIED WITH FED EX EA 7-533070651 ON THE CRACKED AND EXFOLIATED SKIN AT BS 1060 STR 30.Apr 1, 2004 · N285FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00815Skin · gougedFUSELAGE SKIN IS GOUGED AT BS 1005 BETWEEN STR 25R AND 26R. GOUGE IN SKIN AT BS 1005, STR 25R & 26R WAS FOUND TO BE OUT OF LIMITS. REPAIRED SKIN PER FED EX EA 7-5330-76233.Apr 1, 2004 · N282FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00814Skin · corrodedCORROSION LT WING UPPER SKIN T/E SPAR AREA 8 INCHES FROM WING TO BODY FAIRING UPPER SURFACE OF SKIN. BLENDED CORROSION LT WING UPPER SKIN T/E SPARE 8 INCHES FROM WING TO BODY FAIRING. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA 1.25 X 1 INCH AND REPAIRED IAW Apr 1, 2004 · N282FE · Boeing 727200 · Wing, Plate/SkinSDR 04FDEA00782Fitting · crackedLEFT WING INBOARD AILERON HINGE FITTING AND WEB IS CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-1, REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-10-1 AND BOEING DWG 65-21709.Mar 31, 2004 · N280FE · Boeing 727200 · AileronsSDR 04FDEA00775Shear Tie · corrodedCORROSION WHILE WORKING N00607 FOUND CORROSION AT BS 1148 WL 153 ON SHEAR TIE. COMPLIED WITH FED EX EA 7-5310-55267 ON SHEAR TIE THAT WAS CORRODED AT BS 1148 WL 153.Mar 30, 2004 · N285FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00774Stringer · corrodedCORROSION WHILE WORKING N00607 FOUND CORROSION AT BS 1142-1148 WL 152 ON STR 30. *S/D* COMPLIED WITH FED EX EA 7-5330-70652 ON CORRODED STRINGER AT BS 1142-1148 WL 152 ON STR 30.Mar 30, 2004 · N285FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA00773Shear Tie · corrodedCORROSION ON SHEAR TIE, IN AFT CARGO BAY, BS 1148, WL 149, LBL 9. *S/D* COMPLIED WITH FED EX EA 7-5310-55267 ON SHEAR TIE THAT WAS CORRODED AT BS 1148 WL 149 LBL 9.Mar 30, 2004 · N285FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00772Intercostal · corrodedCORROSION WHILE WORKING N00402 FOUND INTERCOSTAL CORRODED AT BL 0 BS 1130-1148. *S/D* CORROSION ON INTERCOSTAL FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-20-1, 51-10-2, 51-30-2.Mar 30, 2004 · N285FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA00764Hinge · gougedMAIN CARGO DOOR, DOOR HINGE LUG MINOR GOUGE REPAIR BS 616.5. COMPLIED WITH EA 7-5230-75124 DOOR - MAIN CARGO DOOR DOOR HINGE LUG MINOR GOUGE REPAIR FS 616.5 AT MAE.Mar 27, 2004 · N280FE · Boeing 727200 · Cargo/Baggage DoorsSDR 04FDEA00762Control Box · inoperativeMAIN GEAR ANTI SKID OUTBOARD INOP & INBD INOP LIGHTS INTERMITTEN ON TAKEOFF ROLL WITH NO BRAKES APPLIED. REMOVED AND REPLACED ANTI SKID CONTROL BOX, OPS CHECK AND SELF TEST GOOD AT THIS TIME IAW 727 MM 32-42-001-5.Mar 27, 2004 · N258FE · Boeing 727200 · Brake Anti-Skid SectionSDR 04FDEA00754Skin · corrodedFOUND CORROSION AT BS 1142-1148 WL 152 BL 0 ON INNER SKIN. *S/D* REMOVED CORROSION ON INNER SKIN AT BS 1139-1164 LBL 1 TO LBL 2 AT WL 152. FOUND TO BE IN LIMITS. DEEPEST BLEND WAS .012 ORIGINAL THICKNESS IS .140. ALODINED, PRIMED AND PAINTED PER 727 SRM 5Mar 25, 2004 · N285FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00737Skin · dentedDENT IN EXTERNAL SKIN OF NR 2 ENG INLET 12 INCHES FROM L/E AT 9 O'CLOCK POSITION. DENT IN EXTERNAL SKIN OF NR 2 ENGINE INLET 12 INCHES FROM L/E AT 9 O'CLOCK POSITION AREA 1.5 X .090 INCH DEEP A/Y=16.6, FOUND OUT OF LIMITS PER SRM 54-30-01. REPAIRED DENT PER Mar 23, 2004 · N282FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00733Skin · gougedLEFT AFT EMERGENCY EXIT DOOR EXTERNAL SKIN IS GOUGED AT LWR AFT CORNER. REMOVED DAMAGE AREA OF LEFT AFT EMERGENCY EXIT DOOR SKIN. FABRICATED REPAIR, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR AS PER SRM 52-00-2 AND INSTALLED ALL FASTENERS REMOVED FOR ACCMar 23, 2004 · N282FE · Boeing 727200 · Emergency ExitsSDR 04FDEA00736Spar · chafedVERTICAL STAB MID SPAR CHAFED AT PANEL 9601 (LT SIDE). REPAIRED DAMAGED AREA ON VERTICAL STAB MID SPAR BEHIND PANEL 9601 PER FED EX EA 7-5530-76229 AND SRM 55-30-6 FIG 3.Mar 23, 2004 · N282FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 04FDEA00735Spar · chafedVERTICAL STAB MID SPAR CHAFED AT PANEL 9602 (RT SIDE). REPAIRED THE RT VERTICAL MID SPAR AT PANEL 9602 IAW FED EX EA 7-5530-76229 AND SRM 55-30-6 FIG 3.Mar 23, 2004 · N282FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 04FDEA00734Shear Tie · corrodedCORROSION ON STUB FRAME SHEAR TIE STA 950E 4 BETWEEN STR 28R AND 29R.Mar 23, 2004 · N282FE · Boeing 727200 · Fuselage Main, Structure
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