Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  ORDER BY difficulty_date DESC"

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SDR I5EA20111105Support Fitting · corrodedDURING HFEC INSPECTION OF THE SIDE ENGINE FWD MOUNT SUPPORT FITTING FASTENER INSPECTION REQUIRED BY SB 727-54A0010. SURFACE CORROSION WAS FOUND. INFORMATION HAS BEEN SUBMITTED TO ENGINEERING FOR REVIEW AND DISPOSITION.Nov 10, 2011 · N727NY · Boeing 727232 · Engine Mount SectionSDR I5EA20111104Skin Panel · crackedHFEC INDICATES CRACK IN SCRIBE LINE LOCATED AT BS 693 - 695, S14R. INFORMATION HAS BEEN SUBMITTED TO ENGINEERING FOR REVIEW AND DISPOSITION.Nov 10, 2011 · N727NY · Boeing 727232 · Fuselage Main, Plate/SkinSDR I5EA20111103Skin Panel · crackedCRACK FOUND IN FUSELAGE SKIN (HFEC VERIFIED) .40" LONG EXTENDING UNDER BUTT JOINT AT BS 481, S14L. INFORMATION HAS BEEN SUBMITTED TO ENGINEERING FOR REVIEW AND DISPOSITION.Nov 10, 2011 · N727NY · Boeing 727232 · Fuselage Main, Plate/SkinSDR I5EA20111102Skin Panel · crackedHFEC INDICATES CRACK IN SCRIBE LINE LOCATED AT BS 439 - 465, S14R. INFORMATION HAS BEEN SUBMITTED TO ENGINEERING FOR REVIEW AND DISPOSITION.Nov 10, 2011 · N727NY · Boeing 727232 · Fuselage Main, Plate/SkinSDR FOTR2011100406432Frame · corrodedSURFACE CORROSION AT BS 727, FRAME LBL 5 TO RBL 5 , AFT SIDE, LWR AFT CARGO. REPAIRED ON FASI WO 21142, NR 06432.Oct 4, 2011 · N498DA · Boeing 727232 · Fuselage Main, FrameSDR FDEA201108103183Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE STA 720 TO 720E, 10" BL 0. REMOVED SEAT TRACK SECTION STA 720 TO STA 740 BL 0, IAW SRM 51-30-2. FABRICATED SEAT TRACK SECTION, IAW SRM 53-10-2, FIG 7A, INSTALLED SEAT TRACK SECTION, IAW SRM 51-30-2.Aug 10, 2011 · N236FE · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR I5EA20110505Battery Pack · dischargedEMERGENCY LIGHTS INOP.May 10, 2011 · N727NY · Boeing 727232 · Emergency LightingSDR I5EA20110504Battery Pack · dischargedEMERGENCY LIGHTS INOP.May 10, 2011 · N727NY · Boeing 727232 · Emergency LightingSDR I5EA20110512Structure · corrodedCORROSION AROUND FASTENER HEAD AT STATION 312 BETWEEN STRINGER 22R AND STRINGER 23R.May 8, 2011 · N727NY · Boeing 727232 · Fuselage Miscellaneous StructureSDR NACA20110021Skin · crackedCRACK IN FUSELAGE SKIN AT STA 727B - 733, STR 181L. REPAIRED CRACK IN FUSELAGE AT STA 727B-733 IAW B737-200 SRM 53-30-3 FIG 48, DETAIL XI.Jan 18, 2011 · N321DL · Boeing 727232 · Fuselage Main, Plate/SkinSDR I5EA20101007Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.Oct 26, 2010 · N727NY · Boeing 727232 · Emergency LightingSDR I5EA20101006Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.Oct 26, 2010 · N727NY · Boeing 727232 · Emergency LightingSDR I5EA20101005Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.Oct 26, 2010 · N727NY · Boeing 727232 · Emergency LightingSDR I5EA20101004Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.Oct 26, 2010 · N727NY · Boeing 727232 · Emergency LightingSDR I5EA20101003Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.Oct 26, 2010 · N727NY · Boeing 727232 · Emergency LightingSDR I5EA20101002Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.Oct 26, 2010 · N727NY · Boeing 727232 · Emergency LightingSDR I5EA20101001Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.Oct 26, 2010 · N727NY · Boeing 727232 · Emergency LightingSDR FDEA201010013850Connector · failed30 SECONDS AFTER TAKE OFF CARGO SMOKE WARNING OCCURED. BELLS AND LIGHTS FOR ABOUT 3 SECONDS THEN WENT OUT. 10 SECONDS LATER WARNING OCCURED AGAIN AND LASTED FOR ABOUT 10 SECONDS AND THEN STOPPED AGAIN. REINSTALLED CONNECTOR PLUGS ON NR 1 AND NR 2 LWR CARGOct 1, 2010 · N498FE · Boeing 727232 · Fire Protection System WiringSDR FDEA201009243702Fire Detector · false activationON TAKEOFF APPROX 1000' AGL GOT AN INTERMITTENT FIREBELL AND S/O SAW CARGO SMOKE WARNING LOWER FWD CARGO ON, THEN THE LIGHT WENT OUT. AML REFLECTED A PREVIOUS WRITEUP ON THE SAME SYS. DEEMED TO RETURN AND LAND IMMEDIATELY. REMOVED SMOKE DETECTORS 1,2,3, &Sep 24, 2010 · N498FE · Boeing 727232 · Fire DetectionSDR FDEA200907252750Connector · shortedDURING CLIMB, ACFT CABIN ACT WAS TOO HIGH. FOUND PACK VALVE C/B POPPED. CABIN ALT STABILIZED AT 8500' AT 20,000 WITH L AFT PACK OPERATING ONLY. TROUBLESHOT SYS, FOUND PACK VALVE BREAKER WOULD RESET MOMENTARILY. CHECKED BOTH FWD PACK SHUTOFF VALVES NO DEFEJul 25, 2009 · N498FE · Boeing 727232 · Air Conditioning System WiringSDR RYN2008F00024Structure · corrodedLT HARD AFT OVERWING ESCAPE HATCH CUTOUT LOWER SECTION HAVE CORROSION. REPAIRED LT AFT OVERWING ESCAPE HATCH CUTOUT BY FABRICATING AND INSTALLING A DOUBLER IAW SRM 53-30-3. (K)Oct 1, 2008 · N727NY · Boeing 727232 · Emergency ExitsSDR RYN2008F00023Structure · corrodedRT HORIZONTAL STABILIZER TRAILING EDGE UPPER CHORD HAS CORROSION AT STABILIZER STA 189.68. REPLACED UPPER CHORD AT RT HORIZONTAL STABILIZER TRAILING EDGE IAW SRM 51-10-1 AND 51-30-3. (K)Oct 1, 2008 · N727NY · Boeing 727232 · Horizontal Stabilizer StructureSDR RYN2008F00022Nose Cowl · dentedNR 3 ENGINE NOSE COWL HAS DENT AT 5 OCLOCK POSITION, LEADING EDGE. REMOVED DENTED AREA AND ACCOMPLISHED NOSE COWL LEADING EDGE LIP SKIN REPAIR IAW SRM 54-30-1, 54-30-3, AND 51-30-2, 51-20-00, 51-31-00. (K)Oct 1, 2008 · N727NY · Boeing 727232 · Nacelle/Pylon, Main FrameSDR 08FDEA02845Stringer · crackedRT WING, STR 10 CRACKED AT WS 656.5, ITEM IS AD DRIVEN, IF CRACKS EXCEED LIMITS IN SECTION II, FIG 12, CONTACT FED EX STRUCTURES ENGINEERING FOR REPAIR INSTRUCTIONS PER WORK CARD E7-5710-7-4322. STOP DRILLED CRACK, VERIFIED CRACK TERMINATION AT STOP DRILL, LOJul 12, 2008 · N497FE · Boeing 727232 · Wing, Longeron/StringerSDR 08FDEA01789Stringer Clip · crackedORIGINAL LOST, A86-143 REF AD 92-12-03, AFT PIT BILGE BODY FRAME STR CLIP IS BUCKLED, CRACKED, CORRODED BS 950F, STR 27L (EO 7-5310-7-2354) N00252. REMOVED AND REPLACED STR CLIP AT AFT PIT BILGE BODY FRAME STR 27L, STA 950F, REF SRM 51-30-2 PG 2-4 . THIS IS May 7, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach FittingsSDR 08FDEA01746Fairing · crackedLEFT WING INBOARD MID FLAP OUTBOARD JACK SCREW FAIRING INTERIOR SKIN CRACKED AT ATTACH HOLE REPAIRED LEFT WING INBD MID FLAP O/B JACK SCREW FAIRING REF SRM 57-20-4 PG 5 AND SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR.May 3, 2008 · N498FE · Boeing 727232 · Trailing Edge FlapsSDR 08FDEA01713Stringer Splice · corrodedFWD PIT STRINGER SPLICE AT 27L GOING THROUGH STA 680 CORRODED ON OUTBD SIDE REMOVED CORROSION FROM ORIGINAL THICKNESS OF 0.064 INCH FROM BUTT SPLICE STRAP WITH 0.054" REMAINING. OUT-OF-LIMITS DUE TO "NO REWORK PERMITTED IN BUTT SPLICE STRAP". FABRICATED REPAMay 1, 2008 · N498FE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR 08FDEA01705Stop Fitting · gougedAFT LOWER NR 3 CARGO DOOR FORWARD FRAME LOWER STOP FITTING GOUGED. DOOR REMOVED REF AMM 52-35-071-4, LWR FORWARD FITTING REMOVED AND INSTALLED REF SRM 51-30-02. DOOR INSTALLED REF AMM 52-35-071, ADJUSTED STOPS. THIS IS CLASSIFIED AS A MAJOR REPAIR.Apr 30, 2008 · N498FE · Boeing 727232 · Cargo/Baggage DoorsSDR 08FDEA01704Rib · crackedRT HORIZONTAL STAB, AFT SUPPORT RIB IS CRACKED NEAR ELEVATOR ATTACH POINT, ELEVATOR STA 99.79 REMOVED WIPER PLATES, REF SRM 51-30-2. FAB RADIUS FILLER FOR REPAIR, .100" 2024-T3 REF DWG 69-33174. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR REF SRM 5Apr 30, 2008 · N498FE · Boeing 727232 · Horizontal Stabilizer, Spar/RibSDR 08FDEA01700Skin · crackedMAIN DECK 1R DOOR EXT SKIN IS BUCKLED/CRACKED AT UPPER HINGE CUT OUT UPPER EDGE, 4 INCHES FROM FWD END. REMOVED DAMAGE AND CHECKED WITH HFEC, NO DEFECTS FOUND. REMOVED LINER SUPPORT, VERIFIED MATERIAL, MADE A .040 INSURANCE CUT REF SRM 52-00-3 FIG 3 STEP 2. Apr 30, 2008 · N498FE · Boeing 727232 · Passenger/Crew DoorsSDR 08FDEA01697Web · corrodedCORROSION ON WEB TO BODY SKIN ON ANGLE ON WEB BETWEEN BS 950A TO 950B, LBL 18, WL 141 REPLACED WEB AT STA 950 - 950B, LBL AND CLIP AT STA 950A LBL 18 REF BOEING DWG 69-44877 AND SRM 51-30-3. THIS IS CLASSIFIED AS A MINOR REPAIR.Apr 30, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 08FDEA01696Panel · delaminatedRIGHT WING L/E LWR PANEL 6402 HAS 2 INCH BY 6 INCH AREA OF DISBOND CORE FROM INNER AND OUTER SURFACES. REPAIRED PANEL 6402 REF SRM 51-40-9 PARAGRAPHS 3D, 4B, 4E, 4F AND AMM 51-20-051-7, 51-20-151-7 TAP TEST GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR.Apr 30, 2008 · N498FE · Boeing 727232 · Wing, Plate/SkinSDR 08FDEA01695Structure · crackedLWR EXT FUSE WING BODY FILLET FAIRING SUPPORT FRAME LWR CHORD ANGLE IS BUCKLED/CRACKED AT I/B END 950A, LBL 14. REPAIRED SUPPORT FRAME LOWER CHORD ANGLE FOR WING TO BODY FAIRING AT 950A, LBL 14 REF SRM 51-40-3. THIS IS CLASSIFIED AS A MINOR.Apr 30, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 08FDEA01496Skin · dentedRT ELEVATOR LWR SKIN HAS A DENT 97 INCHES FROM I/B EDGE, 7 INCHES FWD OF REAR SPAR. MEASURED DENT FOUND TO BE WITHIN LIMITS, MEASURED DENT Y = .040 A = 4 INCHES FOUND TO BE 100 REF SRM 55-10-1 PG 7 FIG 2. THIS IS CLASSIFIED AS A MINOR REPAIR.Apr 23, 2008 · N498FE · Boeing 727232 · Elevator, Plate/SkinSDR 08FDEA01495Skin · crackedMLG WW KEEL BEAM LWR EXT SKIN PANEL AT BS 940 TO 950-12, LBL 5-RBL 5 2 EA CRACKED FASTENER HOLES BS 947, RBL 5 (MKD). REMOVED DAMAGE AND FABRICATED A REPAIR FILLER AND A REPAIR DOUBLER. TREATED, PRIMED AND PAINTED ALL REPAIR PARTS AND INSTALLED. EDGE SEALEDApr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR 08FDEA01494Skin · corrodedMLG W/W KEEL BEAM LWR EXT SKIN PANEL AT BS 940 TO 950 PLUS 12, LBL 5- RBL 5 HAS SEVERAL AREAS OF CORROSION REMOVED AREAS OF CORROSION. REMOVED 0.005 INCH FROM ORIGINAL SKIN THICKNESS OF 0.071 INCH. 0.066 INCH REMAINING AND SKIN PANEL IS WITHIN LIMITS. TREApr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR 08FDEA01493Stringer Clip · corrodedSTRINGER TIE ON STR 26R AT FS 941A HAS CORROSION ON OUTER SIDE OF TIE. REMOVED DAMAGED STRINGER TIE REPLACED NEW STRINGER TIE, REF SRM 51-30-2 PG1. THIS IS CLASSIFIED AS A MAJOR REPAIR.Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach FittingsSDR 08FDEA01489Shear Tie · corrodedFWD PIT SHEAR TIE STA 520 BETWEEN STR 28L-28R CORRODED. REMOVED FASTENER'S TO ACCESS CORROSION IN REF TO SRM 51-30-2 PG 2. REMOVED CORROSION ON FWD SIDE OF SHEAR TIE BS 520 STR 28L-28R IN REF TO SRM 53-10-1. CHECK SHEAR TIE FOR MAT'L LOSS ORIGINAL THICKNEApr 23, 2008 · N498FE · Boeing 727232 · Fuselage Internal Mounting StructureSDR 08FDEA01488Structure · crackedNR 2 ENGINE LEFT FWD COWLING OUTER AFT CORNER MULTIPLE LAYERS OF SHEET METAL ARE CRACKED. REMOVED DAMAGED AREA REF SRM 51-40-2. MATERIAL ID AT 2024 T3 .080 REF SRM 65-10-3 A48140 FOR DOUBLER. MATERIAL ID AT 2024 T3 .100 A 11734 REF SRM 54-30-2 FOR FILLER. Apr 23, 2008 · N498FE · Boeing 727232 · Nacelle/Pylon, Plate/SkinSDR 08FDEA01485Bulkhead · corrodedBS 178 BULKHEAD EXT SURFACE WL 187 - 193 LBL 19" TO 24" HAS CORROSION PITS. CHEMICALLY REMOVED CORROSION FROM BS 178 BULKHEAD EXT SURFACE WL 185-193 LBL 19" TO 24". THICKNESS OF MATERIAL IS .055, MATERIAL REMAINING IS .053 A LOSS OF .022 FOUND TO BE WITH-IN LApr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, BulkheadSDR 08FDEA01484Angle · corrodedCORROSION ON WEB TO BODY SKIN ANGLE ON WEB BETWEEN BS 950A TO 950B, RBL 3, WL 139. REMOVED AND REPLACED INTERCOSTAL WEB AND AFT ATTACH CLIP REF 51-30-2 PG 8. THIS IS CLASSIFIED AS A MINOR REPAIR.Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 08FDEA01482Fitting · crackedMAIN DECK 1R DR BOTTOM CROSS BEAM AFT STOP FITTING IS CRACKED REMOVED AND REPLACED STOP FITTING REF SRM 51-30-2. DOOR ADJUSTEMENT ACCOMPLISED ON W/0 40304 N00067, THIS IS CLASSIFIED AS A MINOR REPAIR.Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach FittingsSDR 08FDEA01481Skin · gougedEXT FUSELAGE SKIN IS GOUGED AT BS 670 O/B OF STR S-28L REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR REF SRM-30-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR AND A CATEGORY "B" REPAIR.Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR 08FDEA01480Intercostal · crackedMAIN DECK 1R DR CROSS BEAM, INTERCOSTAL I/B FLANGE IS CRACKED AT 4TH BEAM FROM BOTTOM, 13 INCHES FROM FWD END. REMOVED OLD INTERCOSTAL 4TH FROM BOTTOM 13 INCHES FROM FWD END. HAD SHOP FABRICATE N00557. DRILLED NEW INTERCOSTAL, INSTALLED INTERCOSTAL TREATEDApr 23, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 08FDEA01458Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 344, LBL 30 REMOVED CORROSION ON FLOOR SUPPORT STA 344, LBL 30, REF SRM 51-10- 6 PG 12. MATERIAL LOSS 50 PERCENT. FOUND TO BE OUT OF LIMITS, REF SRM 53-10-1 PG 1-3. FABRICATED NEW FLOOR SUPPORT AND SHIM, REF BOEING DWG 65-9617Apr 19, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 08FDEA01457Stringer Clip · crackedAFT PIT BILGE BODY FRAME, STR CLIP IS BUCKLED/CRACKED, BS 970, STR 27L. REMOVED AND REPLACED STRINGER CLIP AT BS 970, STRINGER 27L. IAW SRM 51-30-2, SRM 51-30-5. THIS IS CLASSIFIED AS A MINOR REPAIR.Apr 19, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach FittingsSDR 08FDEA01452Bracket · crackedE/E COMPARTMENT LEFT SIDE E1-1 RACK, SHELF FOR POWER SUPPLY TRANSFER RECTIFIER UNIT CRACKED AT FOWARD INBOARD SIDE. REMOVED MOUNTING SHELF, REMOVED DAMAGED BRACKET, FABRICATED NEW BRACKET, TREATED AND PRIMED AND INSTALLED BRACKET, RE SECURED E1-1 SHELF. REF Apr 18, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach FittingsSDR 08FDEA01449Attach Bracket · crackedMAIN ENTRY DOOR 1-L, S/N 261, UPPER AFT LINER ATTACH BRACKET IS CRACKED REMOVED BRACKET IN REF TO SRM 51-30-2 PG 2, VERIFIED MAT'L AS 2024 T3 .040" IN REF TO DWG 65-49652-5 FABRICATED NEW ANGLE IN REF TO DWG 65-49652-5. TREATED AND PRIMED ANGLE IN REF TO SRM Apr 17, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach FittingsSDR 08FDEA01448Shear Tie · corrodedFWD PIT SHEAR TIE CORRODED, STA 660 BETWEEN STR 27R - 26R REMOVED CORROSION ON FWD SHEAR TIE STA 660 STR 27R - 26R REF SRM 51-10-6 PG 12 ORIGINAL MATERIAL .050". MATERIAL REMAINING .035", MATERIAL LOSS .015". FOUND OUT OF LIMITS REF SRM 53-10-1 PG 1-2. FAApr 17, 2008 · N498FE · Boeing 727232 · Fuselage Internal Mounting StructureSDR 08FDEA01443Stringer Clip · damagedSTRINGER CLIP CRACKED ON STR 27L FS 950A REMOVED DAMAGED CLIP, REPLACED CLIP, REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Apr 17, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach Fittings
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