Boeing 727-232

Service difficulty reports · 6,539

Newest first. General aviation reporting is voluntary.

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 = '727232'
  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 DL72S981699Spar Web · crackedTHE CENTER WING REAR SPAR WEB WAS FOUND WITH 5 CRACKS NEAR UPPER SPAR CAP. THE CRACKS ARE TYPICAL OF THOSE IN BAC S/B 727-57A0182. THE SPAR WEB WAS MODIFIED PER THE S/B WITH A CHANGE TO THE REPAIR AT RBL 20 WHERE A PREVIOUS LOCAL REPAIR WAS INSTALLED. THEAug 14, 1998 · N528DA · Boeing 727232 · Wing SparSDR DL72S981696Wire · brokenEMERGENCY EXIT FLOOR LIGHTS DO NOT WORK FROM ROW 28 BACK. REPAIRED BROKEN WIRES AT END OF TRACK.Aug 14, 1998 · N478DA · Boeing 727232 · Light System WiringSDR DL72S981676Rib · crackedDURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERTICAL FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. THE CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE 2 FWD MOST FASTENER HOLES AND TRAVELS DOWN, THRU THE ENTIRE THICKNESS OF THE HAug 14, 1998 · N405DA · Boeing 727232 · Wing, Rib/BulkheadSDR CALA9801458Pan Web · corrodedINSPECTION FOUND LT AFT LAV PAN WEB CORRODED. THE CORRODED AREA WAS REMOVED IAW SRM 51-10-6. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11.Aug 14, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981673Web · crackedRT VERTICAL TORQUE BOX WEB CRACKED .25 INCH PAST ROUTE OUT AT LIGHTNING HOLE STA 1275 RT UPPER HOLE. REPAIRED PER M/M 53-11-0 FIG 819.Aug 13, 1998 · N478DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981672Panel · crackedNR 2 LT BALANCE BOARD CLOSE OUT PANEL HAS A 2 INCH CRACK AT O/B END. REPAIRED PER SRM 55-20-3.Aug 13, 1998 · N478DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S981671Support · crackedNR 8 SLAT ACTUATOR SUPPORT CRACKED I/B SIDE. REPAIRED PER MM 57-20-21.Aug 13, 1998 · N478DA · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9801452Angle · crackedINSPECTION FOUND APPROXIMATELY A 2 CRACK IN LT WING LEADING EDGE SLAT NR 2 INBOARD SLAT TRACK OUTBOARD SIDE L ANGLE. THE ANGLE WAS REPLACED IAW SRM 57-30-4, 51-20-12, AND 51-30-2.Aug 13, 1998 · N14788 · Boeing 727232 · Leading Edge DevicesSDR CALA9801451Access Plate · corrodedINSPECTION FOUND WING CENTER SECTION LOWER SKIN PLENUM ASSEMBLY INSPECTION ACCESS PLATE CORRODED ON FORWARD RT SIDE. A NEW ACCESS PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-20-1, AND MM 51-20-11.Aug 13, 1998 · N14788 · Boeing 727232 · Wing, Plate/SkinSDR CALA9801450Angle · crackedINSPECTION FOUND APPROXIMATELY A 2 CRACK IN RT WING NR 8 FLAP TRACK INBOARD TRAILING EDGE ATTACH ANGLE. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11.Aug 13, 1998 · N14788 · Boeing 727232 · Trailing Edge FlapsSDR CALA9801449Support · crackedINSPECTION FOUND A 5/8 CRACK IN OUTBOARD END OF FLOORBOARD SUPPORT AT BS 760, RBL 45.5. THE FLOORBOARD SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2.Aug 13, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981664Stringer · crackedA 1 INCH CRACK AT BOLT TO EDGE ON STR 8 FIN STA 157.2 RT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.Aug 12, 1998 · N502DA · Boeing 727232 · Vertical StabilizerSDR CALA9801444Support · crackedINSPECTION FOUND A 2 INCH CRACK IN RT INBOARD END OF FLOOR SUPPORT AT BS 760, BL 0. THE CRACKED SECTION OF FLOOR SUPPORT WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-30-2.Aug 11, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801443Bracket · crackedINSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN RT WING INBOARD NR 7 FLAP TRACK TRAILING EDGE ATTACH BRACKET. THE ATTACH BRACKET WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51-20-0.Aug 11, 1998 · N14788 · Boeing 727232 · Trailing Edge FlapsSDR DL72S982010Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 19 AND 23 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Aug 10, 1998 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982009Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 37 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Aug 10, 1998 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982008Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 35 INCHES FROM THE I/B END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.Aug 10, 1998 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982007Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 44 INCHES FROM O/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Aug 10, 1998 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981693Floorbeam · corrodedFOUND DURING MV1 CORROSION VISIT NRC 40, CORROSION AT FLOORBEAM STA 344 FROM BL 0 TO LBL 60. WORKED WITH NRC 31. REPAIRED PER SRM 53-10-8.Aug 10, 1998 · N515DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S981692Floorbeam · corrodedFOUND DURING MV1 CORROSION VISIT NRC 31, CORROSION AT CLIP NUT HOLES UPPER AND LOWER SIDE OF FLOORBEAM STA 344 BL 0 RBL 24 AREA RBL 18 TO RBL 24 WITHIN LIMITS SRM 53-10-1. AREA RBL 18 TO BL 0 WORKED ON NRC 40 SRM 53-10-8.Aug 10, 1998 · N515DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S981648Wire · brokenEMERGENCY TRACK LIGHTING SECTION IN FWD COACH AREA DOES NOT ILLUMINATE. REPAIRED SECTION OF WIRE.Aug 10, 1998 · N532DA · Boeing 727232 · Light System WiringSDR CALA9801442Skin · crackedINSPECTION FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN AT STA 1183, WL 189, RBL 30. A DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW BOEING 727 DRAWING NR 65C31446-3.Aug 10, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801441Spar Channel · crackedINSPECTION FOUND U-CHANNEL AT REAR SPAR OF LT WING LOWER SURFACE JUST INBOARD OF SECOND OUTBOARD FLAP TRANSMISSION WORN AND CRACKED OUT OF NUT PLATE HOLE. THE CHANNEL WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-30-2.Aug 10, 1998 · N14788 · Boeing 727232 · Wing SparSDR CALA9801440Pan · crackedINSPECTION FOUND AFT EDGE OF PRESSURE PAN CRACKED APPROXIMATELY TWO INCHES AT FASTENER HOLE STA 740-760, LT SIDE. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11.Aug 10, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981650Bulkhead Web · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH CRACK AT RBL 25 AND WL 169. THE CRACK WAS REPAIRED WITH A TITANIUM REPAIR DOUBLER ON A TEMPORARY BASIS WITH REPETITIVE INSPECTIONS. THE PERMANENT REPAIR WILL ACCOMPLISH A WEB MODIFICATION PER BAC S/B 727-53-02Aug 8, 1998 · N543DA · Boeing 727232 · Fuselage Main, BulkheadSDR CALA9801422Strap · corrodedINSPECTION FOUND BUTT STRAP IN FORWARD CARGO PIT CORRODED AT LT STA 555-630. A NEW BUTT STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-12.Aug 8, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801421Strap · corrodedINSPECTION FOUND BUTT STRAP CORRODED IN AFT PIT AT STA 950A. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, PAGE 7, 51-10-2, PAGE 4, AND MM 51-20-12, PAGE 710.Aug 8, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801420Splice · corrodedINSPECTION FOUND BUTT SPLICE NR 3 IN FORWARD CARGO COMPARTMENT ON RT SIDE CORRODED. A NEW BUTT SPLICE WAS FABRICATED AND INSTALLED IAW MM 51-20-1, 51-10-2, AND 51-20-12.Aug 7, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801419Splice · corrodedINSPECTION FOUND BUTT SPLICE NR 2 IN FORWARD CARGO COMPARTMENT ON RT SIDE CORRODED. A NEW BUTT SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-12.Aug 7, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981616Battery Pack · dischargedALL 1ST CABIN SEAT MOUNTED EMERGENCY EXIT LIGHT AND ROWS 10 AND 11 EMERGENCY EXIT PATH LIGHTS INOP DURING STBY POWER CHECK. REPLACED BATTERY PACK AND BATTERY RACK OPS CKS OK.Aug 6, 1998 · N529DA · Boeing 727232 · Emergency LightingSDR DL72S981614Frame · corrosionCORROSION WAS FOUND ON THE O/B FLANGE OF THE O/B CHORD OF THE C2 DOOR SILL. APPROX 0.060 OF MATERIAL FROM THE UPPER SURFACE OF THE FLANGE WAS REMOVED. REPAIRED PER ERA 331905-14.Aug 6, 1998 · N523DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S981613Skin · crackedL1 DOOR SURROUND BEAR STRAP WAS FOUND CRACKED IN THE LWR AFT CORNER OF THE DOOR. CRACK WAS TRIMMED OUT THRU THE SKIN, BONDED DOUBLER AND BEAR STRAP. REPAIRED PER ERA 331987-14.Aug 6, 1998 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981612Frame · crackedA CRACK WAS FOUND IN THE FRAME AT FS 380 AND WL 280, JUST ABOVE THE R1 DOOR CUTOUT. REPAIRED PER ERA 331909-14.Aug 6, 1998 · N523DA · Boeing 727232 · Fuselage Main, FrameSDR CALA9801410Strap · corrodedINSPECTION FOUND FORWARD CARGO PIT FLOOR SUPPORT STRAP CORRODED WITH ELONGATED HOLES AT STA 540. A SUPPORT STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.Aug 6, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801409Tip · crackedINSPECTION FOUND LT WING TIP INBOARD ACCESS PANEL 8112 DEFORMED AND CRACKED. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-20-01.Aug 6, 1998 · N14788 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9801408Floor · puncturedINSPECTION FOUND A HOLE IN FORWARD PIT FLOOR PANEL AT STA 640-720. THE DAMAGED AREA WAS CUT OUT. TWO DOUBLERS AND REPAIR FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-7, 51-10-2, 51-30-2, AND MM 51-20-11.Aug 6, 1998 · N14788 · Boeing 727232 · Fuselage Floor PanelSDR CALA9801407Floor · puncturedINSPECTION FOUND A PUNCTURE IN AFT CARGO FLOOR PANEL AT STA 950E. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-10-7, 51-10-2, 51-30-2, AND MM 51-20-11.Aug 6, 1998 · N14788 · Boeing 727232 · Fuselage Floor PanelSDR DL72S981606Oxygen Bottle · emptyCREW OXYGEN READS ZERO, SUSPECT REGULATOR AT JUMPSEAT STUCK IN EMERGENCY POSITION. FREED JUMPSEAT 02 SWITCH, REPLACED CREW O2 BOTTLE LEAK AND OPS CKS OK.Aug 5, 1998 · N497DA · Boeing 727232 · Crew Oxygen SystemSDR DL72S981602Frame · crackedA 1 INCH CRACK FUSELAGE FRAME FWD SIDE AFT RT SVC DOOR UPPER STOP PAD. REPAIR PER M/M 53-13-0.Aug 4, 1998 · N420DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981601Hose · leakingAFTER T/O, LOST A-SYS HYD FLUID. RETURNED TO MSY. FOUND LEAKING SUPPLY LINE AT LEFT ELEVATOR PCU. REPLACED LINE.Aug 4, 1998 · N511DA · Boeing 727232 · Hydraulic System, MainSDR DL72S981630Fitting · corrodedLEFT WING FWD WING FITTING BORE HAS CORROSION AND SCORING, FOUND WHEN BUSHING REMOVED. REMOVED BTL PIN ON R/C 59, OPN 5508AD AND REMOVED FWD BUSHING PER M/M 57-41-11. FOUND CORROSION TO BE WITHIN .15 OF INNER EDGE OF TERMINAL FITTING AT 10 AND 11 O'CLOCK POSAug 1, 1998 · N405DA · Boeing 727232 · Wing, Fuselage Attach FittingsSDR DL72S981592Skin · corrodedCORROSION WAS FOUND IN THE SKIN AT THE STRINGER 26L LAP SPLICE. THE CORRODED AREA WAS TRIMMED OUT AND AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED. THE SKIN LAP WAS SEPARATED AND INSPECTED FWD AND AFT OF THE DAMAGED AREA AND WAS RESTORED WITH PROTRUDINGAug 1, 1998 · N484DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981594Skin · dentedTHE FUSELAGE SKIN WAS BADLY DENTED AT FS 295 BETWEEN STR 12L AND 13L DUE TO A BIRD STRIKE. THE DAMAGED AREA WAS CUTOUT AND REPAIRED PER THE B727 SRM 53-30-3, FIG 1 WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS DOCUMENTED PER ER/A 365361-14 WHICH AJul 31, 1998 · N419DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981593Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT THE STRINGER 26L LAPSPLICE. THE CORRODED AREA WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 365330-14, REV B.Jul 31, 1998 · N484DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L981596Spar · crackedA TYPICAL CRACK WAS FOUND IN THE REAR SPAR OF THE LT ELEVATOR EXTENDING FROM UNDER THE SHEAR PLATE OF THE MIDDLE TAB FITTING. THE CRACK EXTENDS .125 LONG BEYOND THE FITTING. THE CRACK WAS STOP DRILLED PER BAC S/B 727-55-0089 AND WILL BE RE-INSPECTED WITHIN 1Jul 31, 1998 · N506DA · Boeing 727232 · Elevator, Spar/RibSDR DL72L981583Web · crackedFOUND ON F1 LETTER CK, CRACK IN VERTICAL WEB STA 1225 FROM FASTENER HOLE. REPAIRED PER MM 53-11-0.Jul 30, 1998 · N506DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981604Stringer · corrodedFOUND DURING MV1 CORROSION VISIT NRC 121, CORROSION ON STR 29 LT OUTBOARD LEG AFT OF STA 990 TO STA 1010. REPAIRED PER SRM 53-10-11 FIG 3.Jul 29, 1998 · N493DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S981579Rib · crackedNR 7 SLAT O/B ACTUATOR ATTACH RIB HAS BEEN STOP DRILLED TWICE INDICATING THAT CRACK HAS CONTINUED TO GROW. REMOVED ACCESS PANELS TO RIB. FABRICATED DOUBLER. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER MM 57-54-0 FIG 804. REPAIR OK PER M/M. OK TO CLOSE SJul 29, 1998 · N523DA · Boeing 727232 · Leading Edge DevicesSDR DL72S981578Angle · crackedNR 5 SLAT ANGLE CRACKED AT O/B SIDE OF ACTUATOR ATTACH RIB. REMOVED PANELS 6501, 6573 AND 6502 FOR ACCESS. REPAIRED PER MM 57-54-0, FIG 804. INSTALLED PANELS 6501, 6573 AND 6502.Jul 29, 1998 · N523DA · Boeing 727232 · Leading Edge DevicesSDR DL72S981574Line · failed20 MIN AFTER TAKEOFF FROM ABQ, HAD TOTAL LOSS OF A SYSTEM HYDRAULICS. C/W POM PROCEDURES. DIVERTED TO DFW. REPLACED BROKEN LINE TO A SYSTEM HYDRAULIC MODULE. REPLACED NR 1 ENGINE DRIVEN HYD PUMP. PRESSURE AND LEAK CHECK OK.Jul 29, 1998 · N416DA · Boeing 727232 · Hydraulic System, Main
Back to Boeing 727-232