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 DL72S991402Valve · failedENG RUNNING ESS PWR SEL ON ENG 1, BOTH PACKS ON. APU GEN/FIELD BREAKER OPENED WITH ASSOCIATED AMBER LIGHTS, 1-3 BTBS OPEN WITH LIGHTS. PACKS TRIPPED, SMOKE, HOT PACK SMELL AND LOSS ELECT. RETURNED TO GATE. ELECT FAULT PANEL UNDEREXCITED SYS 1-3. LIGHTS ILJun 20, 1999 · N535DA · Boeing 727232 · Cabin Cooling SystemSDR DL72L991401Connector · shortedCONTINUOUS FIRE WARNING ON NR 3 ENGINE. UNABLE TO SILENCE FIRE WARN. BOTH EXTINGUISHER BOTTLES DISCHARGED WITH NO HELP. NR 3 ENGINE SHUT DOWN. RECEIVED WARNING APPROX 50 MIN INTO FLIGHT. ENG WINDMILLED FOR APPROX 5 MIN AFTER SHUTDOWN. FOUND LWR FIRJun 20, 1999 · N514DA · Boeing 727232 · Fire DetectionSDR MZZA99125Splice · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH IG CORROSION WAS FOUND ON STRINGER 30 SPLICE ON CARGO COMPARTMENT AT BS 1010. THE DAMAGED PART WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAPTER 53-10-03 FIG 1. (M)Jun 18, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99118Stringer · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 12 AND WS 686.5 WEB ATTACHMENT. THE CRACKED STRINGER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M)Jun 18, 1999 · N15790 · Boeing 727232 · Wing, Longeron/StringerSDR MZZA99117Stringer · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 11 AND WS 629 WEB ATTACHMENT. THE CRACKED STIFFENER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M)Jun 18, 1999 · N15790 · Boeing 727232 · Wing, Longeron/StringerSDR DL72L991500Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 36 INCHES FROM I/B END. THE DAMAGE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Jun 18, 1999 · N502DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991498Skin · crackedDURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 36 INCHES FROM I/B END OF FLAP. THE CRACK WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 809.Jun 18, 1999 · N502DA · Boeing 727232 · Wing StructureSDR DL72L991388Skin · crackedDURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S26R LAP SPLICE BETWEEN BS 540-560. THE CRACK WAS FOUND IN FASTENER ROW 9 AS ID'D IN FIGURE 6 OF THE SUBJECT SI. REPAIRED PER ERA 333288-14AD.Jun 18, 1999 · N502DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991387Skin · crackedDURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP SPLICE BETWEEN BS 1070-1090. THE CRACK WAS FOUND IN FASTENER ROW 4 AS ID'D IN FIGURE 6 OF THE SUBJECT SI. REPAIRED PER ERA 333282-14AD.Jun 18, 1999 · N502DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991386Skin · crackedDURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP SPLICE BETWEEN BS 700-720. THE CRACK WAS FOUND IN FASTENER ROW 4 AS ID'D IN FIGURE 6 OF THE SU BJECT SI. REPAIRED PER ERA 333284-14AD.Jun 18, 1999 · N502DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991385Skin · crackedDURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP SPLICE BETWEEN BS 600-620. THE CRACK WAS FOUND IN FASTENER ROW 10 AS ID'D IN FIGURE 6 OF THE SUBJECT SI. REPAIRED PER ERA 333281-14AD.Jun 18, 1999 · N502DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991384Skin · crackedDURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP SPLICE BETWEEN BS 440-460. THE CRACK WAS FOUND IN FASTENER ROW 12 AS ID'D IN FIGURE 6 OF THE SUBJECT SI. REPAIRED PER ERA 333280-14AD.Jun 18, 1999 · N502DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991382Sill · corrodedFUSELAGE C2 DOOR SURROUND LOWER SILL OUTBD CHORD, CORROSION REPAIR. THE OUTBOARD CHORD OF THE C2 DOOR OPENING LOWER SILL WAS FOUND CORRODED ON THE OUTBD FLANGE BETWEEN FS 950F+11 AND FS 960. THE CORROSION WAS BLENDED AWAY WITH A MAXIMUM DEPTH OF .075. THE DJun 17, 1999 · N535DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991376Wire · damagedON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITHNEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERVICE LETTER 727-SL-24Jun 17, 1999 · N509DA · Boeing 727232 · Electrical Power System WiringSDR DL72L991375Wire · damagedON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITHNEW TYPE CABLES BMS 13-58 D. P/N 012210733 PER BOEING SERVICE LETTER 727-SL-2Jun 17, 1999 · N509DA · Boeing 727232 · Electrical Power System WiringSDR DL72K991380Light · inoperativeEMERGENCY EXIT LIGHT AT R1 DOOR INOP. REPLACED EMERGENCY LIGHT ASSEMBLY AT R1 DOOR, OPS NORMAL.Jun 17, 1999 · N412DA · Boeing 727232 · Emergency LightingSDR CALA9900699Skin · corrodedINSPECTION FOUND FUSELAGE SKIN BULGED AFT OF EXTERNAL POWER RECEPTACLE AT STA 294, WL 160. THE BULGED AREA WAS CUT OUT. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3.Jun 17, 1999 · N27783 · Boeing 727232 · Fuselage Main, Plate/SkinSDR MZZA99126Stringer · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON STRINGER 26R BETWEEN BS 448 AND BS 480. THE CORRODED PART OF STRINGER WAS TRIMMED AND REPAIRED PER B727 CHAPTER 53-10-03 FIG 1. (M)Jun 16, 1999 · N15790 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR MZZA99112Web · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.625 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB AT BS 1213. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M)Jun 16, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S991372Skin · crackedREF NRC 52 - TPA LETTER CHECK C-1, .5 INCH CRACK IN DOOR SKIN, R-1 DOOR LOWER FWD CORNER. INSTALLED DOUBLER PER M/M 52-11-01, NR 8.Jun 16, 1999 · N402DA · Boeing 727232 · Service DoorsSDR DL72S991371Skin · crackedREF NRC 53 TPA LETTER CHECK C-1, .5 INCH CRACK IN R-1 DOOR SKIN AT LWR AFT CORNER. INSTALLED DOUBLER PER M/M 52-11-01, NR 8.Jun 16, 1999 · N402DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S991360Frame · crackedFRAME AT BS 620 WAS FOUND CRACKED REMOVAL OF THE CRACK REQUIRED REMOVAL OF APPROX 5 OF THE UPPER FLANGE FROM THE PRODUCTION SPLICE AT RBL 11 INBD TO RBL 6. REPAIRED PER ERA 333235-14.Jun 16, 1999 · N536DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S991359Skin · gougedGOUGE FOUND IN FUSELAGE SKIN AT AFT EDGE OF THE C2 DOOR AT BS 990. DAMAGE AREA IS LOCATED AT S24R PLUS 5 AND IN THE SKIN ONLY. REPAIRED PER ERA 333244-14, REV A.Jun 16, 1999 · N536DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991833Spar · damagedLWR AFT SPAR CAP PANEL ATTACH HOLE ELONGATED 55 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802 NON SHOP ORDER 791453.Jun 16, 1999 · N502DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991831Skin · crackedT/E WEDGE LWR SKIN CRACKED 36 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 809.Jun 16, 1999 · N502DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991829Spar · crackedNR 2 MID FLAP AFT LWR SPAR CAP, REPAIR CRACKED 36 FROM I /B END. REPAIRED PER M/M 57-52-0 FIG 802.Jun 16, 1999 · N502DA · Boeing 727232 · Trailing Edge FlapsSDR CALA9900693Skin · bulgedINSPECTION FOUND RT FUSELAGE BELLY SKIN BULGED AT FS 360 AFT OF MLG. A REPAIR WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.Jun 16, 1999 · N27783 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9900692Wire · brokenINSPECTION FOUND EMERGENCY PATH LIGHTING AT SEAT ROW 28 INOPERATIVE. WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.Jun 16, 1999 · N27783 · Boeing 727232 · Light System WiringSDR CALA9900691Wire · brokenINSPECTION FOUND EMERGENCY PATH LIGHTING AT ROW 19 AND 20 INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.Jun 16, 1999 · N27783 · Boeing 727232 · Light System WiringSDR CALA9900690Battery Pack · dischargedINSPECTION FOUND THE LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-00.Jun 16, 1999 · N27783 · Boeing 727232 · Emergency LightingSDR CALA9900689Battery Pack · dischargedINSPECTION FOUND MAIN CABIN EXIT LIGHT AT OVERWING EXIT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.Jun 16, 1999 · N27783 · Boeing 727232 · Emergency LightingSDR CALA9900688Battery Pack · dischargedINSPECTION FOUND LT CENTER OVERWING EMERGENCY EXIT LIGHT FLASHING. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.Jun 16, 1999 · N27783 · Boeing 727232 · Emergency LightingSDR CALA9900687Battery Pack · dischargedINSPECTION FOUND THE R-2 DOOR EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.Jun 16, 1999 · N27783 · Boeing 727232 · Emergency LightingSDR MZZA99120Frame · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 30 SQUARE INCH AREA IG CORROSION WAS FOUND ON FUSELAGE FRAME AT BS 219 AND RT WL 233. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER SRM 51-40-03. (M)Jun 15, 1999 · N15790 · Boeing 727232 · Fuselage Main, StructureSDR DL72S991351Bracket · crackedFOUND ON D1 LETTER CK, NR 6 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.Jun 15, 1999 · N494DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S991350Skin · crackedRIGHT ELEVATOR UPPER SKIN CRACKED DAMAGED APPROX .5 INCH, 24 INCHES OUTBD OF TAB. RIGHT ELEVATOR UPPER SKIN CRACKED .375 INCH APPROX 20 INCHES OUTBD OF TAB. REPAIRED PER ERA367622-14 CODE 4-55-21.Jun 15, 1999 · N494DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S991357Skin · crackedLFEC INSPECTIONS PER SI 4-74176-12AD, REV J ON S26L LAP JOINT FROM BS 481-681 YIELDED SEVERAL CRACK INDICATIONS. ACCOMPLISHMENT OF THE HFEC CONFIRMED 4 CRACKS IN THE LOWER LAP ROW IN THE OVERLAPPED (LWR) SKIN. REPAIRED PER ERA 367594-14AD, REV A.Jun 14, 1999 · N405DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991537Rib · crackedRIB CRACKED INSIDE NR 4 L/E SLAT INBD SIDE OF ACTUATOR ATTACH POINT. REMOVED DAMAGED AREA FABRICATED DOUBLER AND REPLACEMENT CLIP PER M/M 57-54-00 FIG 809. TREAT AND PAINTED. OK TO INSTALL. REPAIRED CRACKED RIB MM 57-40-00 FIG 809.Jun 14, 1999 · N502DA · Boeing 727232 · Leading Edge DevicesSDR DL72L991389Spar · misdrilledNR 2 MIDFLAP / UPPER SPAR CHORD / WBL 124.2: ALT FASTENER INSTALLATION - AD 94-07-08. DURING ACCOMPLISHMENT OF EO 4-58708-3AD, MTC WAS UNABLE TO INSTALL THE REQUIRED HI-LOK COLLAR DUE TO INTERFERENCE WITH INSIDE SPAR RADIUS. AUTHORIZED INSTALLATION USINGJun 14, 1999 · N502DA · Boeing 727232 · Trailing Edge FlapsSDR MZZA99140Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 4 INCH AREA IG CORROSION WAS FOUND ON PASSENGER FLOOR SEAT TRACK AT BS 395 AND RBL 40. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)Jun 11, 1999 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S991323Frame · severedC3 DOOR FWD FRAME AT BS 1090 WAS FOUND SEVERED ABOVE S27R. A PARTIAL FRAME REPLACEMENT WAS MADE. NO SKIN CRACKING REPORTED. REPAIRED PER ERA 367579-14AD.Jun 11, 1999 · N520DA · Boeing 727232 · Fuselage Main, FrameSDR MZZA99134Floorbeam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 6 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT BS 328 FROM LBL 01 TO RBL 05. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-04 FIG 2Jun 10, 1999 · N15790 · Boeing 727232 · Fuselage Main, Floor BeamSDR MZZA99133Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BETWEEN BS 360/380 ALONG RBL 18. THE DAMGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)Jun 10, 1999 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR MZZA99132Seat Track · corrodedTNN - DURING D-CHECK INSPECTON ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 20 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BETWEEN BS 360 AND 380 ALONG RBL 22 AND RBL 24. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-1Jun 10, 1999 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S991307Skin · crackedDURING LFEC INSPECTION PER SI 4-74176-12AD, NUMEROUS CRACK INDICATIONS WERE FOUND IN THE VARIOUS FRAME BAYS EXTENDING FROM BS 360-480 ALONG S4R. THERE WAS A PREVIOUS REPAIR PER ERA 332834-14AD, REV B WHICH WILL BE REMOVED AND INCORPORATED INTO THIS REPAIR. RJun 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K991311Relay · overheatedJUST PRIOR TO PUSHBACK DETECTED SLIGHT ODOR AFTER ENGINE START. CYCLED PACKS AND GASPER FAN ODOR GOT PROGRESSIVELY WORSE, SEEMED CONFINED TO THE COCKPIT. ISOLATED SMELL TO COCKPIT CEILING. FOUND EMERGENCY EXIT SIGN RELAY BAD. REPLACED SAME, NO OTHER FJun 10, 1999 · N417DA · Boeing 727232 · Emergency LightingSDR DL72S991301Rib · crackedA 1 INCH CRACK IN L/E OF NOSE RIB NR 8 SLAT I/B SIDE OF O/B TRACK. REPAIRED PER M/M 57-54-0 PG 813.Jun 9, 1999 · N520DA · Boeing 727232 · Leading Edge DevicesSDR MZZA99119Stiffener · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING FRONT SPAR STIFFENER AT SS 58. THE CORRODED WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)Jun 8, 1999 · N15790 · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S991287Skin · crackedINTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 14 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP FOR THE PANEL WAS CUTOUT AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 367553-14Jun 8, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991280Light · inoperativeLT OVERWING EXTERIOR EMERGENCY LIGHT INOP.Jun 7, 1999 · N404DA · Boeing 727232 · Emergency Lighting
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