Boeing 737-230

Service difficulty reports · 466

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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 = '737230'
  ORDER BY difficulty_date DESC"

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SDR 2002F00109Sensor · malfunctionedFLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNLG FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. (M)Jan 18, 2002 · N818AL · Boeing 737230 · Cabin Temperature SensorSDR TSAA0253022Skin · crackedREPAIRED CRACK AT FS 965 (AFT ENTRY DOOR). CUTOUT AND REMOVED CRACK PORTION OF SKIN AROUND LOWER FORWARD AREA. PERFORMED HFEC INSPECTION AROUND CUT OUT AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED A REPAIR FILLER AND PLATE IAW SRM 53-30-3. AIRCRAFT RETUJan 14, 2002 · N821AL · Boeing 737230 · Fuselage Main, Plate/SkinSDR TSAA0253007Skin · crackedREPAIRED 1.25 INCH FUSELAGE SKIN CRACK AT BS 787 S-11L. TRIMMED OUT CRACK DAMAGE AND VERIFIED WITH HFEC, NO DEFECTS NOTED. FABRICATED, INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-30-3 FIGURE 25. AIRCRAFT RETURNED TO SERVICE. (M)Jan 7, 2002 · N818AL · Boeing 737230 · Fuselage Main, Plate/SkinSDR TSAA0255019Skin · damagedCOMPOSITE DAMAGE TO LEFT SIDE AT RUDDER STATION 86.59 TO STATION 66.59. REMOVED ALL CONTAMINATION AND WATER FROM DAMAGED AREA. FABRICATED, CLEANED, AND INSTALLED HONEYCOMB REPLACEMENT CORE PLUG. REPAIRED IAW SRM 55-40-5 AND 51-40-14 REPAIR NR 3. (M)Jan 2, 2002 · N823AL · Boeing 737230 · Rudder, Plate/SkinSDR TSAA0133183Battery Pack · dischargedREPLACED RIGHT OVERWING LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 27, 2001 · N818AL · Boeing 737230 · Emergency LightingSDR TSAA0253017Spar · corrodedBLENDOUT THE CORROSION DAMAGE ON HORIZONTAL STABILIZER UPPER CHORD AT ELEVATOR STATION 66.54 TO A 10:1 RATIO SPANWISE. FLAP PEEN REPAIR AREA. FABRICATED AND INSTALLED AN EXTERNAL DOUBLER. SHOT PEEN, ALODINE, AND PRIMED EXTERNAL DOUBLER IAW ECO 2513. AIRCRADec 17, 2001 · N823AL · Boeing 737230 · Horizontal Stabilizer, Spar/RibSDR TSAA0253011Keelbeam · corrodedDISCOVERED CORROSION AT RIGHT KEEL BEAM LOWER CHORD LOWER SURFACE AT BS 727. REMOVED CORROSION PER SRM 51-10-6. VISUALLY, INSPECTED THE AREA TO ENSURE NO CRACKS AND ALL CORROSION REMOVED. FABRICATED A FILLER, DOUBLER, AND TRIPLER AND INSTALLED. AIRCRAFT OKDec 15, 2001 · N823AL · Boeing 737230 · Fuselage Main, KeelSDR TSAA0253010Frame · crackedREMOVED ALL FASTENERS COMMON TO BS 727 OUTER CHORD FROM S-27L UP TO S18L. CHORD CRACKED BETWEEN S23L AND S24L. AIRCRAFT OK FOR SERVICE. (M)Dec 5, 2001 · N823AL · Boeing 737230 · Fuselage Main, FrameSDR TSAA0253012Spar · corrodedDISCOVERED CORROSION AT RIGHT WING WBL 304.5 FORWARD SPAR LOWER CHORD. REMOVED CORROSION PER SRM 737-100/200, 57-30-1 FIGURE 1. HFEC INSPECTED BLENDOUT AREA TO ENSURE NO CRACKS AND CORROSION REMOVED. RESTORED AIRCRAFT TO NORMAL IAW ECO 2135. AIRCRAFT OK FODec 5, 2001 · N823AL · Boeing 737230 · Wing SparSDR TSAA0153161Skin · crackedDISCOVERED CRACK AT BS 727A, S-15R. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)Nov 21, 2001 · N820AL · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0030Flap · delaminatedDuring "C" Inspection.-L-H Wing Imb Fore Flap upper Surface WBL 150.4 Delaminated.-Repaired L-H Wing Imb Fore Flap P/N 65-46430-89, S/N BN-430 Due to Delamination From WBL 73.00 to 89 & From WBL 156.15 to 145.15 IAW COOPESA EO No. COO-CMP-3-57-613-01, Dated NoNov 21, 2001 · N122NJ · Boeing 737230 · Trailing Edge FlapsSDR P2EA2001V0029Flap · delaminatedDuring "C" Check Inspection.-L-H Wing Outb Flap Imb Hinge Flap, T/E Section Delaminated.-Repaired L-H Outb Flipper Flap, P/N 65-71930-91 Due to Delamination IAW COOPESA EO No. COO-CMP-3-57-610-01, Dated Nov 06, 2001 Approved on FAA 8110-3 Form By DERT710167SW.Nov 21, 2001 · N122NJ · Boeing 737230 · Trailing Edge FlapsSDR P2EA2001V0028Flap · wornDuring "C" Check Inspection.-R-H Wing Imb Fore Flap Skin Worn at Imb Side.-Repaired R-H Imb Fore Flap, P/N 65-46430-90, S/N BN436 Due to Worn Skin IAW COOPESA EO No. COO-CMP-3-57-608-01, Dated Nov 06, 2001 Approved on FAA 8110-3 Form By DERT-710167SW.Note: SeeNov 21, 2001 · N122NJ · Boeing 737230 · Trailing Edge FlapsSDR P2EA2001V0027Flap · delaminatedDuring "C" Check Inspection.-R-H Wing Imb Aft Flap Delaminated & Dented.-Repaired R-H Wing Imb Flap P/N 65-46434-140, S/N BN442 Due to Delamination From Wbl 180.75 to 165.875 & From Wbl 155.75 to 143 IAW COOPESA EO No.COO-CMP-3-57-612-01 Dated Nov 06, 2001, ApNov 21, 2001 · N122NJ · Boeing 737230 · Trailing Edge FlapsSDR P2EA2001V0025Door · delaminatedDuring "C" Check Inspection.-R-H NLG Door, P/N 65-50520-504, S/N BNW330 Found With Delamination.-Repaired R-H NLG Door Due to Delamination From BS294.5 to BS262.5, IAW COOPESA EO No.COO-CMP-3-52-614-01, Dated Nov 07, 2001 & Documented on FAA 8110-3 Form ApprovNov 20, 2001 · N122NJ · Boeing 737230 · Landing Gear DoorsSDR P2EA2001V0026Flap · delaminatedDuring "c" Check Inspection.-L-H Imb Mid Flap, P/N 65-79953 T/E With Delamination.-Repair T/E of Imb Mid Flap P/N 65-79953 Due to Delamination IAW COOPESA EO No.COO-CMP-3-57-611-01 Dated Nov 06,2001 & Documented on FAA 8110-3 Form Approved by DERT-710167SW.NotNov 20, 2001 · N122NJ · Boeing 737230 · Trailing Edge FlapsSDR P2EA2001V0024Attach Angle · crackedDuring "C" Check Inspection.-Control Cabin, Fwd Pressure Bulkhead BS178, R-H Side Chord Cracked Between WL 207 & 210.-Preventive Modification accomplished at Fwd Pressure Bulkhead BS178, R-H Chord, Between WL184 & 230 due to Crack IAW Boeing S/B 737-53A1173, RNov 14, 2001 · N122NJ · Boeing 737230 · Fuselage Main, BulkheadSDR P2EA2001V0023Skin · dentedDuring "C" Check Inspection.-Fuselage at BS325, Between Str 20 & 21 R-H, Skin With Dent Out of Limits.-Fuselage Skin Section Repaired, From BS320 to BS350.5, Between Str 19 & 24 R-H, IAW SRM 53-30-3, Fig 17.Note: See COOPESA Work Order No.O10863 1-8, VAM100 NoNov 14, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0022Skin · crackedDuring "C" Check Inspection.-L2 Door Area, Fuselage Lower Hinge Cut out, Lower Section, Skin With Sharp Edges & Crack.-Repaired Fuselage Skin Section at L2 door Lower Hinge Cut out, From BS945to BS956, Between Str 13 & 16 L-H, IAW SRM 53-30-3, Fig 34.Note: SeeNov 14, 2001 · N122NJ · Boeing 737230 · Fuselage, Door HingeSDR P2EA2001V0021Skin · dentedDuring "C" Check Inspection.-Fuselage at BS499, Between Str 26 & 27 R-H, Skin With Dent Out of Limits.-Fuselage Skin Section Repaired From BS492 to BS504.5, Between Str 25 & 28 R-H, Due to Dent, IAW Boeing Telex COO-SJO-01-00893H & COOPESA E.O. No.COO-3-53-607Nov 13, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0020Skin · dentedDuring "C" Check Inspection.-Fuselage at BS984, Between Str 24 & 25 L-H, Skin With Dent Out of Limits.-Fuselage Skin Section Repaired From BS982 to BS986.5, Between Str 24 & 25 L-H, Due to Dent IAW SRM 53-30-3 Fig 5.Note: See COOPESA Work Order No.O10863 1-17,Nov 13, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0019Stringer · crackedDuring "C" Check Inspection.-Fuselage, BS1080, Str 22 R-H With Crack.-Fuselage Stringer Section Repaired at Str 22 R-H, From BS1050 to BS1088, IAW SRM 53-10-3, Fig 1Note: See COOPESA Work Order No. O10863 1-70, VAM100 No. 227 & 122SDA099.Nov 12, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Longeron/StringerSDR P2EA2001V0018Skin · dentedDuring "C" Check Inspection.-Fuselage, at BS390, Between Str 17 & 18 L-H, Skin With Dent Out of Limits.-Repaired Fuselage Skin Section From BS387 to BS396, Between Str17 & 18 L-H,IAW SRM53-30-3 Fig17Note: See COOPESA Work Order No. O10863 1-9, VAM100 No.046 & Nov 12, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0017Skin Panel · crackedDuring "C" Check Inspection.-Fuselage, Keel Beam Panel Cracked at BS 698 and With Loose Rivets at BS726, Str27 L-H.-Replaced Fuselage Keel Beam Skin Panel from BS 661.75 to BS 726.75, Between LBL 6.30 to RBL 6.30 due to Cracks IAW Boeing S/B 737-53-1104, SectiNov 12, 2001 · N122NJ · Boeing 737230 · Fuselage Main, KeelSDR P2EA2001V0016Fairing · wornDuring "C" Check Inspection.-Engine No.1, Nacelle Fairing, Imb Aft Section, Outter Skin With Wear.-Engine No.1, Nacelle Fairing, Imb Aft Section, Outter Skin Repaired due to Wear, IAW COOPESA E.O. No. EO-100-3-54-609-01, Dated Nov 06, 2001 Documented on FAA811Nov 12, 2001 · N122NJ · Boeing 737230 · Nacelle/Pylon, Plate/SkinSDR P2EA2001V0015Skin · dentedDuring "c" Check Inspection:-Fuselage, BS1086, Between Str 25 & 26 R-H Skin With Dent Out of Limits.-Repaired Fuselage Skin Section From BS1069.5 to BS1090.5, Between Str 20 & 27 R-H due to Dent, IAW COOPESA E.O. No.EO-100-3-53-604-01, Dated Nov 05, 2001 DocumNov 12, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0014Fairing · wornDuring "C" Check Inspection:-No.2 Engine Pylon, Aft Fairing Worn at Imb Side.-No. 2 Pylon Imboard Fairing Outer Skin Repaired due to Wear, IAW COOPESA E.O. No. EO-COO-3-54-609-01, Dated Nov 06, 2001, Documented on FAA 8110-3 form approved by DERT710167SW.Note:Nov 12, 2001 · N122NJ · Boeing 737230 · Nacelle/Pylon, Plate/SkinSDR P2EA2001V0013Skin · dentedC CHECK, VERTICAL FIN WITH DENTS BETWEEN FIN STA 191.5 - 180.3. REPAIRED SKIN IAW SRM 55-30-6 FIG 2.Nov 12, 2001 · N122NJ · Boeing 737230 · Vertical Stabilizer, Plate/SkinSDR P2EA2001V0012Door Frame · crackedDURING C CHECK INSPECTION, L1 DOOR FWD AND AFT LOWER CORNER AND LOWER PAN WITH A CRACK. REPAIRED DOOR FRAME IAW SRM 51-40-3 FIG 1.Nov 12, 2001 · N122NJ · Boeing 737230 · Passenger/Crew DoorsSDR TSAA0133150Battery Pack · dischargedREPLACED FORWARD SERVICE AND ENTRY DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 8, 2001 · N820AL · Boeing 737230 · Emergency LightingSDR TSAA0133146Battery Pack · dischargedREPLACED LEFT OVERWING IDENT POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Oct 27, 2001 · N818AL · Boeing 737230 · Emergency LightingSDR P2EA2001V0008Shroud · crackedDURING C-CHECK FOUND APU SHROUD (COWL) LEFT AFT SIDE CRACKED. APU LOWER SHROUD SKIN REPAIRED IAW COOPESA EO COO-3-49-587-01, DOCUMENTED ON FAA FORM 8110-3.Oct 22, 2001 · N124NJ · Boeing 737230 · APU Cowling/ContainmentSDR TSAA0133144Battery Pack · dischargedREPLACED NR 5 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)Oct 20, 2001 · N821AL · Boeing 737230 · Emergency LightingSDR P2EA2001V0007Crossbeam · crackedDURING C CHECK WAS FOUND THE FWD CARGO DOOR, FWD LOWER CORNER CROSS BEAM CRACKED. FWD CARGO DOOR CROSS BEAM FWD T CHORD AND PERFORMED PREVENTIVE MODIFICATION IAW SB 737-52A1100 REV 4, SECTION III FIG 4 AND 6.Oct 19, 2001 · N124NJ · Boeing 737230 · Cargo/Baggage DoorsSDR P2EA2001V0004Keelbeam · crackedDURING C CHECK FOUND THE AFT CARGO COMPARTMENT STR 27R AT BS 727+16 KEEL BEAM CHORD WITH CRACK. FUSELAGE KELL BEAM SECTION REPAIRED AT STR 27R, BETWEEN BS 727+9.75 AND BS 727A+7.25 DUE TO CRACK IAW COOPESA E.O NR COO-3-53-585-01. DOCUMENTED ON FAA FORM 8110-3 Oct 19, 2001 · N124NJ · Boeing 737230 · Fuselage Main, KeelSDR P2EA2001V0003Skin · dentedDURING C CHECK FOUND THE EXTERNAL FUSELAGE SKIN AT BS 909.25 BETWEEN STR 21R AND 22R WITH DENT OUT LIMITS. FUSELAGE SKIN SECTION REPAIRED FROM BS 907 TO BS 912 BETWEEN STR 21R AND STR 23R IAW SRM 53-30-3 FIG 28.Oct 19, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0001Skin · dentedDURING C CHECK: EXTERNAL FUSELAGE AT BS 1042 BETWEEN STR 14L AND 15L SKIN WITH DENT. FUSELAGE SKIN SECTION REPAIRED FROM BS 1039 TO BS 1048 BETWEEN STR 13L TO STR 16L IAW SRM 53-30-3 FIG 6.Oct 19, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0011Skin · wornDURING C-CHECK, FOUND THE LEFT WING T/E FORE FLAP P/N 65-46430-89, S/N BN 436 UPPER SKIN WORN. LT WING I/B FORE FLAP REPAIRED FROM WBL 74.5 TO WBL 79.5 IAW SRM 51-40-20 REPAIR 21 FIG 30.Oct 18, 2001 · N124NJ · Boeing 737230 · Trailing Edge FlapsSDR P2EA2001V0005Skin · dentedDURING C CHECK: FWD CARGO DOOR EXTERNAL SKIN WITH SEVERAL DENTS OUT LIMITS. FWD CARGO DOOR SKIN REPLACED IAW SRM 52-30-2 FIG 3.Oct 18, 2001 · N124NJ · Boeing 737230 · Cargo/Baggage DoorsSDR P2EA2001V0002Skin · canningDURING C CHECK WAS FOUND THE EXTERNAL FUSELAGE SKIN AT BS 1078 BETWEEN STR 23R AND STR 24R WITH OIL CAN. FUSELAGE SKIN SECTION REPAIRED FROM BS 1054 TO BS 1088 BETWEEN STR 16R AND STR 25R IAW COOPESA EO COO-3-53-581-01, DOCUMENT ON FAA 810-3 APPROVED BY FAA DEOct 18, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001V0010Skin · dentedDURING C-CHECK RIGHT WING L/E SECTION FSS 338 OUTER SKIN WITH DENT. RIGHT WING L/E SECTION BETWEEN FSS 333.8 AND FSS 345.8 DUE TO DENT IAW SRM 57-30-4 FIG 5.Oct 18, 2001 · N124NJ · Boeing 737230 · Wing, Plate/SkinSDR P2EA2001V0006Skin · dentedDURING C CHECK EXTERNAL FUSELAGE BS 374 STR 20R SKIN WITH DENT OUT LIMITS. SKIN SECTION REPAIRED FROM BS 367 TO 381.5 BTW STR 19R AND STR 21R IAW COOPESA EO COO-3-53-580-01 APPROVED BY DER.Oct 18, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA2001M0008SkinDuring Inspection found Crack in fuselage skin at BS 847 and STR. 25R approx. 1.00" in length.See Vanguard Aircraft log page #92242Oct 16, 2001 · N124NJ · Boeing 737230 · Fuselage Structure (General)SDR P2EA01195Skin · damagedSJO - DURING C-CHECK, AFT ENTRY DOOR, EXTERIOR SKIN WITH TEMPORARY REPAIR AT LOWER HINGE. REPAIRED DOOR SKIN SECTION, BETWEEN BEAMS 5 AND 6, FROM BS 959 TO BS 963.750, IAW SRM 52-00-3, FIG 3. (M)Sep 18, 2001 · N123NJ · Boeing 737230 · Passenger/Crew DoorsSDR P2EA01190Coupler · failedFLT 552 - MDW - YAW DAMPER INOPERATIVE. REMOVED AND REPLACED YAW DAMPER COUPLER OPERATIONAL CHECK NORMAL IAW MM 22-12-0. (M)Sep 16, 2001 · N122NJ · Boeing 737230 · Autopilot SystemSDR P2EA01192Gyro · failedFLT 313 - MCI - WITH `A` AUTO PILOT ENGAGED, YOKE JERKS/PUMPS 3 OR 4 TIMES ABRUPTLY IN DESCENT. REMOVED AND REPLACED NR 1 VERTICAL GYRO AND OPERATIONAL CHECK NORMAL IAW MM 22-11-01. (M)Sep 15, 2001 · N124NJ · Boeing 737230 · Attitude Gyro and Indicating SystemSDR P2EA01194Stringer · corrodedSJO - DURING C-CHECK, AFT CARGO COMPARTMENT BS 927 STRINGER 27 RIGHT WITH CORROSION. STRINGER 27 RIGHT REPAIRED, FROM BS 902 TO BS 962, DUE TO CORROSION IAW SRM 53-10-3 FIG 1. (M)Sep 14, 2001 · N123NJ · Boeing 737230 · Fuselage Main, Longeron/StringerSDR P2EA01183Skin · delaminatedSJO - DURING C-CHECK, FOUND LEFT WING INBOARD MID FLAP T/E PANEL CENTER AREA, WBL 135, LOWER SURFACE, DENT FILLING COMPOUND MIGRATED. REPAIRED LEFT WING INBOARD MID FLAP, P/N 65-46486, COOPESA CODE TMC-078, AT T/E SECTION, DUE TO DELAMINATION, FROM WBL 106.24Sep 9, 2001 · N123NJ · Boeing 737230 · Trailing Edge FlapsSDR P2EA01184Autopilot Sys · malfunctionedA CHANNEL AUTO PILOT STARTED TO SHAKE IN THE DESCENT. PERFORMED ADJUSTMENT AND TEST PER MM 22-11-01, NO DEFECTS NOTED. (M)Sep 9, 2001 · N124NJ · Boeing 737230 · Autopilot SystemSDR P2EA01185Frame · crackedSJO - DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT, BS 460, BETWEEN STRINGER 20 AND 21 LEFT FRAME WITH CRACK. REPAIRED FUSELAGE FRAME SECTION AT BS 460, BETWEEN STRINGER 19 AND 26 LEFT DUE TO CRACKS IAW COOPESA EO NR COO-3-53-519-01. THIS REPAIR HAS BEEN ASep 8, 2001 · N123NJ · Boeing 737230 · Fuselage Main, Frame
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