Boeing 737-2B7

Service difficulty reports · 1,360

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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 = '7372B7'
  ORDER BY difficulty_date DESC"

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SDR P2EA01113Skin · dentedSJO - DURING C-CHECK, FUSELAGE BS 1026 BETWEEN STRINGER 27L AND 27R SKIN WITH DENT OUT OF LIMITS. (M)Jul 3, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR 2001F00242Intercostal · crackedDURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 LEFT SIDE INTERCOSTAL CRACKED AT WL 195. PRESSURE BULKHEAD BS 178 INTERCOSTAL REWORKED AT LBL 24.67 WL 195 IAW SRM 53-10-1 FIG 10. (M)Jul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR 2001F00241Intercostal · crackedSJO - DURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 RIGHT INTERCOSTAL CRACKED WL 195. PRESSURE BULKHEAD BS 178 INTERCOSTAL REWORKED AT RBL 24.67 WL 195 IAW SRM 53-10-1 FIG 10. (M)Jul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR 2001F00240Bulkhead · crackedDURING C-CHECK INSPECTION PER SB 737-53A1173, PRESSURE BULKHEAD BS 178 WEB CRACKED AT WL 218, RBL 10.7. PRESSURE BULKHEAD BS 178 WEB REPAIRED FROM RBL 1.5 TO 18 BETWEEN WL 237 AND 230.5 SRM 53-10-11 FIG 1 DET II. REF P2EA01125. (M)Jul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, BulkheadSDR P2EA01125Bulkhead · crackedDURING C-CHECK INSPECTION PER SB 737-53A1173, PRESSURE BULKHEAD BS 178 WEB CRACKED AT WL 234, LBL 10. PRESSURE BULKHEAD BS 178 WEB REPAIRED FROM LBL 6.75 TO 16.25 BETWEEN WL 237 AND 230.5 IAW SRM 53-10-11 FIG 1 DET II. (M)Jul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, BulkheadSDR 2001F00228Frame · crackedDURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 LEFT SIDE LATERAL CHORD CRACKED AT WL 207. REPLACED LEFT SIDE CHORD FROM WL230 TO 188.5, LEFT SIDE WEB REPLACED FROM LBL 16 TO LBL 29, ACCOMPLISHED IAW S/B 737-53A1173 REV 3, SECTION III Jul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, FrameSDR 2001F00227Frame · crackedDURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 RIGHT SIDE LATERAL CHORD CRACKED AT WL 207. PRESSURE BULKHEAD BS 178 RIGHT LATERAL CHORD REPLACED FROM WL 230 TO 188.5 DUE TO CRACK RT SIDE WEB REPLACED FROM RBL 16 TO RBL 29, WORK ACCOMPJul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, FrameSDR P2EA01124Stiffener · crackedDURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 VERTICAL CHORD CRACKED AT LBL 57 WL 184. PRESSURE BULKHEAD BS 178 VERTICAL CHORD REPAIRED AT LBL 57 FROM WL 178.4 TO 196.5 DUE TO CRACK IAW 53-10-11 FIG 8. (M)Jul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA010780Splice · corrodedCLT - FOUND STRINGER SPLICE CORRODED 1 INCH BY 4 INCHES, BS 986.5, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3 FIG 1. (M)Jul 2, 2001 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR P2EA01111Frame · crackedSJO - DURING C-CHECK INSPECTION PER S/B 737-53A1173, FOUND PRESSURE BULKHEAD, BS 178 VERTICAL CHORD CRACKED AT LBL 5.7 WL 184, PRESSURE BULKHEAD BS 178 RIGHT SIDE LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD BS 178 LEFT SIDE LATERAL CHORD CRACKED AT WL 2Jul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, FrameSDR P2EA01112Bulkhead · crackedDURING C-CHECK INSPECTION PER S/B 737-53A1173 PRESSURE BULKHEAD, BS 178 WEB CRACKED AT WL 234, LBL 10 INCHES, PRESSURE BULKHEAD BS 178 WEB CRACKED AT WL 218, RBL 10.7 INCH, PRESSURE BULKHEAD BS 178, RT SIDE INTERCOSTAL CRACKED AT WL 195, PRESSURE BULKHEAD BS 1Jul 2, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, BulkheadSDR USAASB01188Battery Pack · inoperativeTHE L1 AND L2 EXTERIOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M)Jun 30, 2001 · N284AU · Boeing 7372B7 · Emergency LightingSDR P2EA01110Stringer · corrodedSJO - DURING C-CHECK, LOWER FUSELAGE, E/E COMPARTMENT FROM BS 344 TO 360, STRINGER 25 LEFT WITH CORROSION. TRIM OF FUSELAGE FRAME SECTION AT BS 344, AT STRINGER 25 LEFT PERFORMED DUE TO ACCESS FOR REPAIR AT STRINGER 25L. FUSELAGE STRINGER 25L REPAIRED BETWEEJun 20, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAASB01179Sign · brokenBDL - THE LEFT OVERWING EMERGENCY EXIT SIGN WAS BROKEN. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN ASSEMBLY. (M)Jun 19, 2001 · N275AU · Boeing 7372B7 · Emergency LightingSDR P2EA01104Skin · dentedSJO - DURING C-CHECK, FOUND FUSELAGE STATION 817, BETWEEN STRINGER 26 AND 27 RT SKIN WITH DENT OUT OF LIMITS. FUSELAGE SKIN REPAIR FROM BS 813 TO 824.5 BETWEEN STRINGER 26 AND 28RT DUE TO DENT IAW SRM 53-30-3, FIG 6. (M)Jun 17, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB01176Battery Pack · dischargedBWI - THE LEFT OVERWING AN LEFT LOWER FUSELAGE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M)Jun 16, 2001 · N273AU · Boeing 7372B7 · Emergency LightingSDR USAASB01174Charger · failedBWI - MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY LIGHT BETWEEN ROW 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Jun 15, 2001 · N272AU · Boeing 7372B7 · Emergency LightingSDR P2EA01106Slat · delaminatedSJO - DURING C-CHECK, LEFT WING NR 3 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 0.00 TO SS15.00. REPAIRED LEFT WING NR 3 SLAT P/N 65-46423-273A, S/N BN-7 DUE TO DELAMINATION BETWEEN SLAT STATION .27 AND 18.52 IAW COOPESA EO NR COO-CMP-Jun 14, 2001 · N127NJ · Boeing 7372B7 · Leading Edge DevicesSDR P2EA01107Slat · delaminatedSJO - DURING C-CHECK, FOUND RIGHT WING NR 6 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 352 TO SS 360 AND FROM SS417 TO SS 430. REPAIRED RT WING NR 6 SLAT TRAILING EDGE SECTION P/N 65-46421-228A, S/N BN-19 DUE TO DELAMINATION BETWEEN SLJun 14, 2001 · N127NJ · Boeing 7372B7 · Leading Edge DevicesSDR P2EA01108Skin · delaminatedDURING C-CHECK, FOUND LEFT WING INBOARD AFT FLAP LOWER SKIN WITH DELAMINATION FROM WBL 88 TO WBL 95. REPAIRED LEFT WING INBOARD AFT FLAP P/N 65-46434-139, S/N 652 DUE TO DELAMINATION AT LOWER SKIN BETWEEN WBL 88 AND 111.75 IAW COOPESA EO NR COO-CMP-3-57-260-0Jun 14, 2001 · N127NJ · Boeing 7372B7 · Trailing Edge FlapsSDR P2EA01109Skin · delaminatedSJO - DURING C-CHECK, FOUND LEFT WING AILERON UPPER SKIN WITH DENTS AND LOWER SKIN WITH DELAMINATION AT WBL 480. REPAIRED LEFT WING AILERON P/N 65-46454-23A, S/N 555 DUE TO DELAMINATION BETWEEN WBL STATION 471 AND 486 IAW COOPESA EO NR COO-CMP-3-57-259-01 DATJun 14, 2001 · N127NJ · Boeing 7372B7 · AileronsSDR P2EA01098Skin · delaminatedSJO - DURING C-CHECK, FOUND LEFT WING AILERON UPPER SKIN WITH DENTS AND LOWER SKIN WITH DELAMINATION AT WBL 480. (M)Jun 14, 2001 · N127NJ · Boeing 7372B7 · AileronsSDR P2EA01095Slat · delaminatedSJO - DURING C-CHECK, RIGHT WING NR 6 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 352 TO SS 360 AND FROM SS 417 TO SS 430. (M)Jun 14, 2001 · N127NJ · Boeing 7372B7 · Leading Edge DevicesSDR P2EA01096Slat · delaminatedSJO - DURING C-CHECK, FOUND LEFT WING NR 3 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 0.00 TO SS15.00. (M)Jun 14, 2001 · N127NJ · Boeing 7372B7 · Leading Edge DevicesSDR P2EA01097Skin · delaminatedSJO - DURING C-CHECK, FOUND LEFT WING INBOARD AFT FLAP LOWER SKIN WITH DELAMINATION FROM WBL 71 TO WBL 95. (M)Jun 14, 2001 · N127NJ · Boeing 7372B7 · Trailing Edge FlapsSDR P2EA01105Skin · crackedDURING C-CHECK, FOUND LOWER FUSELAGE, PNEUMATIC GROUND CONNECTOR AREA, FROM BS 520 TO BS 540 BETWEEN STRINGER 28L TO 28R, CUTOUT SKIN WITH SHARP EDGES AND CRACK. REPAIRED FUSELAGE SKIN. CUT OUT AREA FORM BS 500B PLUS 18 TO BS 540 BETWEEN STRINGER 27L AND 27RJun 13, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR P2EA01103Skin · dentedDURING C-CHECK, FUSELAGE STATION 274, BETWEEN STRINGER 16 AND 17 RT SKIN WITH DENT. FUSELAGE SKIN REPAIRED FROM BS 269.5 AND 271.5 BETWEEN STRINGER 16 AND 18 RIGHT DUE TO DENT IAW SRM 53-30-3, FIG 1. (M)Jun 13, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR P2EA01102Stringer · corrodedSJO - DURING C-CHECK, FOUND LOWER FUSELAGE, AFT ACCESSORY COMPARTMENT BETWEEN BS 986.5 AND 1016 STRINGER 27 LEFT CORRODED, LEVEL 2. FUSELAGE STRINGER SECTION REPAIRED AT STRINGER 27 LEFT SIDE BETWEEN BS 986.5 AND 1016 IAW SRM 53-10-3, FIG 1. (M)Jun 13, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR P2EA01100Stringer · corrodedSJO - DURING C-CHECK, LOWER FUSELAGE AFT ACCESSORY COMPARTMENT BETWEEN BS 967 AND 984.5 STRINGER 25 LEFT CORRODED LEVEL 2. FUSELAGE STRINGER SECTION REPAIRED AT STRINGER 25 LEFT SIDE BETWEEN BS 967 AND 984.5 IAW SRM 53-10-3, FIG 1. (M)Jun 13, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR P2EA01101Stringer · corrodedSJO - DURING C-CHECK, LOWER FUSELAGE, AFT ACCESSORY COMPT BETWEEN BS 967 AND 985.5 STRINGER 26RT CORRODED, LEVEL 2. FUSELAGE STRINGER SECTION REPAIRED AT STRINGER 26 RT SIDE BETWEEN BS 967 AND 986.5 IAW SRM 53-10-3 FIG 1. (M)Jun 13, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR P2EA01099Skin · damagedSJO - DURING C-CHECK, FOUND LOWER FUSELAGE PNEUMATIC GROUND CONNECTOR AREA, FROM BS 520 TO BS 540 BETWEEN STRINGER 28L TO 28R, CUT OUT SKIN WITH SHARP EDGES AND CRACK. (M)Jun 13, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA010797Support Fitting · corrodedPIT - FOUND SUPPORT FITTING CORRODED .020 INCH - .010 INCH, NOSE GEAR RIGHT TRUNNION SUPPORT FITTING BORE. REAMED BORE, INSTALLED SLEEVE PER EA 71444. (M)Jun 12, 2001 · N282AU · Boeing 7372B7 · Nose/Tail Landing Gear Attach SectionSDR P2EA01093Bulkhead · crackedSJO - DURING C-CHECK, INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD, BS 178 VERTICAL CHORD CRACKED AT LBL 57 WL 185, PRESSURE BULKHEAD BS 178 RIGHT LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD, BS 178 LEFT LATERAL CHORD CRACKED AT WL 207. BS 178 FORJun 11, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, BulkheadSDR P2EA01094Bulkhead · crackedDURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 WEB CRACKED AT WL 234, RBL 12 INCHES, PRESSURE BULKHEAD BS 178 RT SIDE INTERCOSTAL CRACKED AT WL 195, PRESSURE BULKHEAD BS 178 LEFT SIDE INTERCOSTAL CRACKED AT WL 185. BS 178 FORWARD PRESJun 11, 2001 · N127NJ · Boeing 7372B7 · Fuselage Main, BulkheadSDR USAA010622Skin · crackedCLT - FOUND FUSELAGE SKIN HAS APPROXIMATELY .5 INCH CRACK, BS 380, FUSELAGE BELLY S-28L, COOLING DUCT CUTOUT. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-04. (M)Jun 8, 2001 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA010616Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED APPROXIMATELY .25 INCH, BS 327 STRINGER 17R, FORWARD GALLEY SERVICE DOOR CUTOUT, AFT LOWER CORNER. DAMAGE REMOVED, INSTALLED REPAIR FILLER WITH DOUBLER AND TRIPLER PER SRM 53-30-03, FIG 26. (M)Jun 5, 2001 · N284AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB01162Battery Pack · dischargedBDL - MAINTENANCE FOUND THE MID-LEVEL EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Jun 5, 2001 · N287AU · Boeing 7372B7 · Emergency LightingSDR USAASB01160Flap · jammedEWR - FLT 2671 - DURING DESCENT, AIRCRAFT ENCOUNTERED TRAILING EDGE FLAP ASYMMETRY. CAPTAIN REQUESTED TO LAND AT EWR INSTEAD OF LGA DUE TO THE HIGHER LANDING SPEEDS FOR THIS TYPE OF FAILURE. AFTER LANDING AT EWR, WITHOUT INCIDENT, CAPTAIN REPORTED THAT THE LJun 4, 2001 · N269AU · Boeing 7372B7 · Trailing Edge Flap Control SystemSDR USAASB01154Fuse · blownTPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE FUSE IN THE POWER SUPPLY BLOWN. REMOVED AND REPLACED FUSE. OPS CHECK GOOD. (M)Jun 2, 2001 · N272AU · Boeing 7372B7 · Emergency LightingSDR USAASB01155Charger · failedLGA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE OVERWING EMERGENCY EXIT LOCATOR LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK M1052 (P/N 9008-3-5A). OPS CHECK GOOD. (M)Jun 2, 2001 · N273AU · Boeing 7372B7 · Emergency LightingSDR USAA010598Skin · dentedCLT - FOUND BULKHEAD SKIN DENTED 1 INCH BY .5 INCH BY .005 INCH DEEP, BS 1016 PRESSURE BULKHEAD, LBL 10 INCHES FROM CENTER. INSTALLED DOUBLER PER SRM 53-10-4 FIG 3. (M)Jun 1, 2001 · N284AU · Boeing 7372B7 · Fuselage Main, BulkheadSDR USAA010599Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 1 INCH AREA, BS 360 LEFT. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 51-10-1. (M)Jun 1, 2001 · N284AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA010600Fitting · crackedCLT - FOUND LEFT MLG BEAM FITTING CRACKED .125 INCH, .25 INCH FROM FASTENER HOLE TO EDGER ABOVE CUTOUT. TEMPORARY REPAIR PER TYPICAL REPAIR 57-40-10 PER EA 69608. (M)Jun 1, 2001 · N284AU · Boeing 7372B7 · Main Landing GearSDR USAA010601Splice · crackedCLT - FOUND STRINGER SPLICE HAS 1 INCH CRACK, BS 360 STRINGER 15L. REMOVED DAMAGE SPLICE, INSTALLED NEW SPLICE PER SRM 51-10-1. (M)Jun 1, 2001 · N284AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA010602Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 747, STRINGER 7L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)Jun 1, 2001 · N284AU · Boeing 7372B7 · Nacelle/Pylon StructureSDR USAA010603Frame · crackedCLT - FOUND FRAME CRACKED .0625 INCH, BS 767, STRINGER 13L. ENLARGED FASTENER HOLE TO .25 INCH, INSTALLED HI-LOCK PER SRM 51-10-02. (M)Jun 1, 2001 · N284AU · Boeing 7372B7 · Fuselage Structure (General)SDR USAA010595Hinge Fitting · corrodedCLT - FOUND STAB HINGE FITTING CORRODED APPROXIMATELY 1 SQUARE INCH AREA, RIGHT CENTER SECTION, REAR SPAR, LOWER ATTACH POINT LUG. CORROSION REMOVED, LUG REWORKED PER EA 69577. (M)May 31, 2001 · N284AU · Boeing 7372B7 · Horizontal Stabilizer StructureSDR USAA010596Frame · corrodedCLT - FOUND FRAME CORRODED APPROXIMATELY 4 SQUARE INCH AREA, BS 847, ABOVE STRINGER 25R. REMOVED DAMAGED SECTION, REPLACED SECTION PER BOEING DRAWING NR 65C35243 AND EA69063. (M)May 31, 2001 · N284AU · Boeing 7372B7 · Nacelle/Pylon StructureSDR USAA010594Hinge Fitting · corrodedCLT - FOUND STAB HINGE FITTING CORRODED APPROXIMATELY 1.5 SQUARE INCH AREA, RT CENTER SECTION FORWARD LOWER ATTACH INBOARD CLEVIS, OUTBOARD FACE. CORROSION REMOVED, LUG REWORKED PER EA 69577. (M)May 31, 2001 · N284AU · Boeing 7372B7 · Horizontal Stabilizer StructureSDR USAA010589Hinge Fitting · corrodedCLT - FOUND STABILIZER HINGE FITTING CORRODED 1 SQUARE INCH, LEFT HORIZ STAB REAR SPAR, LOWER ATTACH POINT LUG. REWORKED PER EA 69633. (M)May 31, 2001 · N284AU · Boeing 7372B7 · Horizontal Stabilizer Structure
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