N219US, cancelled Jul 19, 2000

Service difficulty reports · 90

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N219US' AND deregistration_id = 'N219US-2000-07-19'
  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 P2EA99354Floorbeam · corrodedSJO - C-CHECK, FLOORBEAM WEB CORRODED AT BS 259.5, FROM WL 208.5 TO WL 206, BETWEEN LBL 13 INCH TO RBL 13 INCH. DEFECT SIZE, LENGTH 16 INCHES, WIDTH 5 INCHES. REPAIRED FLOORBEAM WEB AT BS 259.5 BETWEEN LBL 17 INCH AND RBL 14.5 INCH FROM WL 208.5 TO WL 193. Dec 3, 1999 · N219US · Boeing 737281 · Fuselage Main, Floor BeamSDR P2EA99351Floorbeam · corrodedSJO - C-CHECK, FLOORBEAM CORROSION AT BS 259.5, WL 208.5, BETWEEN LBL 20 AND RBL 15 INCHES. DEFECT SIZE, LENGTH 14 INCHES, WIDTH 4 INCHES. REPAIRED FLOORBEAM ANGLE AT BS 259 FROM LBL 23 INCHES TO RBL 21.5 INCHES WL 208. ALSO, REPLACED FLOOR BEAM UPPER ANGLEDec 3, 1999 · N219US · Boeing 737281 · Fuselage Main, Floor BeamSDR P2EA99350Angle · corrodedSJO - C-CHECK, FLOOR SUPPORT ANGLE CORRODED AT BS 270, WL 208.5, BETWEEN RBL 17 INCHE LBL 10 INCH. DEFECT SIZE, LENGTH 10 INCH, WIDTH 2 INCH. REPAIRED FLOOR SUPPORT ANGLE AT BS 270, WL 208.5, BETWEEN LBL 54 INCH TO RBL 25.5 INCH PER COOPESA EO COO-3-53-714-9Dec 3, 1999 · N219US · Boeing 737281 · Fuselage Miscellaneous StructureSDR P2EA99342Skin · delaminatedSJO - C-CHECK, LEFT AC BAY DOOR DELAMINATED. REPAIRED LEFT AC BAY DOOR PER EO COO-CMP-3-53-704-99 DATED DECEMBER 4, 1999. (M)Dec 3, 1999 · N219US · Boeing 737281 · Air Conditioning DoorsSDR P2EA99335Bulkhead · crackedSJO - C-CHECK, WEB CRACKED AT BS 178, LBL 10 INCHES, WL 235. DEFECT SIZE, LENGTH .375 INCH. REPAIRED BULKHEAD WEB AT BS 178 FROM LBL 7 TO LBL 17.5, BETWEEN WL 240 AND WL 230.5 PER SRM 53-10-11 FIG 1. (M)Dec 2, 1999 · N219US · Boeing 737281 · Fuselage Main, BulkheadSDR P2EA99352Rib · crackedSJO - C-CHECK ITEM, SUPPORT RIB CRACKED AT RT WING SLAT STATION 25. DEFECT SIZE, LENGTH .75 INCH. REPLACED SLAT TRACK SUPPORT RIB AT SLAT STATION 25 PER SRM 51-10-1 PAGE 5. (M)Dec 1, 1999 · N219US · Boeing 737281 · Wing, Rib/BulkheadSDR P2EA99345Skin · dentedSJO - C-CHECK, E/E DOOR HAS A DENT OUT OF LIMITS, DEFECT SIZE, LENGTH 1.75 INCH, WIDTH 1.5 INCH, DEPTH .045 INCH. REPLACED DOOR SKIN PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M)Dec 1, 1999 · N219US · Boeing 737281 · Electrical/Electronic Compartment DoorsSDR P2EA99355Skin · crackedSJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 727 TO BS 727A BETWEEN STRINGER 14 RT AND 16 RT. DEFECT SIZE LENGTH 1.75 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 727 TO BS 727A PLUS 9.9, BETWEEN STRINGER 16 AND 20 RT PER BOEING FAX COO-SJO-990060 DATED DECENov 30, 1999 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA99336Skin · crackedSJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 268 TO BS 277, BETWEEN STRINGER 15 RT AND 16 RT. DEFECT SIZE 1 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 263.5 TO BS 280, BETWEEN STRINGER 14 RT AND STRINGER 17 RT PER SRM 53-30-3, FIG 17. (M)Nov 30, 1999 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA99311Transmitter · inoperativeFLT 588 - MCI - ABORTED TAKEOFF, NO EMERGENCY DECLARED. DURING TAKEOFF ROLL, NR 2 EPR GAUGE READS ZERO. REPLACED NR 2 EPR TRANSMITTER AND NR 2 EPR INDICATOR PER MM 77-11-21, OPS CHECK OK. (M)Nov 12, 1999 · N219US · Boeing 737281 · Engine Pressure Ratio (EPR)SDR P2EA99253Skin · crackedSJO - C-CHECK, LEFT RAM DOOR INNER SKIN CRACKED, DEFECT SIZE, LENGTH 3 INCHES AND WIDTH 1 INCH. REPAIRED RAM DOOR INTERNAL SKIN PER COOPESA EO COO-3-52-708-99 DATED DECEMBER 4, 1999. (M)Oct 5, 1999 · N219US · Boeing 737281 · Air Distribution SystemSDR P2EA99220Door · missingNSP - FLT 707 - THIS IS A SUPPLEMENTAL/CLOSING ACTION FOR MRR 99220. ON WALK-AROUND INSPECTION AFTER FLIGHT MAINTENANCE, CREW DISCOVERED THE CENTER BOOST PUMP DOOR P/N 65-45487-7 MISSING. DEFERRED PER CDL 57-30-4. REQUESTED PANEL. REF: DEFERRED ITEM C2199Jul 20, 1999 · N219US · Boeing 737281 · Wing, Plate/SkinSDR P2EA99195Pump · leakingPIT - FLT 588 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. TOTAL LOSS OF SYSTEM 'A' HYDRAULICS. FOUND NR 2 ENGINE SYSTEM 'A' HDYRAULIC PUMP SHAFT SEAL BLOWN. REPLACED NR 2 (SYSTEM 'A') ENGINE HYDRAULIC PUMP PER MM 29-11-31A. OPERATION AND LEAK CHECKS OK. May 25, 1999 · N219US · Boeing 737281 · Hydraulic Pump (Electric/Engine), MainSDR P2EA99090Mechanism · wornMCI - FLT 819 - RETRACTING FLAPS FROM 5 TO 1 DEGREE OUT OF MDW, FELT HEAVY FLUTTER. GOING FROM FLAPS 1 TO 5 ON LANDING AT MCI FELT MINOR FLUTTER. LANDING AT MCI, SELECTED FLAPS 25 AND GAUGE INDICATED 15. SELECTED FLAPS 30 AND GAUGE INDICATED BETWEEN 25 AND 30Mar 12, 1999 · N219US · Boeing 737281 · Trailing Edge Flap Control SystemSDR P2EA99001Valve · failedMSP - FLT 404 - DURAL BLEED INDICATION DURING TAKEOFF. ABORTED TAKEOFF AT 70 KNOTS, RETURNED TO GATE. DEFERRED PER MEL 36-6, CI M219725 ASSIGNED. FEF CI M219725. DUAL BLEED INDICATION INOPERATIVE. REPLACED APU LOAD CONTROL VALVE PER MM 49-52-11A, CLEARED Jan 7, 1999 · N219US · Boeing 737281 · APU Bleed Air SystemSDR P2EA98312Window · crackedMCI - FLT 586 - THE AIRCRAFT DEPARTED MCI AND 35 MINUTES INTO FLIGHT THE FIRST OFFICERS SLIDING WINDOW CRACKED. THE AIRCRAFT RETURNED TO MCI WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE CRACKED F/O WINDOW AND WINDOW HEAT CONTROL UNIT. (M)Dec 26, 1998 · N219US · Boeing 737281 · Flight Compartment WindowsSDR P2EA98311Skin · crackedSJO - NR 1 THRUST REVERSER LOWER BUCKET EXTERNAL SKIN CRACKED, DEFECT SIZE LENGTH 2.75 INCH. REPAIRED THRUST REVERSER PER COOPESA EO COO-3-78-754-98 DATED DEC 17, 1998. (M)Dec 15, 1998 · N219US · Boeing 737281 · Engine Thrust ReverserSDR P2EA98305Skin · damagedSJO - PROVISIONAL REPAIR AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED FUSELAGE SKIN SECTION FROM BS 299 TO BS 305 BETWEEN STRINGER 12 RT AND STRINGER 14 RT PER SRM 53-30-3 FIG 31, DETAIL III. (M)Dec 8, 1998 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA98296Slat · delaminatedSJO - NR 5 SLAT DELAMINATED, DEFECT SIZE TOTAL 400 SQ INCH. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-719-98 DATED DEC 2, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)Dec 1, 1998 · N219US · Boeing 737281 · SpoilersSDR P2EA98307Skin · delaminatedSJO - NR 5 SPOILER DELAMINATED, DEFECT SIZE TOTAL 234 SQUARE INCH. REPAIRED NR 5 SPOILER PER COOPESA EO C00-3-57-709-98 DATED NOV 30, 1998. (M)Nov 27, 1998 · N219US · Boeing 737281 · SpoilersSDR P2EA98306Skin · delaminatedSJO - NR 2 SPOILER DELAMINATED, DEFECT SIZE TOTAL 6 SQUARE INCH. REPAIRED NR 2 SPOILER PER COOPESA EO COO-3-57-710-98 DATED NOV 30, 1998. (M)Nov 27, 1998 · N219US · Boeing 737281 · SpoilersSDR P2EA98303Skin · delaminatedSJO - NR 7 SPOILER DELAMINATED, DEFECT SIZE TOTAL 325 SQUARE INCH. REPAIRED NR 7 SPOILER PER COOPESA EO COO-3-57-711-98 DATED NOV 30, 1998. (M)Nov 27, 1998 · N219US · Boeing 737281 · SpoilersSDR P2EA98298Spoiler · delaminatedSJO - NR 8 SPOILER DELAMINATED, DEFECT SIZE TOTAL 320 SQ IN. REPAIRED NR 8 SPOILER PER COOPESA EO C00-3-57-713-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)Nov 27, 1998 · N219US · Boeing 737281 · SpoilersSDR P2EA98295Spoiler · delaminatedSJO - NR 6 SPOILER DELAMINATED, DEFECT SIZE TOTAL 160 SQ INCH. REPAIRED NR 6 SPOILER PER COOPESA EO COO-3-57-712-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)Nov 27, 1998 · N219US · Boeing 737281 · SpoilersSDR P2EA98294Skin · damagedSJO - FUSELAGE SKIN DOUBLER MISSING MATERIAL AT BS 178, WL 243, BETWEEN LBL 2 INCH AND LBL 7 INCH. REPLACED WINDOW CENTER POST DOUBLER AT BS 178, SL 243, BETWEEN LBL 7 INCH AND RBL PER BOEING SERVICE BULLETIN 737-53-1059 REV 1, SECTION III, FIG 2 DATED MAY 17Nov 22, 1998 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA98267Stringer · crackedSJO - STRINGER 15 LEFT CRACKED AT BS 360, DEFECT SIZE LENGTH .5 INCH. REPLACED STRINGER 15 LEFT SECTION FROM BS 348 TO BS 367 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Nov 21, 1998 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA98266Stringer · crackedSJO - STRINGER 14 LEFT CRACKED AT BS 360, DEFECT SIZE LENGTH .5 INCH. REPLACED FUSELAGE STRINGER 14 LT SECTION FROM BS 367 TO BS 348 PR SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Nov 21, 1998 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA98265Frame · crackedSJO - FRAME WEB CRACKED AT BS 303.9, BETWEEN STRINGER 16L AND STRINGER 17L, DEFECT SIZE, LENGTH 1 INCH. REPAIRED FUSELAGE WEB SECTION AT BS 303.9, BETWEEN STRINGER 15 LEFT AND B STRINGER 18 LT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Nov 21, 1998 · N219US · Boeing 737281 · Fuselage Main, FrameSDR P2EA98293Stringer · corrodedSJO - FOUND CORROSION AT BS 727A, STRINGER 22 LEFT, LOWER CHORD, DEFECT SIZE LENGTH 2.5 INCH WIDTH 1 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 727 PLUS 11 INCH AND BS 727A PLUS 8 INCH, BETWEEN STRINGER 21 LEFT AND STRINGER 23 LEFT PER SRM 53-30-3, FIG 6. Nov 20, 1998 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA98273Skin · corrodedFUSELAGE SKIN CORRODED BETWEEN BS 907 AND BS 967, BETWEEN STRINGER 4 RT AND STRINER 5 RT. REPLACED FUSELAGE SKIN SECTION FROM BS 902.5 TO BS 914, BETWEEN STRINGER 4 RT AND STRINGER 5 RT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. REMOVED CORROSION FROM BS 907 TONov 20, 1998 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA98268Beam · crackedSJO - FORWARD SERVICE DOOR NR 7 BEAM CRACKED, DEFECT SIZE LENGTH .5 INCH. REPAIRED FUSELAGE SKIN FORWARD ENTRY DOOR BEAM NR 7 BETWEEN BS 302 AND BS 309 PER SRM 51-40-3 FIG 1. (M)Nov 20, 1998 · N219US · Boeing 737281 · Service DoorsSDR P2EA98264Frame · crackedSJO - FRAME CRACKED AT BS 344, BETWEEN STRINGER 23 RT AND STRINGER 24 RT, DEFECT SIZE LENGTH 6.75 INCH. REPLACED FRAME SECTION AT BS 344, BETWEEN STRINGER 21 RT AND STRINGER 27 RT PER 51-10-1 PAGE 5 AND SRM 51-30-2. REPAIRED FUSELAGE FRAME ANGLE SECTION AT BNov 20, 1998 · N219US · Boeing 737281 · Fuselage Main, FrameSDR P2EA98301Seat Track · crackedSJO - SEAT TRACK CRACKED AT BS 709, RBL 25 INCHES, WL 203.1, DEFECT SIZE LENGTH .625 INCH. REPAIRED FLOORBEAM SECTION FROM BS 698 AND BS 717, RBL 25 INCHES PER BOEING SERVICE BULLETIN 737-57-1210 DATED APRIL 4, 1991 SECTION III FIG 5 AND BOEING FAX COO-SJO-98Nov 19, 1998 · N219US · Boeing 737281 · Fuselage, Seat/Cargo Attach FittingsSDR P2EA98299Seat Track · crackedSJO - SEAT TRACK LOWER CHORD CRACKED AT FROM BS 663.75 TO BS 690 AT RBL 24.5, DEFECT SIZE LENGTH .563. REPAIRED FLOORBEAM UPPER CHORD BETWEEN BS 660 AND BS 682, LBL 24.82 PER BOEING INSTRUCTION LIST OF DATE INCLUDED ON FAA FOR 8110-3 AND COOPESA EO COO-3-57-6Nov 19, 1998 · N219US · Boeing 737281 · Fuselage, Seat/Cargo Attach FittingsSDR P2EA98291Angle · crackedSJO - ANGLE CRACKED AT BS 559, RBL 46, WL 205 DEFECT SIZE LENGTH .4375. REPLACED FUSELAGE LOWER CHORD AT BS 559, WL 204, BETWEEN RBL 46 INCHES AND RBL 70 INCHES PER BOEING SERVICE BULLETIN 737-53-1061, REV 4, SECTION 111 FIG 2 DATED JULY 16, 1992. (M)Nov 19, 1998 · N219US · Boeing 737281 · Fuselage Miscellaneous StructureSDR P2EA98290Floorbeam · crackedSJO - FLOORBEAM CRACKED AT BS 578, RBL 50, WL 206, DEFECT SIZE .5 INCH. REPAIRED FLOORBEAM WEB AT BS 578, BETWEEN RBL 45 INCHES TO RBL 70 INCHES, FROM WL 208 TO WL 204 PER SRM 51-30-2 AND 51-10-1 PAGE 5. (M)Nov 19, 1998 · N219US · Boeing 737281 · Fuselage Main, Floor BeamSDR P2EA98280Web · crackedSJO - WEB CRACKED AT BS 663.75, RBL 0, WL 206. DEFECT SIZE LENGTH 1.5 INCH. REPAIRED CENTER WING BOX, FLOORBEAM UPPER CHORD BETWEEN BS 650 AND BS 675, BL 0 PER BOEING SERVICE BULLETIN 737-57-1210 DATED APRIL 4, 1991, SECTION III FIG 4. (M)Nov 19, 1998 · N219US · Boeing 737281 · Wing Miscellaneous StructureSDR P2EA98274Rib · crackedSJO - RIB CRACKED AT RIGHT WING FUEL TANK WBL 135.5, DEFECT SIZE LENGTH 1.125 INCH. REPAIRED RIGHT WING RIB LOWER CHORD AT WBL 135.5, BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SERVICE BULLETIN 737-57-1186 DATED 4-13-98, SECTION III, PART 3 FIG 3. (M)Nov 19, 1998 · N219US · Boeing 737281 · Wing, Rib/BulkheadSDR P2EA98270Seat Track · crackedSJO - SEAT TRACK WEB CRACKED AT BS 639, RBL 45.5, WL 201, DEFECT SIZE LENGTH 1 INCH. REPAIRED FUSELAGE WEB SECTION FROM BS 636 TO BS 642, FROM WL 204 TO WL 199.5, RBL 45.5 PER 51-40-2 FIG 1 PAGE 3. (M)Nov 19, 1998 · N219US · Boeing 737281 · Fuselage, Seat/Cargo Attach FittingsSDR P2EA98269Stringer · crackedSJO - STRINGER 5 LEFT SPLICE CRACKED AT BS 360, DEFECT SIZE LENGTH .75 INCH. REPLACED FUSELAGE STRINGER 5 LEFT SPLICE FROM 348.2 TO BS 367 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Nov 19, 1998 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA98260Angle · crackedSJO - RIGHT EMERGENCY EXIT DOOR FRAME ANGLE CRACKED AT FORWARD SECTION, DEFECT SIZE LENGTH .375 INCH. REPLACED RIGHT EMERGENCY EXIT DOOR FORWARD FRAME ANGLE AT BS 622 PER SRM 51-10-01 PAGE 1 AND SRM 51-30-2. (M)Nov 19, 1998 · N219US · Boeing 737281 · Emergency ExitsSDR P2EA98258Skin · damagedSJO - LEFT WING OUTBOARD FOREFLAP LEADING EDGE SKIN REPAIR DOUBLER WORN. REPAIRED FOREFLAP LEADING EDGE SKIN BETWEEN WSL 493 AND WSL 488 PER SRM 57-50-4 FIG 1. (M)Nov 19, 1998 · N219US · Boeing 737281 · Wing, Plate/SkinSDR SIMA98257Skin · crackedSJO - FORWARD RIGHT UPPER HINGE CUTOUT CRACKED AT BS 310, DEFECT SIZE LENGTH .50 INCH. REPAIRED FORWARD RIGHT SERVICE DOOR SKIN SECTION BETWEEN BS 308 AND BS 316, BETWEEN BEAM NR 3 AND BEAM NR 4 PER SRM 52-00-03 FIG 3. (M)Nov 18, 1998 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA98308Skin · crackedSJO - INTERNAL DOUBLER CRACKED FORWARD ENTRY DOORWAY UPPER HINGE CUTOUT, DEFECT SIZE LENGTH 1.937 INCH. REPAIRED FUSELAGE SKIN FROM BS 297 TO BS 305 BETWEEN STRINGER 9 LEFT AND STRINGER 11 LT PER COOPESA EO C00-3-53-723-98 DATED DEC 4, 1998 AND BOEING FAX COONov 18, 1998 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA98302Web · crackedSJO - WEB CRACKED AT BS 253, LBL 8 INCHES DEFECT SIZE, LENGTH .375 INCH. REPAIRED FUSELAGE WEB SECTION BETWEEN BS 232 AND BS 257, WL 190 FROM BL 0 TO LBL 18 INCHES PER COOPESA EO COO-3-53-717-98 DATED DEC 2, 1998 AND BOEING FAX COO-SJO 98-1021RR DATED DEC 1, Nov 18, 1998 · N219US · Boeing 737281 · Fuselage Miscellaneous StructureSDR P2EA98300Frame · crackedSJO - AFT ENTRY DOOR LOWER PAN SECTION CRACKED. DEFECT SIZE LENGTH 1.125 INCH. REPLACED AFT ENTRY DOOR FRAME AT BS 949 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Nov 18, 1998 · N219US · Boeing 737281 · Fuselage Main, FrameSDR P2EA98297Skin · canningSJO - AFT CARGO DOOR DENTED AND OL CANNED, DEFECT SIZE WIDTH 2.125 INCH DEPTH .060. REPLACED AFT CARGO DOOR OUTER SKIN BETWEEN BS 839 AND BS 887 PER SRM 51-10-1 PAGE 5 AND 51-20-2. (M)Nov 18, 1998 · N219US · Boeing 737281 · Cargo/Baggage DoorsSDR P2EA98292Stringer · corrodedSJO - STRINGER 22 LEFT CORRODED BETWEEN BS 727 AND BS 727A, DEFECT SIZE LENGTH 3 INCH WIDTH .75 INCH. REPAIRED STRINGER 22 LEFT BETWEEN BS 727 AND BS 727A PLUS 13 INCHS PER SRM 53-10-3 FIG 1, SHEET 7. (M)Nov 18, 1998 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA98288Skin · crackedSJO - INTERNAL DOUBLER CRACKED AT THE AFT SERVICE DOORWAY LOWER HINGE CUTOUT, DEFECT SIZE LENGTH .75 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 939 TO BS 953, BETWEEN STRINGER 13 RT AND STRINGER 14 RT PER COOPESA EO COO-3-53-715-98 DATED DEC 2, 1998 AND BOENov 18, 1998 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA98281Frame · crackedSJO - FRAME CRACKED AT BS 578, WL 207, LBL 65, DEFECT SIZE LENGTH 5 INCH. REPLACED FUSELAGE FRAME SECTION AT BS 578, BETWEEN STRINGER 12 LEFT AND STRINGER 18 LEFT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Nov 18, 1998 · N219US · Boeing 737281 · Fuselage Main, Frame
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