# Service difficulty reports: N603DJ, cancelled Mar 30, 2001 A list on [N603DJ, cancelled Mar 30, 2001](https://openairdocs.org/deregistered/N603DJ-2001-03-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 4 · 152 reports - [SDR P2E00315](https://openairdocs.org/sdr/P2E00315.md): Lap Joint · cracked · Oct 26, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LOWER ROW OF LONGITUDINAL LAP JOINT AT BS727 STR 10L FASTENER HOLE WITH CRACK L=0.125 W=0.032 INCH. REPAIRED THE EXTERIOR FUSELAGE LOWER ROW OF LONGITUDINAL LAP JOINT AT BS 727 10L FASTENER HOLE - [SDR COOSDR000016](https://openairdocs.org/sdr/COOSDR000016.md): Lap Joint · cracked · Oct 26, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > EXTERIOR FUSELAGE AT BS 727A PLUS 10, STR 10 LT LAP JOINT AREA, LOWER SKIN WITH HOLE CRACKED. POSSIBLE CAUSE OF CRACK WAS SKIN FATIGUE. (X) - [SDR P2EA00320](https://openairdocs.org/sdr/P2EA00320.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > DURING SPECIAL INSPECTION FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS880-890 STR 25R WITH LEVEL 2 CORROSION L=2.00 W=2.00 D=0.008. REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS 880-890 STR 25R IAW BOEING S/B 737-53-A1224 PART III PAR C DATED 8-17-2000 AND S - [SDR P2EA00319](https://openairdocs.org/sdr/P2EA00319.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS893-895 STR 20L WITH LEVEL 2 CORROSION L-2.00 W=2.00 D=0.008. REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS 893-895 STR 20L IAW BOEING S/B 737-53-A1224 PART III PAR C DATED 8-17-200 - [SDR P2EA00318](https://openairdocs.org/sdr/P2EA00318.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS747-749 STR 25L WITH LEVEL 3 CORROSION L-2.00 W=2.00 D=0.009. REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS747-749 STR 25L IAW BOEING S/B 737-53-A1224 PART III PAR C DATED 8-17-2000 - [SDR P2EA00317](https://openairdocs.org/sdr/P2EA00317.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS 747-751 STR 25 RT WITH LEVEL 2 CORROSION L=2.00 W=2.00 D=0.009. REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS747-751 STR 25R IAW BOEING S/B 737-53-A1224 PART III PAR C DATED 8-17- - [SDR P2EA00316](https://openairdocs.org/sdr/P2EA00316.md): Lap Joint · cracked · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE UPPER ROW OF LONGITUDINAL LAP JOINT AT BS 787 STR 14L FASTENER HOLE WITH CRACK L=O.125 W=0.002. REPAIRED THE EXTERIOR FUSELAGE UPPER ROW OF LONGITUDINAL LAP JOINT AT BS 787 14L FASTENER HOLE IAW BO - [SDR P2EA00321](https://openairdocs.org/sdr/P2EA00321.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS953-961 STR 4L WITH LEVEL 2 CORROSION L=23.00 IN, W=3.0-00 IN, D=0.009 IN REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS953-961 STR 4L IAW BOEING S/B 737-53-A1224 PART III PAR C DATED - [SDR COOSDR000022](https://openairdocs.org/sdr/COOSDR000022.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > FUSELAGE SKIN FROM BS 880 TO BS 890, STR 25RT, LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CRACK WAS SKIN CORROSION. (X) - [SDR COOSDR000021](https://openairdocs.org/sdr/COOSDR000021.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > FUSELAGE SKIN FROM BS 893 TO BS 895, STR 20 LT - LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CRACK WAS SKIN FATIGUE. (X) - [SDR COOSDR000020](https://openairdocs.org/sdr/COOSDR000020.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > FUSELAGE SKIN FROM BS 747 TO BS 751, STR 25 RT - LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CORROSION WAS SKIN FATIGUE. (X) - [SDR COOSDR000019](https://openairdocs.org/sdr/COOSDR000019.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > FUSELAGE SKIN FROM BS 747 TO BS 749, STR 25 LT, LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF THE CORROSION WAS SKIN FATIGUE. (X) - [SDR COOSDR000018](https://openairdocs.org/sdr/COOSDR000018.md): Lap Joint · cracked · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > FUSELAGE SKIN AT BS 787, STR 14 LT - LAP JOINT AREA, UPPER ROW WITH HOLE CRACKED. POSSIBLE CAUSE OF THE CORROSION WAS SKIN FATIGUE. (X) - [SDR COOSDR000017](https://openairdocs.org/sdr/COOSDR000017.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > FUSELAGE SKIN FROM BS 930 TO BS 961 STR 4 LT - LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF THE CORROSION WAS SKIN FATIGUE. (X) - [SDR P2EA00312](https://openairdocs.org/sdr/P2EA00312.md): Skin · cracked · Oct 24, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE SKIN FROM BS482-484 BETWEEN STR 9L AND 10L WITH CRACK L=0.50 W=0.002. REPAIRED THE EXTERIOR FUSELAGE SKIN FROM BS482-484 BETWEEN STR 9L AND 10L IAW BOEING SRM 53-30-3 FIG 9 - [SDR P2EA00226](https://openairdocs.org/sdr/P2EA00226.md): Structure · cracked · Jul 11, 2000 · N603DJ · Boeing 737222 · Passenger/Crew Doors > MCI - DURING MAINTENANCE, L1 DOOR CRACKED AT BS 341, WL 284.75. REPAIRED CRACK FROM BS 339 TO BS 344 AND FROM WL 284.75 TO 279.75 IAW SRM 52-00-3 FIG 2. (M) - [SDR P2EA00210](https://openairdocs.org/sdr/P2EA00210.md): Actuator · unserviceable · Jun 14, 2000 · N603DJ · Boeing 737222 · Drag Control Actuator > FLT 414 - MDW - FOUND LOST A SYSTEM HYDRAULIC PRESSURE AND QUANTITY WHILE TAXING TO GATE. REMOVED AND REPLACED THE NR 1 GROUND SPOILER ACTUATOR PER BOEING MM 27-62-10. LEAK CHECK AND OPERATIONAL CHECK NORMAL. (M) - [SDR P2EA00119](https://openairdocs.org/sdr/P2EA00119.md): Fitting · stripped · May 10, 2000 · N603DJ · Boeing 737222 · Turbine Engine Reduction Gear > PIT - FLT 732 - ON SHORT FINAL, NR 1 ENGINE OIL QUANTITY WENT TO ZERO. OIL PRESSURE FLUCTUATED 35 - 45 PSI, OIL PRESSURE LIGHT FLICKERED ON. UPON LANDING, OIL QUANTITY WAS ZERO, OIL PRESSURE WAS 20 SPI, OIL LIGHT WAS ON. CREW SHUT DOWN NR 1 ENGINE. FOUND L - [SDR P2EA00067](https://openairdocs.org/sdr/P2EA00067.md): Hydraulic Line · leaking · Mar 11, 2000 · N603DJ · Boeing 737222 · Hydraulic System, Main > PIT - FLT 701 - AIR RETURN TO PIT, EMERGENCY DECLARED, LANDING UNEVENTFUL. LOST A SYSTEM HYDRAULIC QUANTITY AND PRESSURE IN FLIGHT. REPLACED RIGHT WING SPOILER SYSTEM HYDRAULIC RETURN LINE WITH TEMPORARY FLEX LINE. SERVICED A HYDRAULIC SYSTEM PER MM 12-12-0 - [SDR P2EA00061](https://openairdocs.org/sdr/P2EA00061.md): Spar · corroded · Feb 24, 2000 · N603DJ · Boeing 737222 · Wing Spar > SJO - DURING Q-CHECK, FOUND CORROSION ON RIGHT WING FRONT SPAR UPPER CHORD AT FS 562. REPAIRED RIGHT WING SPAR UPPER CHORD BETWEEN FS 544.5 AND FS 588 IAW COOPESA EO COO-3-57-088-00 DATED 2/18/2000. (M) - [SDR P2EA00059](https://openairdocs.org/sdr/P2EA00059.md): Skin · canning · Feb 24, 2000 · N603DJ · Boeing 737222 · Passenger/Crew Doors > SJO - DURING Q-CHECK, FOUND R1 DOOR SKIN AT HANDLE CUT OUT IS OIL CANNED. REPAIRED DOOR BETWEEN NR 4 BEAM AND NR 5 BEAM IAW SRM 52-00-3, FIG 6. (M) - [SDR P2EA00058](https://openairdocs.org/sdr/P2EA00058.md): Skin · cracked · Feb 21, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > SJO - DURING Q-CHECK, FOUND R1 DOOR LOWER HINGE CUTOUT SECTION CRACKED. REPAIRED CUTOUT FROM BS 288.5 TO BS 304.5 BETWEEN 12L AND 14L IAW SRM 53-30-3, FIG 31. (M) - [SDR P2EA00057](https://openairdocs.org/sdr/P2EA00057.md): Thrust Reverser · out of adj · Feb 12, 2000 · N603DJ · Boeing 737222 · Engine Thrust Reverser > SJO - DURING Q-CHECK, NR 1 ENGINE THRUST REVERSER BUMPER DOUBLER REQUIRES ADJUSTMENT. FABRICATED BUMPER DOUBLER IAW COOPESA EO COO-3-78-097-00, DATED 02-21-2000. REMOVED AND REPLACED DOUBLER IAW SRM 51-10-1. (M) - [SDR P2EA00054](https://openairdocs.org/sdr/P2EA00054.md): Skin · delaminated · Feb 5, 2000 · N603DJ · Boeing 737222 · Ailerons > SJO - DURING Q-CHECK, LEFT WING AILERON INBOARD TOP SECTION DELAMINATED. REPAIRED AILERON IAW COOPESA EO COO-CMP-3-57-072-00, DATED 2/7/2000. (M) - [SDR P2EA00053](https://openairdocs.org/sdr/P2EA00053.md): Beam · cracked · Feb 5, 2000 · N603DJ · Boeing 737222 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, STUD BEAM WEB CRACKED AT BS 639. REPAIRED STUD BEAM WEB AT BS 639, BETWEEN LBL 46 AND LBL 56.5 AND FROM WL 200 TO WL 208 IAW SB 737-53-1061 REV 4 PART III FIG 2 DATED JULY 16, 1992. (M) - [SDR P2EA00051](https://openairdocs.org/sdr/P2EA00051.md): Fitting · misdrilled · Feb 4, 2000 · N603DJ · Boeing 737222 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, NOSE LANDING GEAR LEFT TRUNNION FITTING DRILLED. REPAIRED TRUNNION FITTING IAW COOPESA EO COO-3-53-081-00, DATED 02/10/2000. (M) - [SDR P2EA00038](https://openairdocs.org/sdr/P2EA00038.md): Stringer · corroded · Feb 4, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Longeron/Stringer > SJO - DURING Q-CHECK, CORROSION ON STRINGER 25R AT BS 950. REPAIRED STRINGER 25R FROM BS 950 TO BS 1003 IAW SRM 53-10-2 FIG 1. (M) - [SDR P2EA00037](https://openairdocs.org/sdr/P2EA00037.md): Floorbeam · corroded · Feb 4, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, CORROSION ON VERTICAL STIFFENER (FLOORBEAM) AT BS 286.5 LBL 18 FROM WL 154 TO WL 194. FABRICATED VERTICAL STIFFENER IAW COOPESA EO NR COO-3-53-074-00 AND SRM 51-10-0 PAGE 5. REMOVED AND REPLACED VERTICAL STIFFENER IAW SRM 51-30-2. (M) - [SDR P2EA00026](https://openairdocs.org/sdr/P2EA00026.md): Stringer · corroded · Jan 30, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Longeron/Stringer > SJO - DURING Q-CHECK, FOUND CORROSION BETWEEN BS 360 AND BS 380 AT STRINGER 21L. REPAIRED STRINGER 21L, BETWEEN BS 360 AND BS 395 IAW SRM 53-10-3 FIG 1. (M) - [SDR P2EA00050](https://openairdocs.org/sdr/P2EA00050.md): Stringer · corroded · Jan 29, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Longeron/Stringer > DURING Q-CHECK, FOUND CORROSION ON STRINGER 28L AT BS 328. REPLACED STRINGER 28L IW SRM 51-30-2. (M) - [SDR P2EA00049](https://openairdocs.org/sdr/P2EA00049.md): Frame · corroded · Jan 29, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FOUND CORROSION ON FRAME LOWER CHORD AT BS 286.5, WL 53 AND LBL 16. FABRICATED CHORD IAW SRM 53-10-1 PAGE 5. REMOVED AND REPLACED CHORD BETWEEN BS 235.5 AND BS 294.5 IAW SRM 51-30-2. (M) - [SDR P2EA00043](https://openairdocs.org/sdr/P2EA00043.md): Frame · corroded · Jan 29, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FOUND CORROSION ON FRAME LOWER FLANGE AT BS 335, BETWEEN 27L AND 28L. REPAIRED FRAME LOWER FLANGE AT BS 335 FROM 28L TO 27L IAW SRM 53-10-4, FIG 4. (M) - [SDR P2EA00064](https://openairdocs.org/sdr/P2EA00064.md): Skin · corroded · Jan 28, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > SJO - DURING Q-CHECK, FOUND CORROSION ON FUSELAGE SKIN AT BS 347, BETWEEN STRINGER 24L AND BL 0. TEAR STRAPS MISSING FROM NEW SKIN. REPLACED SKIN FROM BS 259.5 TO BS 360, BETWEEN STRINGER 24L AND BL 0 IAW SRM 51-10-1 PAGE 5 AND SRM 51-30-2. FABRICATED AND I - [SDR P2EA00062](https://openairdocs.org/sdr/P2EA00062.md): Floorbeam · corroded · Jan 28, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 360, BETWEEN RBL 65 AND LBL 65. REPAIRED FLOORBEAM AT BS 360 BETWEEN RBL 4 AND RBL 65 IAW EO COO-3-53-071-00 DATED 2/9/2000. REMOVED CORROSION FROM LBL 65 TO RBL 4 IAW SRM 51-10-6. (M) - [SDR P2EA00044](https://openairdocs.org/sdr/P2EA00044.md): Floorbeam · cracked · Jan 28, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, FOUND FLOORBEAM CRACKED AT BS 520, LBL 45 AND WL 208. REPAIRED FLOORBEAM FROM LBL 40.5 TO LBL 50.5 IAW SB 737-53-1120, SECTION III, PART VI, FIG 28 AND FOG 29 DATED MAY 13, 1993. (M) - [SDR P2EA00063](https://openairdocs.org/sdr/P2EA00063.md): Frame · corroded · Jan 28, 2000 · N603DJ · Boeing 737222 · Vertical Stabilizer, Spar/Rib > SJO - DURING Q-CHECK, FOUND CORROSION ON VERTICAL STABILIZER AT RIGHT SIDE CHORD AT FIN STATION 77.77. REPAIRED STABILIZER CHORD BETWEEN STATION 67.44 AND STATION 105.5 IAW COOPESA EO COO=3=55-084-00 DATED 02/11/2000. FABRICATED SPAR SECTION IAW COOPESA COO- - [SDR P2EA00042](https://openairdocs.org/sdr/P2EA00042.md): Floorbeam · corroded · Jan 28, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, FOUND CORROSION FLOORBEAM AT BS 328 BETWEEN BL 0 AND LBL 63. REPAIRED FLOORBEAM FROM LBL 65 TO RBL 65 IAW SRM 53-10-9 FIG 5. (M) - [SDR P2EA00035](https://openairdocs.org/sdr/P2EA00035.md): Frame · cracked · Jan 28, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FRAME LOWER FLANGE CRACKED AT BS 360 BETWEEN 14R AND 15R. REPAIRED FRAME LOWER FLANGE AT BS 360 BETWEEN STRINGER 14R AND 15R IAW SRM 53-10-4 FIG 10. (M) - [SDR P2EA00060](https://openairdocs.org/sdr/P2EA00060.md): Skin · corroded · Jan 27, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > SJO - DURING Q-CHECK, FOUND CORROSION ON SKIN BETWEEN BS 243 AND BS 259, WL 161 AND LBL 18. REPAIRED SKIN FROM BS 236.5 TO BS 259 AND BETWEEN STRINGERS 23 AND 26L IAW COOPESA EO COO-3-53-006-00, DATED 2/5/2000. (M) - [SDR P2EA00052](https://openairdocs.org/sdr/P2EA00052.md): Frame · cracked · Jan 27, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FRAME WEB CRACKED AT BS 639, BETWEEN 16L AND 17L. REPAIRED FRAME WEB AT BS 639 IAW SB 737-53-1061, REV 4 DATED JULY 16, 1992. (M) - [SDR P2EA00048](https://openairdocs.org/sdr/P2EA00048.md): Frame · corroded · Jan 27, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FOUND CORROSION ON FRAME AT BS 285, BETWEEN 26L AND 27L. FABRICATED FRAME AND ANGLE SUPPORT AT BS 285, BETWEEN 23L AND 27L IAW SRM 51-10-1, PAGE 5. REMOVED AND REPLACED FRAME AND ANGLES IAW SRM 51-30-2. (M) - [SDR P2EA00065](https://openairdocs.org/sdr/P2EA00065.md): Hinge · cracked · Jan 27, 2000 · N603DJ · Boeing 737222 · Passenger/Crew Doors > SJO - DURING Q-CHECK, R1 DOOR UPPER HINGE INNER DOUBLER AT BS 302 WORN AND UPPER HINGE CRACKED. REPAIRED STRUCTURE FROM BS 295 TO BS 305 BETWEEN STRINGER 8L AND STRINGER 12L IAW COOPESA EO COO-3-53-085-00 DATED 02/11/2000. REPAIRED R1 DOOR UPPER HINGE IAW SB - [SDR P2EA00034](https://openairdocs.org/sdr/P2EA00034.md): Floorbeam · corroded · Jan 27, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 967, FROM LBL 17 TO LBL 51. REPAIRED FLOORBEAM UPPER FLANGE FROM LBL 36 TO LBL 50 IAW SRM 53-10-9 FIG 7. (M) - [SDR P2EA00021](https://openairdocs.org/sdr/P2EA00021.md): Angle · cracked · Jan 27, 2000 · N603DJ · Boeing 737222 · Engine Cowling System > SJO - DURING Q-CHECK, FOUND NR 2 ENGINE NOSE COWL AFT SECTION WALL ANGLE CRACKED A 7 O'CLOCK POSITION. FABRICATED ANGLE IAW SRM 51-20-01. REMOVED AND REPLACED IAW SRM 51-30-2. (M) - [SDR P2EA00056](https://openairdocs.org/sdr/P2EA00056.md): Skin · canning · Jan 26, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin > SJO - DURING Q-CHECK, FUSELAGE SKIN OIL CANNED FROM BS 787 TO BS 807, BETWEEN 22L AND 23L. REPAIRED FUSELAGE SKIN FROM BS 786 TO 811 BETWEEN 21L AND 24L IAW SRM 53-30-3 FIG 1. (M) - [SDR P2EA00055](https://openairdocs.org/sdr/P2EA00055.md): Skin · damaged · Jan 26, 2000 · N603DJ · Boeing 737222 · Leading Edge Devices > SJO - DURING Q-CHECK, FOUND NR 5 SLAT LOWER TRAILING EDGE DAMAGED AT STATION 198 AND STATION 196. REPAIRED NR 5 SLAT IAW COOPESA EO COO-3-57-065-00, DATED 2/4/2000. (M) - [SDR P2EA00047](https://openairdocs.org/sdr/P2EA00047.md): Bulkhead · cracked · Jan 26, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Bulkhead > SJO - DURING Q-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 227.8 WL 182 AND BL 0. REPAIRED WEB AT BS 227.8 BETWEEN WL 188 AND WL 159 IAW SB 737-53-1054, REV 2, SECTION III, FIG 8 DATED 02/29/96. (M) - [SDR P2EA00046](https://openairdocs.org/sdr/P2EA00046.md): Frame · dented · Jan 26, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FRAME DENTED AT BS 500B, BETWEEN 21L AND 25L. REPAIRED FRAME AT BS 500B FRAME 20L TO 25L IAW SRM 51-40-3, FIG 1. (M) - [SDR P2EA00041](https://openairdocs.org/sdr/P2EA00041.md): Fitting · corroded · Jan 26, 2000 · N603DJ · Boeing 737222 · Fuselage Miscellaneous Structure > SJO - FOUND DURING Q-CHECK, CORROSION ON 23L END FITTING AT BS 540. FABRICATED END FITTING IAW SRM 51-10-1 PAGE 5. REMOVED AND REPLACED IAW SRM 51-30-2. (M) - [SDR P2EA00020](https://openairdocs.org/sdr/P2EA00020.md): Splice · corroded · Jan 26, 2000 · N603DJ · Boeing 737222 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND CORROSION AT STRINGER SPLICE AT BS 907, STRINGER 19L. FABRICATED SPLICE IAW SRM 51-20-1, REMOVED AND REPLACED IAW SRM 51-30-02. (M) Next page: https://openairdocs.org/deregistered/N603DJ-2001-03-30/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N603DJ' AND deregistration_id = 'N603DJ-2001-03-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N603DJ-2001-03-30/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.