# N603DJ: Boeing 737-222, registration cancelled 2001-03-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 30, 2001
- Exported to: Peru
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-222](https://openairdocs.org/model/boeing-737-222) (registry code 1384473)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 19955
- Type of aircraft: Fixed wing multi engine
- Certificate issued: March 28, 2001
- Last registry action: March 28, 2001
- Mode S code: A7D2B8
- Owner when cancelled: [Airplane Holdings Corp Trustee](https://openairdocs.org/faa-owner/AIRPLANE%20HOLDINGS%20CORP%20TRUSTEE)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.7655° N, 80.1843° W: Placed by OpenAirDocs at the center of ZIP code 33131, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N603DJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=603DJ
- Page: https://openairdocs.org/deregistered/N603DJ-2001-03-30

From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-222: https://openairdocs.org/model/boeing-737-222.md

## Service difficulty reports (152, newest 50)

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

- [SDR P2E00315](https://openairdocs.org/sdr/P2E00315), Oct 26, 2000: LAP JOINT. CRACKED. 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
- [SDR COOSDR000016](https://openairdocs.org/sdr/COOSDR000016), Oct 26, 2000: LAP JOINT. CRACKED. 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), Oct 25, 2000: LAP JOINT. CORRODED. 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 FUSELAG
- [SDR P2EA00319](https://openairdocs.org/sdr/P2EA00319), Oct 25, 2000: LAP JOINT. CORRODED. 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
- [SDR P2EA00318](https://openairdocs.org/sdr/P2EA00318), Oct 25, 2000: LAP JOINT. CORRODED. 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
- [SDR P2EA00317](https://openairdocs.org/sdr/P2EA00317), Oct 25, 2000: LAP JOINT. CORRODED. 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 EXTER
- [SDR P2EA00316](https://openairdocs.org/sdr/P2EA00316), Oct 25, 2000: LAP JOINT. CRACKED. 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. RE
- [SDR P2EA00321](https://openairdocs.org/sdr/P2EA00321), Oct 25, 2000: LAP JOINT. CORRODED. 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 
- [SDR COOSDR000022](https://openairdocs.org/sdr/COOSDR000022), Oct 25, 2000: LAP JOINT. CORRODED. 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), Oct 25, 2000: LAP JOINT. CORRODED. 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), Oct 25, 2000: LAP JOINT. CORRODED. 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), Oct 25, 2000: LAP JOINT. CORRODED. 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), Oct 25, 2000: LAP JOINT. CRACKED. 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), Oct 25, 2000: LAP JOINT. CORRODED. 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), Oct 24, 2000: SKIN. CRACKED. 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 FUSELA
- [SDR P2EA00226](https://openairdocs.org/sdr/P2EA00226), Jul 11, 2000: STRUCTURE. CRACKED. 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), Jun 14, 2000: ACTUATOR. UNSERVICEABLE. 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
- [SDR P2EA00119](https://openairdocs.org/sdr/P2EA00119), May 10, 2000: FITTING. STRIPPED. 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 Q
- [SDR P2EA00067](https://openairdocs.org/sdr/P2EA00067), Mar 11, 2000: HYDRAULIC LINE. LEAKING. PIT - FLT 701 - AIR RETURN TO PIT, EMERGENCY DECLARED, LANDING UNEVENTFUL. LOST A SYSTEM HYDRAULIC QUANTITY AND PRESSURE IN FLIGHT. REPLACED RIGHT WING SPOILER 
- [SDR P2EA00061](https://openairdocs.org/sdr/P2EA00061), Feb 24, 2000: SPAR. CORRODED. 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 COOPE
- [SDR P2EA00059](https://openairdocs.org/sdr/P2EA00059), Feb 24, 2000: SKIN. CANNING. 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), Feb 21, 2000: SKIN. CRACKED. 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. (
- [SDR P2EA00057](https://openairdocs.org/sdr/P2EA00057), Feb 12, 2000: THRUST REVERSER. OUT OF ADJ. 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
- [SDR P2EA00054](https://openairdocs.org/sdr/P2EA00054), Feb 5, 2000: SKIN. DELAMINATED. 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), Feb 5, 2000: BEAM. CRACKED. 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 737-53-106
- [SDR P2EA00051](https://openairdocs.org/sdr/P2EA00051), Feb 4, 2000: FITTING. MISDRILLED. 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), Feb 4, 2000: STRINGER. CORRODED. 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), Feb 4, 2000: FLOORBEAM. CORRODED. 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-
- [SDR P2EA00026](https://openairdocs.org/sdr/P2EA00026), Jan 30, 2000: STRINGER. CORRODED. 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), Jan 29, 2000: STRINGER. CORRODED. 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), Jan 29, 2000: FRAME. CORRODED. 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 BE
- [SDR P2EA00043](https://openairdocs.org/sdr/P2EA00043), Jan 29, 2000: FRAME. CORRODED. 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-
- [SDR P2EA00064](https://openairdocs.org/sdr/P2EA00064), Jan 28, 2000: SKIN. CORRODED. 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 
- [SDR P2EA00062](https://openairdocs.org/sdr/P2EA00062), Jan 28, 2000: FLOORBEAM. CORRODED. 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-3-53-0
- [SDR P2EA00044](https://openairdocs.org/sdr/P2EA00044), Jan 28, 2000: FLOORBEAM. CRACKED. 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 V
- [SDR P2EA00063](https://openairdocs.org/sdr/P2EA00063), Jan 28, 2000: FRAME. CORRODED. 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 STATI
- [SDR P2EA00042](https://openairdocs.org/sdr/P2EA00042), Jan 28, 2000: FLOORBEAM. CORRODED. 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), Jan 28, 2000: FRAME. CRACKED. 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
- [SDR P2EA00060](https://openairdocs.org/sdr/P2EA00060), Jan 27, 2000: SKIN. CORRODED. 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 2
- [SDR P2EA00052](https://openairdocs.org/sdr/P2EA00052), Jan 27, 2000: FRAME. CRACKED. 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), Jan 27, 2000: FRAME. CORRODED. 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
- [SDR P2EA00065](https://openairdocs.org/sdr/P2EA00065), Jan 27, 2000: HINGE. CRACKED. 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
- [SDR P2EA00034](https://openairdocs.org/sdr/P2EA00034), Jan 27, 2000: FLOORBEAM. CORRODED. 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
- [SDR P2EA00021](https://openairdocs.org/sdr/P2EA00021), Jan 27, 2000: ANGLE. CRACKED. 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 I
- [SDR P2EA00056](https://openairdocs.org/sdr/P2EA00056), Jan 26, 2000: SKIN. CANNING. 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
- [SDR P2EA00055](https://openairdocs.org/sdr/P2EA00055), Jan 26, 2000: SKIN. DAMAGED. 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 2/4/2
- [SDR P2EA00047](https://openairdocs.org/sdr/P2EA00047), Jan 26, 2000: BULKHEAD. CRACKED. 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, SECT
- [SDR P2EA00046](https://openairdocs.org/sdr/P2EA00046), Jan 26, 2000: FRAME. DENTED. 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), Jan 26, 2000: FITTING. CORRODED. 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), Jan 26, 2000: SPLICE. CORRODED. 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)

All 152: https://openairdocs.org/deregistered/N603DJ-2001-03-30/reports.md

## FAA accident and incident reports (5)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20000510016379I](https://openairdocs.org/incident/20000510016379I), May 10, 2000: Boeing 737222 (N603DJ), Pittsburgh, PA. (-23)On may 10, 2000, at 1737E, a Boeing 737, s/n 19955, registered as N603DJ and operating as vaguard airlines (P2EA) flight 732, was on approach to landing…
- [Incident 20000311002329I](https://openairdocs.org/incident/20000311002329I), Mar 11, 2000: Boeing 737222 (N603DJ), Pittsburgh, PA. (-23) On March 11, 2000, at 0825E, a B-737 registered as NO3DJ, and operating as P2EA (vanguard) flight 701 was on approach to "pit" when they reported a…
- [Incident 19990922032209I](https://openairdocs.org/incident/19990922032209I), Sep 22, 1999: Boeing 737222 (N603DJ), Kansas City, MO. (-23) Nose gear failed to retract after take off. Emergency equipment was notified but not on standby. The Boeing 737 aircraft landed without incident and…
- [Incident 19981110039619I](https://openairdocs.org/incident/19981110039619I), Nov 10, 1998: Boeing 737222 (N603DJ), Minneapolis, MN. (-5) On 11/10/98 at msp airport, vangard flt 418 departed for chicago midway airport. Upon climb out at approximately 30 miles out the pilot declared an…
- [Incident 19981029039399I](https://openairdocs.org/incident/19981029039399I), Oct 29, 1998: Boeing 737222 (N603DJ), Moline, IL. (-5) On October 29, 1998, the crew of a vanguard airlines Boeing 737 made an emergency landing at Quad citiies airport due to smoke in the cockpit. Preliminary…

## Other aircraft with N603DJ

- [Registered now](https://openairdocs.org/aircraft/N603DJ): Cirrus Design SR22, S/N 10313, built 2024

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