# N912MP: 1968 Boeing 737-247, registration cancelled 2004-02-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 5, 2004
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-247](https://openairdocs.org/model/boeing-737-247) (registry code 138448D)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 19607
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard
- Certificate issued: December 1, 2003
- Last registry action: December 1, 2003
- Mode S code: AC9F3A
- Owner when cancelled: [Total Aerospace Services Inc](https://openairdocs.org/faa-owner/TOTAL%20AEROSPACE%20SERVICES%20INC)
- Location: [Davie, FL](https://openairdocs.org/faa-place/FL/Davie)
- Owner type: Corporation
- Owner's area on the map: 26.0669° N, 80.2244° W: Placed by OpenAirDocs at the center of ZIP code 33314, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N912MP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=912MP
- Page: https://openairdocs.org/deregistered/N912MP-2004-02-05

From the FAA registry file of October 29, 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 737-247: https://openairdocs.org/model/boeing-737-247.md

## Service difficulty reports (167, newest 50)

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

- [SDR P2EA2001M0016](https://openairdocs.org/sdr/P2EA2001M0016), Dec 19, 2001: ENGINE. MALFUNCTIONED. ON SCHEDULED PUSHBACK FOR FLIGHT 400 PILOT REPORTED THAT NR 2 ENGINE WOULD NOT START. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. NR 2 ENGINE OPERATIONAL CHECKE
- [SDR P2EA01063](https://openairdocs.org/sdr/P2EA01063), May 14, 2001: BUSHING. LOOSE. MCI - FLT 350 - DURING FLIGHT AT 300 KNOTS, AIRCRAFT HAD LOW FREQUENCY AIRFRAME VIBRATION. PERFORMED DETAILED INSPECTION OF FLIGHT CONTROLS IAW BOEING MM 27-11-
- [SDR P2EA01007](https://openairdocs.org/sdr/P2EA01007), Mar 23, 2001: DOUBLER. LEAKING. SJO - REPAIR LEAKING ON FUSELAGE AT BS 727 TO BS 907 BETWEEN STRINGER 3R AND 5R. SENT TO BOEING ENGINEERING ON 3/26/01. IT WAS DETERMINED THAT NO MINOR REPAIR E
- [SDR P2EA01001](https://openairdocs.org/sdr/P2EA01001), Jan 2, 2001: ADC. MALFUNCTIONED. MCI - FLT 301 - AUTO PRESSURIZATION FAILED ON CLIMB-OUT, STANDBY PRESSURIZATION COULD NOT MAINTAIN PRESSURIZATION SCHEDULE. AIRCRAFT RETURNED TO MCI WITH NO INC
- [SDR P2EA00454](https://openairdocs.org/sdr/P2EA00454), Dec 3, 2000: INDICATOR. MALFUNCTIONED. MCI - FLT 360 - ON LANDING, DURING L/E SLAT EXTENSION, NR 2 SLAT SHOWED NO INDICATION. EMERGENCY DECLARED AND AIRCRAFT LANDED WITH NO INCIDENT. REPAIRED BROKEN 
- [SDR P2EA00453](https://openairdocs.org/sdr/P2EA00453), Dec 2, 2000: INDICATOR. MALFUNCTIONED. MSY - FLT 355 - ON LANDING, DURING L/E SLAT EXTENSION, (AT FLAPS 5) NR 2 SLAT SHOWED NO INDICATION. EMERGENCY DECLARED AND AIRCRAFT LANDED WITH NO INCIDENT. DIS
- [SDR P2EA00331](https://openairdocs.org/sdr/P2EA00331), Oct 28, 2000: STIFFENER. CRACKED. SJO - DURING Q-CHECK, FOUND THE FORWARD CARGO BULKHEAD VERTICAL STIFFENE AT BS 540, LBL 25, WL 204 WITH CRACK 2 INCHES BY .002 INCH. IDENTIFIED AS REPORTABLE ON
- [SDR P2EA00334](https://openairdocs.org/sdr/P2EA00334), Oct 28, 2000: BULKHEAD. CRACKED. SJO - DURING Q-CHECK, FOUND THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, LBL 14 WL 178 WITH CRACK. L = 1.50 INCHES. W = 0.002 INCH. IDENTIFIED AS RE
- [SDR P2EA00329](https://openairdocs.org/sdr/P2EA00329), Oct 26, 2000: DOOR FRAME. CRACKED. SJO - DURING Q-CHECK, FOUND THE FORWARD CARGO DOOR FRAME LOWER FORWARD CORNER WITH CRACK .75 INCH BY .002 INCH. IDENTIFIED AS REPORTABLE ON 11-07-00. REPAIRED T
- [SDR P2EA00333](https://openairdocs.org/sdr/P2EA00333), Oct 25, 2000: DOOR FRAME. CRACKED. SJO - DURING Q-CHECK, FO UND THE L-1 DOOR JAMB AFT LOWER CORNER SKIN WITH CRACK 2.5 INCH BY .002 INCH. IDENTIFIED AS REPORTABLE ON 11-07-2000. REPAIRED THE L-1 
- [SDR P2EA00328](https://openairdocs.org/sdr/P2EA00328), Oct 25, 2000: SKIN. CORRODED. SJO - DURING Q-CHECK, FOUND THE EXTERIOR FUSELAGE SKIN AT BS 306 - BS 311 STR 24R WITH CORROSION. L = 5.00 INCHES. W = 2.500 INCHES. D = 0.065 INCH. IDENTIFIED 
- [SDR P2EA00330](https://openairdocs.org/sdr/P2EA00330), Oct 23, 2000: STIFFENER. CRACKED. SJO - DURING Q-CHECK, FOUND THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, RBL 25 WL 204 WITH CRACK 1.5 INCH BY .002 INCH. IDENTIFIED AS REPORTABLE ON
- [SDR P2EA00332](https://openairdocs.org/sdr/P2EA00332), Oct 23, 2000: SKIN. DAMAGED. SJO - DURING Q-CHECK, FOUND THE LEFT WING OUTBOARD FORE FLAP, OUTBOARD END, LEADING EDGE SKIN WITH WEAR 10 INCHES BY 1 INCH. IDENTIFIED AS REPORTABLE ON 11-07-0
- [SDR P2EA00337](https://openairdocs.org/sdr/P2EA00337), Oct 23, 2000: LAP JOINT. CRACKED. SJO - DURING Q-CHECK, FOUND THE LOWER EXTERIOR FUSELAGE LAP JOINT UPPER ROW WITH CRACK INDICATION AT BS 948 STR 25R. L = 1.00 INCH. W = 0.001 INCH. IDENTIFIED A
- [SDR P2EA00336](https://openairdocs.org/sdr/P2EA00336), Oct 23, 2000: LAP JOINT. CRACKED. SJO - DURING Q-CHECK, FOUND THE LOWER EXTERIOR FUSELAGE LAP JOINT UPPER ROW WITH CRACK INDICATION AT BS 500B STR 19R. L = 1.00 INCH. W = 0.001 INCH. IDENTIFIED 
- [SDR COOSDR000001](https://openairdocs.org/sdr/COOSDR000001), Oct 22, 2000: SKIN. CRACKED. EXTERIOR FUSELAGE SECTION 41, RT FUSELAGE SKIN CRACKED AT FASTENER HOLE LOCATION, STA 227.8, BS 211.8, WL 215, WL 217, WL 221.5, AND WL 222. POSSIBLE CAUSE OF T
- [SDR P2EA00335](https://openairdocs.org/sdr/P2EA00335), Oct 21, 2000: SKIN. DENTED. SJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLIPPER FLAP, TRAILING EDGE WITH DENT. L = 9.875 INCHES. W = 7.625 INCHES. IDENTIFIED AS REPORTABLE ON 11-7-
- [SDR P2EA00327](https://openairdocs.org/sdr/P2EA00327), Oct 21, 2000: SKIN. CRACKED. SJO - DURING Q-CHECK, FOUND THE EXTERIOR FUSELAGE SKIN AT BS 227.8 WL 225 WITH CRACK. L = 1.200 INCH. W = 0.001 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPAI
- [SDR P2EA00326](https://openairdocs.org/sdr/P2EA00326), Oct 19, 2000: BULKHEAD. CRACKED. SJO - DURING Q-CHECK, FOUND THE LOWER NOSE COMPARTMENT VERTICAL CHORD AT BS 178 LBL 5.7 WL 184 WITH CRACK. L = 1.50 INCHES. W = 0.003 INCH. IDENTIFIED AS REPORT
- [SDR P2EA00314](https://openairdocs.org/sdr/P2EA00314), Oct 14, 2000: STRINGER. DAMAGED. DURING Q CHECK FOUND THE FUSELAGE STRINGER 24R BETWEEN BS 294.5 AND BS 328 WITH ELONGATED HOLES. REPLACED THE FUSELAGE STRINGER 24R BETWEEN BS 294.5 AND BS 328 
- [SDR P2EA00305](https://openairdocs.org/sdr/P2EA00305), Oct 12, 2000: FLOORBEAM. CRACKED. DURING Q CHECK FOUND THE PAX CABIN FLOORBEAM WEB AT BS 312 BETWEEN RBL 8 AND RBL 18 WITH CRACK L=0.50 W=0.002. REPAIRED THE PAX CABIN FLOORBEAM WEB AT BS 312 BE
- [SDR P2EA00302](https://openairdocs.org/sdr/P2EA00302), Oct 12, 2000: FLOORBEAM. CRACKED. DURING Q CHECK FOUND THE PAX CABIN FLOORBEAM WEB AT BS312 BETWEEN RBL 5 AND REL 14 WITH CRACK L=0.75 W=0.002. REPAIRED THE PAX CABIN FLOORBEAM WEB AT BS312 BETW
- [SDR P2EA00322](https://openairdocs.org/sdr/P2EA00322), Oct 12, 2000: PANEL. DELAMINATED. DURING Q CK FOUND LT WING AFT PYLON ACCESS PANEL AT WBL 191 WITH DELAMINATION L=12.0 IN, W=10.0 INREPLACED LEFT WING AFT PYLON PANEL AT WBL 9=191 IAW COOPESA EO
- [SDR P2EA00339](https://openairdocs.org/sdr/P2EA00339), Oct 11, 2000: DOUBLER. CRACKED. SJO - DURING Q-CHECK, FOUND DOUBLER ON PREVIOUS REPAIR ON FLOORBEAM AT AILERON CONTROL QUADRANT AT BS 678 LBL 24.82 CRACKED. L = 1.00 INCH. W = 0.002 INCH. IDEN
- [SDR P2EA00300](https://openairdocs.org/sdr/P2EA00300), Oct 11, 2000: LAP JOINT. CRACKED. SJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE LAP JOINT UPPER ROW AT BS 749L STR 25L WITH CRACK INDICATION. REPAIRED THE LOWER FUSELAGE LAP JOINT UPPER ROW AT 
- [SDR P2EA00299](https://openairdocs.org/sdr/P2EA00299), Oct 11, 2000: LAP JOINT. CRACKED. SJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE LAP JOINT UPPER ROW BETWEEN BS 478 - BS 480L STR 19L WITH CRACK INDICATION. REPAIRED THE LOWER FUSELAGE LAP JOINT
- [SDR COOSDR000009](https://openairdocs.org/sdr/COOSDR000009), Oct 11, 2000: LAP JOINT. CRACKED. FUSELAGE SKIN, STA 749, STR 25L, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR 20001129SH026](https://openairdocs.org/sdr/20001129SH026), Oct 11, 2000: LAP JOINT. CRACKED. FUSELAGE SKIN, STA 948, STR 25R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR COOSDR000007](https://openairdocs.org/sdr/COOSDR000007), Oct 11, 2000: LAP JOINT. CRACKED. FUSELAGE SKIN, BETWEEN STA 478 TO STA 480, STR 19L, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR COOSDR000006](https://openairdocs.org/sdr/COOSDR000006), Oct 11, 2000: LAP JOINT. CRACKED. FUSELAGE SKIN, STA 500B, STR 19R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR COOSDR000005](https://openairdocs.org/sdr/COOSDR000005), Oct 11, 2000: LAP JOINT. CRACKED. FUSELAGE SKIN, BETWEEN STA 306 TO STA 311, STR 24R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR P2EA00338](https://openairdocs.org/sdr/P2EA00338), Oct 10, 2000: DOUBLER. CRACKED. SJO - DURING Q-CHECK, FOUND DOUBLER ON PREVIOUS REPAIR ON FLOORBEAM AT AILERON CONTROL QUADRANT AT BS 678 RBL 24.82 CRACKED. L = 1.00 INCH. W = 0.002 INCH. IDEN
- [SDR P2EA00309](https://openairdocs.org/sdr/P2EA00309), Oct 9, 2000: FRAME. CRACKED. DURING Q CHECK FOUND THE FUSELAGE FRAME WEB AT BS 260L, LBL 19 WL 276 WITH CRACK L=1.00 W=0.002. REPAIRED THE FUSELAGE FRAME WEB AT BS260L, LBL 19"WL276 WITH CR
- [SDR P2EA313](https://openairdocs.org/sdr/P2EA313), Oct 7, 2000: FLOORBEAM. CORRODED. DURING Q CHECK FOUND THE PAX CABIN FLOORBEAM UPPER SURFACE AT BS 947 LBL 45 WITH CORROSION LEVEL 2. REPAIRED THE PAX CABIN FLOORBEAM UPPER SURFACE AT BS947 LBL4
- [SDR P2EA00313](https://openairdocs.org/sdr/P2EA00313), Oct 7, 2000: FLOORBEAM. CORRODED. DURING Q CHECK FOUND THE FAX CABIN FLOORBEAM UPPER SURFACE AT BS 947 LBL45 WITH CORROSION LEVEL 2. REPAIRED THE PAX CABIN FLOORBEAM UPPER SURFACE AT BS947 LBL 4
- [SDR P2EA00308](https://openairdocs.org/sdr/P2EA00308), Oct 7, 2000: FRAME. CRACKED. DURING Q CHECK FOUND THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT BS 420R STR 26R WITH CRACK L=1.00 W=0.002. REPAIRED THE LOWER FUSELAGE FWD CARGO COMPARTM
- [SDR P2EA00307](https://openairdocs.org/sdr/P2EA00307), Oct 7, 2000: FRAME. CRACKED. DURING Q CHECK FOUND THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT BS 420R STR 26R WITH CRACK L=1.00 W=0.002. REPAIRED THE LOWER FUSELAGE FWD CARGO COMPARTM
- [SDR P2EA00304](https://openairdocs.org/sdr/P2EA00304), Oct 7, 2000: ANGLE. CRACKED. DURING Q CHECK FOUND THE AFT CARGO COMPARTMENT LOWER DOOR JAMB ANGLE BETWEEN BS 817 AND 822 RBL 20 WITH CRACK L=1.00 W=0.001. REPAIRED THE AFT CARGO COMPARTMENT
- [SDR P2EA00303](https://openairdocs.org/sdr/P2EA00303), Oct 7, 2000: FRAME. CRACKED. DURING Q CHECK FOUND THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT BS500A BETWEEN STR 20-21L WITH CRACK L=1.50 W=0.002. REPAIRED THE LOWER FUSELAGE FWD CARG
- [SDR P2EA00298](https://openairdocs.org/sdr/P2EA00298), Oct 7, 2000: FRAME. DENTED. SJO - DURING Q-CHECK, FOUND THE AFT CARGO COMPARTMENT AT BS 727B BETWEEN STR 24 - STR 25L FRAME WITH DENT. L - 1.50 INCHES. W = 1.00 INCH. D = 0.125 INCH. REPAI
- [SDR P2EA00297](https://openairdocs.org/sdr/P2EA00297), Oct 7, 2000: FRAME. CRACKED. SJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE FORWARD CARGO COMPARTMENT AT BS 420 BETWEEN STR 20 - STR 21L FRAME WITH CRACK. L = 1.00 INCH. W = 0.002 INCH. REP
- [SDR P2EA00296](https://openairdocs.org/sdr/P2EA00296), Oct 7, 2000: FRAME. CRACKED. SJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE FORWARD CARGO COMPARTMENT AT BS 500 BETWEEN STR 21 - STR 22R FRAME WITH CRACK. L = 1.250 INCHES. W = 0.001 INCH. 
- [SDR P2EA00294](https://openairdocs.org/sdr/P2EA00294), Oct 7, 2000: FRAME. DENTED. DURING Q-CHECK, FOUND THE AFT CARGO COMPARTMENT BS 747 BETWEEN STR 24 - STR 25R FRAME WITH DENT. L = 1.50 INCHES. W = 1.00 INCH. D = 0.160 INCH. REPAIRED THE AF
- [SDR P2EA00293](https://openairdocs.org/sdr/P2EA00293), Oct 7, 2000: DOOR FRAME. CRACKED. SJO - DURING Q-CHECK, FOUND THE R-1 DOOR CUT OUT LOWER CORNER AT BS 315 WITH CRACK. L = 1.50 INCHES. W = 0.002 INCH. REPAIRED THE R-1 DOOR CUT OUT LOWER CORNER 
- [SDR P2EA00292](https://openairdocs.org/sdr/P2EA00292), Oct 7, 2000: SPLICE. CRACKED. SJO - DURING Q-CHECK FOUND THE AFT CARGO COMPARTMENT FROM BS 907 TO BS 927, STR 23L SPLICE WITH CRACK. L = 0.625 INCH. REPLACED THE AFT CARGO COMPARTMENT, STR 2
- [SDR P2EA00291](https://openairdocs.org/sdr/P2EA00291), Oct 7, 2000: FLAP. DELAMINATED. SJO - DURING Q-CHECK, FOUND THE LEFT OUTBOARD AFT FLAP TRAILING EDGE AT WBL 289 WITH DELAMINATION. L = 4.0 INCHES. W = 2.0 INCHES. REPAIRED THE LEFT OUTBOARD AF
- [SDR COOSDR000014](https://openairdocs.org/sdr/COOSDR000014), Oct 7, 2000: FRAME. CRACKED. LOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 500, BETWEEN STR 21R AND STR 22R, FRAME CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR COOSDR000013](https://openairdocs.org/sdr/COOSDR000013), Oct 7, 2000: FRAME. CRACKED. LOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 420, STR 26R, FRAME CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR COOSDR000012](https://openairdocs.org/sdr/COOSDR000012), Oct 7, 2000: FRAME. CRACKED. LOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 500A, BETWEEN STR 20L AND STR 21L, FRAME CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR COOSDR000011](https://openairdocs.org/sdr/COOSDR000011), Oct 7, 2000: SKIN. CRACKED. FUSELAGE SKIN, FORWARD ENTRY DOOR, AFT LOWER CORNER, CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)

All 167: https://openairdocs.org/deregistered/N912MP-2004-02-05/reports.md

## FAA accident and incident reports (4)

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 20000621033199I](https://openairdocs.org/incident/20000621033199I), Jun 21, 2000: Boeing 737247 (N912MP), Kansas City, MO. (-23)On June, 21, 2000, vanguard airlines, flight 303, aircraft 912MP was scheduled to enroute from mci to den. On initial climb out, cabin pressure, auto…
- [Incident 19991113037819I](https://openairdocs.org/incident/19991113037819I), Nov 13, 1999: Boeing 737247 (N912MP), Minneapolis, MN. (-23) Vanguard airlines flight 703 from mdw to msp on approach to msp declared an emergency due to a flap malfunction. Aircraft landed without further indicent…
- [Incident 19990616022749I](https://openairdocs.org/incident/19990616022749I), Jun 16, 1999: Boeing 737247 (N912MP), Kansas City, MO. After takeoff, nose gear indicator light would not illuminate. Pilot returned to mci and landed without incident. Maintenance found open circuit breaker and…
- [Incident 19990203012129I](https://openairdocs.org/incident/19990203012129I), Feb 3, 1999: Boeing 737247 (N912MP). On February 23,1999, vanguard airlines, flight 817, a Boeing 737, was enroute from mci to dfw and turned back to mci due to hydraulic system failure. An…

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