# Service difficulty reports: N912MP, cancelled Feb 5, 2004

A list on [N912MP, cancelled Feb 5, 2004](https://openairdocs.org/deregistered/N912MP-2004-02-05.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 · 167 reports

- [SDR P2EA2001M0016](https://openairdocs.org/sdr/P2EA2001M0016.md): Engine · malfunctioned · Dec 19, 2001 · N912MP · Boeing 737247 · Engine (Turbine/Turboprop)
  > 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 CHECKED IAW MM 71-09-100.
- [SDR P2EA01063](https://openairdocs.org/sdr/P2EA01063.md): Bushing · loose · May 14, 2001 · N912MP · Boeing 737247 · Landing Gear Doors
  > MCI - FLT 350 - DURING FLIGHT AT 300 KNOTS, AIRCRAFT HAD LOW FREQUENCY AIRFRAME VIBRATION. PERFORMED DETAILED INSPECTION OF FLIGHT CONTROLS IAW BOEING MM 27-11-00, 27-51-0 AND 27-61-0, NO DEFECTS FOUND. INSPECTED AIRCRAFT A/C BAY DOORS IAW BOEING MM 52-49-0,
- [SDR P2EA01007](https://openairdocs.org/sdr/P2EA01007.md): Doubler · leaking · Mar 23, 2001 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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 EXISTED. (M)
- [SDR P2EA01001](https://openairdocs.org/sdr/P2EA01001.md): Adc · malfunctioned · Jan 2, 2001 · N912MP · Boeing 737247 · Air Data Computer
  > MCI - FLT 301 - AUTO PRESSURIZATION FAILED ON CLIMB-OUT, STANDBY PRESSURIZATION COULD NOT MAINTAIN PRESSURIZATION SCHEDULE. AIRCRAFT RETURNED TO MCI WITH NO INCIDENT. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER IAW MM 21-30-0, OPERATIONAL CHECK NORMAL. (M)
- [SDR P2EA00454](https://openairdocs.org/sdr/P2EA00454.md): Indicator · malfunctioned · Dec 3, 2000 · N912MP · Boeing 737247 · Leading Edge Slat Position Indicating System
  > 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 WIRE PER MM CHAPTER 20. SYSTEM CHECKED NORMAL PER 27-88-0. (M)
- [SDR P2EA00453](https://openairdocs.org/sdr/P2EA00453.md): Indicator · malfunctioned · Dec 2, 2000 · N912MP · Boeing 737247 · Leading Edge Slat Position Indicating System
  > 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. DISCREPANCY COULD NOT BE DUPLICATE ON THE GROUND. (M)
- [SDR P2EA00331](https://openairdocs.org/sdr/P2EA00331.md): Stiffener · cracked · Oct 28, 2000 · N912MP · Boeing 737247 · Fuselage Miscellaneous Structure
  > 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 11.07-00. REPAIRED THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, LBL 25, WL 204 IAW BO
- [SDR P2EA00334](https://openairdocs.org/sdr/P2EA00334.md): Bulkhead · cracked · Oct 28, 2000 · N912MP · Boeing 737247 · Fuselage Main, Bulkhead
  > 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 REPORTABLE ON 11-7-00. REPLACED THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, LBL 14, W
- [SDR P2EA00329](https://openairdocs.org/sdr/P2EA00329.md): Door Frame · cracked · Oct 26, 2000 · N912MP · Boeing 737247 · Fuselage Main, Structure
  > 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 THE FORWARD CARGO DOOR FRAME LOWER FORWARD CORNER WITH CRACK IAW BOEING SB 737-52-1090 REV 1 DATED
- [SDR P2EA00333](https://openairdocs.org/sdr/P2EA00333.md): Door Frame · cracked · Oct 25, 2000 · N912MP · Boeing 737247 · Fuselage Main, Structure
  > 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 DOOR JAMB AFT LOWER CORNER SKIN IAW BOEING SB 737-53-1083 SECT III PART IV REV 3 DATED DECEMBER 7,
- [SDR P2EA00328](https://openairdocs.org/sdr/P2EA00328.md): Skin · corroded · Oct 25, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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 AS REPORTABLE ON 11-7-00. REPAIRED THE EXTERIOR FUSELAGE SKIN AT BS 306 - BS 311 STR 24R IAW BO
- [SDR P2EA00330](https://openairdocs.org/sdr/P2EA00330.md): Stiffener · cracked · Oct 23, 2000 · N912MP · Boeing 737247 · Fuselage Miscellaneous Structure
  > 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 11-07-2000. REPAIRED THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, RBL 25 WL 204 IAW B
- [SDR P2EA00332](https://openairdocs.org/sdr/P2EA00332.md): Skin · damaged · Oct 23, 2000 · N912MP · Boeing 737247 · Leading Edge Devices
  > 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 11-07-00. REPAIRED THE LEFT WING OUTBOARD FORE FLAP, OUTBOARD END, LEADING EDGE SKIN IAW BOEING FAX COO-S
- [SDR P2EA00337](https://openairdocs.org/sdr/P2EA00337.md): Lap Joint · cracked · Oct 23, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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 AS REPORTABLE ON 11-7-00. REPAIRED THE LOWER EXTERIOR FUSELAGE LAP JOINT UPPER ROW WITH CRACK IND
- [SDR P2EA00336](https://openairdocs.org/sdr/P2EA00336.md): Lap Joint · cracked · Oct 23, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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 AS REPORTABLE ON 11-7-00. REPAIRED THE LOWER EXTERIOR FUSELAGE LAP JOINT UPPER ROW WITH CRACK IN
- [SDR COOSDR000001](https://openairdocs.org/sdr/COOSDR000001.md): Skin · cracked · Oct 22, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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 THE CRACK WAS SKIN FATIGUE. (X)
- [SDR P2EA00335](https://openairdocs.org/sdr/P2EA00335.md): Skin · dented · Oct 21, 2000 · N912MP · Boeing 737247 · Trailing Edge Flaps
  > 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 11-7-00. REPAIRED THE RIGHT WING OUTBOARD FLIPPER FLAP, TRAILING EDGE IAW COOPESA EOS COO-CMP-3-37-62
- [SDR P2EA00327](https://openairdocs.org/sdr/P2EA00327.md): Skin · cracked · Oct 21, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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. REPAIRED THE EXTERIOR FUSELAGE SKIN AT BS 227.8 WL 225 IAW BOEING FAX COO-SJO-00-1180H DATED OCT 17,
- [SDR P2EA00326](https://openairdocs.org/sdr/P2EA00326.md): Bulkhead · cracked · Oct 19, 2000 · N912MP · Boeing 737247 · Fuselage Main, Bulkhead
  > 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 REPORTABLE ON 11-7-00. REPAIRED THE LOWER NOSE COMPARTMENT VERTICAL CHORD AT BS 178 LBL 5.7 WL 184 IAW
- [SDR P2EA00314](https://openairdocs.org/sdr/P2EA00314.md): Stringer · damaged · Oct 14, 2000 · N912MP · Boeing 737247 · Fuselage Main, Longeron/Stringer
  > 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 IAW BOEING SRM 53-10-3 FIG 1
- [SDR P2EA00305](https://openairdocs.org/sdr/P2EA00305.md): Floorbeam · cracked · Oct 12, 2000 · N912MP · Boeing 737247 · Fuselage Main, Floor Beam
  > 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 BETWEEN RBL 8 AND RBL 18 IAW BOEING FAX COO-SJO-OO-1175H DATED OCT 13, 2000 DOCUMENTED ON FAA FORM 8
- [SDR P2EA00302](https://openairdocs.org/sdr/P2EA00302.md): Floorbeam · cracked · Oct 12, 2000 · N912MP · Boeing 737247 · Fuselage Main, Floor Beam
  > 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 BETWEEN RBL 5 AND RBL 14 IAW BOEING FAX COO-SJO-OO-01182H DATED OCT 17, 2000 DOCUMENTED ON FAA FORM 81
- [SDR P2EA00322](https://openairdocs.org/sdr/P2EA00322.md): Panel · delaminated · Oct 12, 2000 · N912MP · Boeing 737247 · Wing, Plate/Skin
  > 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#COO-CMP-3-57-633-00 DATED OCT 9, 2000 DOCUMENTED ON FAA FORM 8110-3 APPROVED AND SUBMITTED BY FAA D
- [SDR P2EA00339](https://openairdocs.org/sdr/P2EA00339.md): Doubler · cracked · Oct 11, 2000 · N912MP · Boeing 737247 · Fuselage Main, Floor Beam
  > 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. IDENTIFIED AS REPORTABLE ON 11-7-00. REPLACED DOUBLER ON PREVIOUS REPAIR ON FLOORBEAM AT AILERON CON
- [SDR P2EA00300](https://openairdocs.org/sdr/P2EA00300.md): Lap Joint · cracked · Oct 11, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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 BS 749L STR 25L IAW BOEING SRM 53-30-3 FIG 13. (X)
- [SDR P2EA00299](https://openairdocs.org/sdr/P2EA00299.md): Lap Joint · cracked · Oct 11, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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 UPPER ROW BETWEEN BS 478 - BS 480L STR 19L IAW BOEING SRM 53-30-3 FIG 14. (X)
- [SDR COOSDR000009](https://openairdocs.org/sdr/COOSDR000009.md): Lap Joint · cracked · Oct 11, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, STA 749, STR 25L, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR 20001129SH026](https://openairdocs.org/sdr/20001129SH026.md): Lap Joint · cracked · Oct 11, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, STA 948, STR 25R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR COOSDR000007](https://openairdocs.org/sdr/COOSDR000007.md): Lap Joint · cracked · Oct 11, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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.md): Lap Joint · cracked · Oct 11, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, STA 500B, STR 19R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
- [SDR COOSDR000005](https://openairdocs.org/sdr/COOSDR000005.md): Lap Joint · cracked · Oct 11, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > 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.md): Doubler · cracked · Oct 10, 2000 · N912MP · Boeing 737247 · Fuselage Main, Floor Beam
  > 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. IDENTIFIED AS REPORTABLE ON 11-7-00. REPLACED DOUBLER ON PREVIOUS REPAIR FLOORBEAM AT AILERON CONTRO
- [SDR P2EA00309](https://openairdocs.org/sdr/P2EA00309.md): Frame · cracked · Oct 9, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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 CRACK L=1.00" W+0.002" IAW 51-40-2 FIG 1
- [SDR P2EA313](https://openairdocs.org/sdr/P2EA313.md): Floorbeam · corroded · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Floor Beam
  > 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 LBL45 IAW BOEING FAX COO-SJO-00-01194H DATED OCT 19, 2000 AND COOPESA EO COO-3-53-636-00 DATED OCT 20,
- [SDR P2EA00313](https://openairdocs.org/sdr/P2EA00313.md): Floorbeam · corroded · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Floor Beam
  > 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 45 IAW BOEING FAX COO-SJO-00-01194H DATED OCT 19, 2000 AND COOPESA EA#COO-3-53-636-00 DATED OCT 20,
- [SDR P2EA00308](https://openairdocs.org/sdr/P2EA00308.md): Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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 COMPARTMENT FRAME AT BS 420R STR 26R IAW BOEING SRM 53-10-4 FIG 1
- [SDR P2EA00307](https://openairdocs.org/sdr/P2EA00307.md): Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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 COMPARTMENT FRAME AT BS 420R STR 26R IAW BOEING SRM 53-10-4 FIG 1
- [SDR P2EA00304](https://openairdocs.org/sdr/P2EA00304.md): Angle · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Miscellaneous Structure
  > 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 LOWER DOOR JAMB ANGLE BETWEEN BS817 AND 822 RBL20" IAW BOEING SRM 51-40-3 FIG 2
- [SDR P2EA00303](https://openairdocs.org/sdr/P2EA00303.md): Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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 CARGO COMPARTMENT FRAME AT VS500A BETWEEN STR 20-21L IAW BOEING SRM 53-10-6 FIG 1
- [SDR P2EA00298](https://openairdocs.org/sdr/P2EA00298.md): Frame · dented · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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. REPAIRED THE AFT CARGO COMPARTMENT AT BS 727B BETWEEN STR 24 - STR 25L FRAME IAW BOEING SRM 51-40-3 F
- [SDR P2EA00297](https://openairdocs.org/sdr/P2EA00297.md): Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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. REPAIRED THE LOWER FUSELAGE FORWARD CARGO COMPARMENT AT BS 420 BETWEEN STR 20 - STR 21L FRAME IAW BO
- [SDR P2EA00296](https://openairdocs.org/sdr/P2EA00296.md): Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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. REPAIRED THE LOWER FUSELAGE FORWARD CARGO COMPARTMENT AT BS 500 BETWEEN STR 21 - STR 22R FRAME IA
- [SDR P2EA00294](https://openairdocs.org/sdr/P2EA00294.md): Frame · dented · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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 AFT CARGO COMPARTMENT BS 747 BETWEEN STR 24 - STR 25R FRAME 6 IAW BOEING SRM 53-10-4. (X)
- [SDR P2EA00293](https://openairdocs.org/sdr/P2EA00293.md): Door Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Structure
  > 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 AT BS 315 IAW BOEING SRM 53-30-3 FIG 26. (X)
- [SDR P2EA00292](https://openairdocs.org/sdr/P2EA00292.md): Splice · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Longeron/Stringer
  > 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 23L SPLICE AT BS 907 TO BS 927 IAW BOEING SRM 51-10-1. (X)
- [SDR P2EA00291](https://openairdocs.org/sdr/P2EA00291.md): Flap · delaminated · Oct 7, 2000 · N912MP · Boeing 737247 · Trailing Edge Flaps
  > 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 AFT FLAP TRAILING EDGE AT WBL 289 IAW BOEING SRM 51-40-6 PARA 2.5 FIG 3. (X)
- [SDR COOSDR000014](https://openairdocs.org/sdr/COOSDR000014.md): Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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.md): Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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.md): Frame · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Frame
  > 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.md): Skin · cracked · Oct 7, 2000 · N912MP · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, FORWARD ENTRY DOOR, AFT LOWER CORNER, CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)

Next page: https://openairdocs.org/deregistered/N912MP-2004-02-05/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 = 'N912MP' AND deregistration_id = 'N912MP-2004-02-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N912MP-2004-02-05/reports

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