# Service difficulty reports: N412CE, cancelled Jul 29, 2013

A list on [N412CE, cancelled Jul 29, 2013](https://openairdocs.org/deregistered/N412CE-2013-07-29.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 2 · 92 reports

- [SDR P2EA00225](https://openairdocs.org/sdr/P2EA00225.md): Floorbeam · cracked · Jul 10, 2000 · N412CE · Boeing 737205 · Fuselage Main, Floor Beam
  > SJO - DURING C-CHECK, LEFT AIR CONDITIONING BAY, WING CENTER SECTIN RBL 40.875 BETWEEN BS 573 AND BS 576 LOWER BEAM WEB WITH A CRACK, 2.5 INCHES LONG BY.001 INCH WIDE. REPAIRED LOWER FUSELAGE BEAM WEB AT WING CENER SECTION PER COOPESA EO COO-3-53-470-00 DATE
- [SDR P2EA00224](https://openairdocs.org/sdr/P2EA00224.md): Floorbeam · corroded · Jul 10, 2000 · N412CE · Boeing 737205 · Fuselage Main, Floor Beam
  > SJO - DURING C-CHECK, RIGHT AIR CONDITIONING BAY, WING CENTER SECTION RBL 40.875 BETWEEN BS 571 AND BS 584 LOWER BEAM WEB WITH A CRACK 2 INCHES LONG BY.002 INCHES WIDE. REPAIRED LOWER FUSELAGE BEAM WEB AT WING CENTER SECTION PER COOPESA EO COO-3-53-467-00 DA
- [SDR P2EA00223](https://openairdocs.org/sdr/P2EA00223.md): Frame · cracked · Jul 10, 2000 · N412CE · Boeing 737205 · Fuselage Main, Frame
  > SJO - DURING C-CHECK, FUSELAGE FRAME CRACKED AT BS 794, BETWEEN STRINGER 18RT AND STRINGER 27 RT, DEFECT SIZE 3 INCHES LONG BY.001 INCH WIDE. REPAIRED FUSELAGE FRAME SECTION PER SERVICE BULLETIN 737-53-1036 REVISION 5 DATED JANUARY 16, 1992, SECTION III, FIG
- [SDR P2EA00220](https://openairdocs.org/sdr/P2EA00220.md): Fairing · delaminated · Jul 10, 2000 · N412CE · Boeing 737205 · Aerodynamic Fairings
  > SJO - DURING C-CHECK, ADF ANTENNA DELAMINATED ON LEFT WING TO BODY FAIRING, DEFECT SIZE 40 INCHES BY 29.750 INCHES. REPAIRED LEFT WING TO BODY SENSE ANTENNA PER COOPESA EO COO-CMP-3-530466-00 DATED 7-11-00. (M)
- [SDR P2EA00200](https://openairdocs.org/sdr/P2EA00200.md): Module · failed · Jun 11, 2000 · N412CE · Boeing 737205 · Stall Warning System
  > FLT 305 - MCI - AIR RETURN, EMERGENCY DECLARED, LANDING UNEVENTFUL. ON CLIMB-OUT, STICK SHAKER WENT OUT AT 210 KNOTS ON FLAP RETRACTION, GOT WORSE, RETURNED TO LAND, STICK SHAKER CONTINUED THROUGH ALL FLAP SETTINGS. REPLACED STALL WARNING MODULE, MM 27-32-0,
- [SDR P2EA00116](https://openairdocs.org/sdr/P2EA00116.md): Actuator · malfunctioned · Apr 25, 2000 · N412CE · Boeing 737205 · Stabilizer Control System
  > MYR - FLT 406 - ON APPRAOCH TO MYR, RECEIVED UNCOMMANDED AFT STABAILIZER TRIM. PUT TRIM CUT OUT SWITCH TO OFF, BUT TRIM DID NOT STOP. GRABBED TRIM WHEEL AND TRIM STOPPED THEN JAMMED. BROKE LOOSE (FREE) USING MANUAL HANDLES AND TRIMMED AIRCRAFT MANUALLY, TRI
- [SDR P2EA99307](https://openairdocs.org/sdr/P2EA99307.md): Acm · failed · Oct 24, 1999 · N412CE · Boeing 737205 · Cabin Cooling System
  > MCI - FLT 584 - AFTER SHUT DOWN OF NR 1 ENGINE A BURNING ODOR WAS NOTICE FOLLOWED, A FEW SECONDS LATER, BY SMOKE IN THE COCKPIT AND FORWARD CABIN. REMOVED AND REPLACED RIGHT PACK AIR CYCLE MACHING PER MM 21-51-11. OPERATION NORMAL. (M)
- [SDR P2EA99227](https://openairdocs.org/sdr/P2EA99227.md): Mechanism · out of adjust · Aug 28, 1999 · N412CE · Boeing 737205 · Trailing Edge Flap Control System
  > PIT - FLT 422 - NO EMERGENCY DECLARED, LANDING NORMAL. STRONG VIBRATION NOTED IN MID CABIN WHEN FLAPS EXTENDED FOR LANDING. ADJUSTED LEFT TRAILING EDGE AFT FLAP PER MM 27-51-12, OPS CHECK NORMAL. (M)
- [SDR P2EA99209](https://openairdocs.org/sdr/P2EA99209.md): Stringer · cracked · May 25, 1999 · N412CE · Boeing 737205 · Fuselage Main, Longeron/Stringer
  > SJO - DURING C-CHECK, STRINGER 17L WAS CRACKED FROM BS 727 TO BS 796. REPAIRED PER EO COO-3-53-334-99 DATED 5/28/99. (M)
- [SDR P2EA99200](https://openairdocs.org/sdr/P2EA99200.md): Angles · cracked · May 21, 1999 · N412CE · Boeing 737205 · Fuselage Miscellaneous Structure
  > SJO - DURING C-CHECK, THE LOWER FUSELAGE, EXTERNAL SKIN DRAG ANGLES AT BS 560, STRINGER 24L WAS FOUND CRACKED. REPAIRED PER, SB 737-53-1031 SECTION III PART III PART II FIG 3 DATED 5/15/98 BY REPLACEMENT OF DRAG ANGLES. (M)
- [SDR P2EA99202](https://openairdocs.org/sdr/P2EA99202.md): Door · cracked · May 20, 1999 · N412CE · Boeing 737205 · Cabin Pressure Control System
  > SJO - DURING C-CHECK, THE LEFT RAM AIR DOOR WAS FOUND CRACKED. REPAIRED PER EO COO-3-52-316-99. (M)
- [SDR P2EA99190](https://openairdocs.org/sdr/P2EA99190.md): Beam · cracked · May 17, 1999 · N412CE · Boeing 737205 · Service Doors
  > SJO - DURNG C-CHECK, THE FORWARD SERVICE DOOR (R1) INTERNAL BEAM NR 7 AFT SECTION IS CRACKED. REPAIRED PER SRM 51-10-03 FIGURE 1. (M)
- [SDR P2EA99192](https://openairdocs.org/sdr/P2EA99192.md): Skin · delaminated · May 12, 1999 · N412CE · Boeing 737205 · Spoilers
  > SJO - DURING C-CHECK, THE NR 8 SPOILER WAS FOUND DELAMINATED. REPAIRED PER COOPESA EO NR COO-CMP-3-57-299-99 DATED MAY 18, 1999. (M)
- [SDR P2EA99191](https://openairdocs.org/sdr/P2EA99191.md): Skin · delamination · May 12, 1999 · N412CE · Boeing 737205 · Spoilers
  > SJO - DURING C-CHECK, THE NR 2 SPOILER, WAS FOUND DELAMINATED. REPAIRED PER COOPESA EO NR COO-CMP-3-57-300-99, DATED MAY 18, 1999. (M)
- [SDR P2EA99203](https://openairdocs.org/sdr/P2EA99203.md): Chord · cracked · May 10, 1999 · N412CE · Boeing 737205 · Fuselage Miscellaneous Structure
  > SJO - DURING C-CHECK, A CHORD WAS FOUND CRACKED AT BS 727, STRINGER 18A, LEFT OUTBOARD SIDE. REPAIRED PER SB 737-53-1088. (M)
- [SDR P2EA99207](https://openairdocs.org/sdr/P2EA99207.md): Frame · cracked · May 8, 1999 · N412CE · Boeing 737205 · Service Doors
  > SJO - DURING C-CHECK, R1 DOOR FORWARD FRAME LOWER REINFORCEMENT WAS CRACKED. REPAIRED PER SRM 51-10-01. (M)
- [SDR P2EA99206](https://openairdocs.org/sdr/P2EA99206.md): Hinge · cracked · May 8, 1999 · N412CE · Boeing 737205 · Spoilers
  > SJO - DURING C-CHECK, LEFT WING NR 1 SPOILER CENTER FITTING WAS CRACKED. FABRICATED FITTING PER EO COO-3-57-301-99. REMOVED AND REPLACED FITTING PER SRM 51-10-01. (M)
- [SDR P2EA99205](https://openairdocs.org/sdr/P2EA99205.md): Beam · cracked · May 8, 1999 · N412CE · Boeing 737205 · Service Doors
  > SJO - DURING C-CHECK, R1 DOOR BEAM NR 6 BETWEEN AFT FRAME AND AFT INTERCOSTAL WAS CRACKED. REPAIRED PER SRM 51-40-03 FIG 1. (M)
- [SDR P2EA99204](https://openairdocs.org/sdr/P2EA99204.md): Frame · cracked · May 8, 1999 · N412CE · Boeing 737205 · Service Doors
  > SJO - DURING C-CHECK, R1 DOOR, AFT FRAME LOWER END WAS CRACKED. REMOVED AND REPLACED FRAME PER SRM 51-10-01. (M)
- [SDR P2EA99201](https://openairdocs.org/sdr/P2EA99201.md): Frame · cracked · May 8, 1999 · N412CE · Boeing 737205 · Service Doors
  > SJO - DURING C-CHECK, R1 DOOR WAS FOUND CRACKED AT FORWARD FRAME LOWER SECTION. REMOVED AND REPLACED FRAME PER SRM 51-10-01. (M)
- [SDR P2EA99196](https://openairdocs.org/sdr/P2EA99196.md): Beam · cracked · May 8, 1999 · N412CE · Boeing 737205 · Passenger/Crew Doors
  > SJO - DURING C-CHECK, R1 DOOR, AFT FRAME, LOWER BEAM REINFORCEMENT WAS CRACKED. REPAIRED PER SRM 51-10-01 PAGE 5 AND 51-30-02. (M)
- [SDR P2EA99194](https://openairdocs.org/sdr/P2EA99194.md): Skin · damaged · May 8, 1999 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - DURNIG C-CHECK, THE LOWER AFT CORNER OF THE FORWARD CARGO COMPARTMENT DOOR CUT OUT WAS FOUND WITH MISSING MATERIAL. REPAIRED DOOR CUT OUT SKIN AND BEARSTRAP BETWEEN BS 477 AND BS 501, FROM STRINGER 23 TO 26R IAW COOPESA EO NR COO-3-53-286-99 AND BOEING
- [SDR P2EA99189](https://openairdocs.org/sdr/P2EA99189.md): Skin · cracked · May 8, 1999 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - DURING C-CHECK, A CRACK WAS FOUND AT THE EXTERNAL FUSELAGE NR 3 WINDOW CUTOUT. REPAIRED PER S/B 737-53-1115 DATED JAN 2, 1988, SECTION II FIG 3. (M)
- [SDR P2EA99187](https://openairdocs.org/sdr/P2EA99187.md): Skin · cracked · May 8, 1999 · N412CE · Boeing 737205 · Service Doors
  > SJO - DURING C-CHECK, A CRACK WAS FOUND ON THE R1 DOOR, EXTERNAL SKIN, NEAR THE LOWER HINGE, LENGTH.5 INCH. REPAIRED PER SRM 52-00-3 FIG 6. (M)
- [SDR P2EA99198](https://openairdocs.org/sdr/P2EA99198.md): Beam · cracked · May 7, 1999 · N412CE · Boeing 737205 · Fuselage Miscellaneous Structure
  > SJO - DURING C-CHECK, LEFT WHEEL WELL SHEAR BEAM BS 668, LBL 65, WL 194 WAS FOUND CRACKED. REPAIRED PER BOEING S/B 737-53-1066 REV 3 DATED 02/25/93, SECTION III AND PART III. (M)
- [SDR P2EA99197](https://openairdocs.org/sdr/P2EA99197.md): Stringer · cracked · May 7, 1999 · N412CE · Boeing 737205 · Fuselage Main, Longeron/Stringer
  > SJO - DURING C-CHECK, SKIN AT BS 727 'A' BETWEEN STRINGER 14R AND 16R WAS FOUND CRACKED IN TWO PLACES. REPAIRED PER EO COO-SJO-99-0628RR DATED 05/20/99. (M)
- [SDR P2EA99193](https://openairdocs.org/sdr/P2EA99193.md): Skin · corroded · May 7, 1999 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - DURING C-CHECK, THE FORWARD LAVATORY SERVICE PANEL CUT OUT SKIN WAS FOUND CORRODED. THE EXTERNAL FUSELAGE SERVICE PANEL DOUBLER WAS REPLACED PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M)
- [SDR P2EA99188](https://openairdocs.org/sdr/P2EA99188.md): Rib · cracked · May 7, 1999 · N412CE · Boeing 737205 · Wing, Rib/Bulkhead
  > SJO - DURNG C-CHECK, WHILE INSPECTING THE LEFT WING TO BODY RIB CHORD AT BS 665, BBL 70.85, A CRACK WAS NOTED ON THE HORIZONTAL FLANGE. LENGTH 2 INCH. THAT CRACK ENDED IN A FASTENER HOLE. THIS DAMAGE IS ACCEPTABLE BUT REQUIRES REINSPECTION AT 1500 CYCLE INT
- [SDR P2EA99183](https://openairdocs.org/sdr/P2EA99183.md): Switch · failed · May 2, 1999 · N412CE · Boeing 737205 · Engine Start Valves/Controls
  > ATL - FLT 301 - NR 1 ENGINE START LIGHT ILLUMINATED ON TAKEOFF. REJECTED TAKEOFF. LIGHT WENT OUT WHEN ENGINES CAME TO IDLE. REPLACED NR 1 ENGINE START VALVE AND START VALVE PRESSURE SWITCH. START VALVE LIGHT OPS CHECK OK. (M)
- [SDR P2EA99208](https://openairdocs.org/sdr/P2EA99208.md): Skin · cracked · Apr 14, 1999 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - DURING C-CHECK, LEFT EXTERNAL SKIN WAS CRACKED THREE PLACES FROM BS 727 TO 727 'A' AND STRINGER 14L TO 17L REPAIRED PER EO COO-3-53-314-99 DATED 5/22/99. (M)
- [SDR P2EA99132](https://openairdocs.org/sdr/P2EA99132.md): Valve · lack of lube · Apr 11, 1999 · N412CE · Boeing 737205 · Engine Start Valves/Controls
  > PIT - FLT 707 - AS POWER WAS APPLIED FOR TAKEOFF, NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. INDICATION WAS ACCOMPANIED BY A POPPING SOUND. CLEANED AND LUBED NR 1 PRESSURE REGULATING SHUTOFF VALVE. OPS CHECK NORMAL. (M)
- [SDR P2EA99003](https://openairdocs.org/sdr/P2EA99003.md): Skin · damaged · Jan 13, 1999 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > MDW - FLT 374 - AIRCRAFT SKIN DAMAGED BY BAGGAGE TUG (CART) AT STATION 380 RT, WL 185. REPAIRED PER SRM 53-30-3, FIG 1. (M)
- [SDR P2EA98175](https://openairdocs.org/sdr/P2EA98175.md): Door Warning · malfunctioned · Sep 29, 1998 · N412CE · Boeing 737205 · Door Warning System
  > MCI - FLT 301 - AIR RETURN, NO EMERGENCY DECLARED, LANDING UNEVENTFUL. AFT CARGO DOOR LIGHT CAME ON AFTER TAKEOFF, AIRCRAFT WAS NOT PRESSURIZING. RETURNED TO MCI. CHECKED AFT CARGO DOOR PROXIMITY SWITCH AND TARGET. NO DEFECTS FOUND, AFT CARGO DOOR WARNING
- [SDR P2EA98156](https://openairdocs.org/sdr/P2EA98156.md): Door · cracked · Aug 11, 1998 · N412CE · Boeing 737205 · Landing Gear Doors
  > MCI - RIGHT NLG DOOR LOWER FORWARD CORNER HAS DAMAGE. INSPECT RIGHT NLG DOOR FORWARD HINGE FITTING FOR CRACKS. REPLACED RIGHT NLG DOOR AND PERFORMED GEAR SWING PER MM 32-22-11. WHILE RIGHT NLG DOOR WAS REMOVED, PERFORMED VISUAL AND DYE PENETRANT INSPECTION
- [SDR P2EA98105](https://openairdocs.org/sdr/P2EA98105.md): Uplock Sensor · out of adjust · May 8, 1998 · N412CE · Boeing 737205 · Landing Gear Position and Warning
  > MCI - FLT 917 - LEFT GEAR RED LIGHT ILLUMINATED. GEAR HANDLE PLACED DOWN, RED LIGHT OUT, GREEN LIGHT ON. ADJUSTED UPLOCK SENSOR PER MM 32-61-21 AND PERFORMED GEAR SWING TO VERIFY OPERATION. (M)
- [SDR P2EA98102](https://openairdocs.org/sdr/P2EA98102.md): Wire · damaged · May 4, 1998 · N412CE · Boeing 737205 · Landing Gear System Wiring
  > FLT 119 - ATL - NO EMERGENCY DECLARED, LANDING NORMAL. LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATES INTERMITTENTLY, IN UP AND OFF POSITIONS. FOUND BLUE WIRE TO UPLOCK SENSOR PINCHED IN ADELL CLAMP IN LT W/W, WHEN GROUNDED ON BARE WIRE RED LIGHT FOR LEFT MAIN GEAR
- [SDR P2EA98096](https://openairdocs.org/sdr/P2EA98096.md): Skin · cracked · Apr 7, 1998 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - EXTERIOR FUSELAGE SKIN CRACKED AT BS 830, STRINGER 14RT. REPAIRED FUSELAGE SKIN SECTION FROM BS 827 TO BS 847, BETWEEN STRINGER 11RT AND STRINGER 14 RT, PER BOEING FAX COO-SJO-98-0296RR DATED 4-3-98. DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTE
- [SDR P2EA98070](https://openairdocs.org/sdr/P2EA98070.md): Chord · cracked · Apr 4, 1998 · N412CE · Boeing 737205 · Trailing Edge Flaps
  > SJO - Q-CHECK, RIGHT WING INBOARD TRAILING EDGE MID FLAP 'T' CHORD CRACKED AT WBL 87.73. REPAIRED MID FLAP TRAILING EDGE PER SRM 51-10-1 FIG PAGE 5. RIVETS REPLACED PER SRM 51-30-2. (M)
- [SDR P2EA98076](https://openairdocs.org/sdr/P2EA98076.md): Frame · corroded · Apr 3, 1998 · N412CE · Boeing 737205 · Fuselage Main, Frame
  > SJO - Q-CHECK, WINDOW FRAME (24LT) WITH PROVISIONAL REPAIR AND CORRODED BEYOND LIMITS, BS 747. REPLACED WINDOW FRAME BETWEEN BS 747 AND BS 767 PER SRM 51-10-1 PAGE 5. (M)
- [SDR P2EA98082](https://openairdocs.org/sdr/P2EA98082.md): Skin · cracked · Apr 1, 1998 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - Q-CHECK, EXTERIOR FUSELAGE SKIN CRACKED AT BS 765 BETWEEN STRINGER 13 LT AND 14 LT. REPAIRED FUSELAGE SKIN SECTION FROM BS 727B PLUS 15 TO BS 767 BETWEEN STRINGER 10 LT AND STRINGER 14 LT PER COOPESA EO NR COO-3-53-199-98 DATED APR 2, 1998, SKETCH SKCOO
- [SDR P2EA98075](https://openairdocs.org/sdr/P2EA98075.md): Chord · corroded · Apr 1, 1998 · N412CE · Boeing 737205 · Fuselage Miscellaneous Structure
  > Q-CHECK, NOSE LANDING GEAR WHEEL WELL TORQUE BOX RIGHT LOWER 'T' CHORD CORRODED BEYOND LIMITS AT BS 227.8. REPLACED T-CHORD BETWEEN BS 227.8 AND BS 294.5, WL 157, RBL 15 PER SRM 51-10-1 PAGE 5. (M)
- [SDR P2EA98074](https://openairdocs.org/sdr/P2EA98074.md): Chord · corroded · Apr 1, 1998 · N412CE · Boeing 737205 · Fuselage Miscellaneous Structure
  > SJO - Q-CHECK, NOSE LANDING GEAR WHEEL WELL TORQUE BOX LOWER LEFT 'T' CHORD CORRODED BEYOND LIMITS AT BS 229.8. FABRICATED 'T' CHORD PER SRM 51-20-1, 51-10-1, 51-10-3, 51-10-2. REPLACED CHORD FROM BS 227.8 TO BS 294.5, WL 157, LBL 15 INCHES PER SRM 51-10-1.
- [SDR P2EA98063](https://openairdocs.org/sdr/P2EA98063.md): Frame · cracked · Mar 31, 1998 · N412CE · Boeing 737205 · Fuselage Miscellaneous Structure
  > SJO - Q-CHECK, FORWARD CARGO DOOR FRAME CRACKED FROM BEAM NR 4 TO BEAM NR 5, INNER SKIN CRACKED BETWEEN BEAM NR 5 AND THE LOWER FRAME. FABRICATED AND REPAIRED NR 5 BEAM PER SRM 51-10-1 PAGE 5, 51-20-1, 51-10-3, BAC 5602, 51-10-2. REPAIRED/REINFORCED PER SB 7
- [SDR P2EA98095](https://openairdocs.org/sdr/P2EA98095.md): Floorbeam · corroded · Mar 30, 1998 · N412CE · Boeing 737205 · Fuselage Main, Floor Beam
  > Q-CHECK ITEM, FLOORBEAM CORRODED BEYOND LIMITS BETWEEN BS 967.5 AND 986.6, RBL 20 WL 208.1. REPAIRED FLOORBEAM BETWEEN BS 967.5 AND BS 986.6 RBL 20 PER BOEING FAX COO-SJO-98-0178RR DATED ON 3-1398. DOCUMENTED ON FAA FOR 8110-3. APPROVED AND SUBMITTED BY FAA
- [SDR P2EA98069](https://openairdocs.org/sdr/P2EA98069.md): Fitting · cracked · Mar 27, 1998 · N412CE · Boeing 737205 · Galley Doors
  > SJO - Q-CHECK, FORWARD GALLEY DOOR (R1) FITTING CRACKED BS 290, STRINGER 8RH. REPLACED FITTING REPLACED PER SRM 51-10-1 FIG PAGE 6. RIVETS REPLACED PER SRM 51-30-2. (M)
- [SDR P2EA980667](https://openairdocs.org/sdr/P2EA980667.md): Fitting · cracked · Mar 27, 1998 · N412CE · Boeing 737205 · Fuselage Miscellaneous Structure
  > SJO - Q-CHECK, FORWARD GALLEY DOOR, LOWER HINGE SUPPORT FITTING CRACKED AT BS 290, STRINGER 14RT. REPLACED FITTING PER SRM 51-10-1, PAGE 6. RIVETS REPLACED PER SRM 51-30-2. (M)
- [SDR P2EA98066](https://openairdocs.org/sdr/P2EA98066.md): Skin · cracked · Mar 27, 1998 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - Q-CHECK, EXTERIOR FUSELAGE SKIN CRACKED BETWEEN BS 500 PLUS 9 INCHES TO BS 500A PLUS 2 INCHEC, STRINGER 12 RT AND STRINGER 14 RT. REPAIRED FUSELAGE SKIN SECTION PER SRM 53-30-3 FIG 38. (M)
- [SDR P2EA98065](https://openairdocs.org/sdr/P2EA98065.md): Skin · cracked · Mar 27, 1998 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - Q-CHECK, EXTERIOR FUSELAGE SECTION CRACKED AT TWO POSITIONS BETWEEN BS 458 AND BS 491, STRINGER 10 RT TO STRINGER 14 RT. REPAIRED FUSELAGE SKIN SECTION PER SRM 53-30-3 FIG 38. (M)
- [SDR P2EA98060](https://openairdocs.org/sdr/P2EA98060.md): Fitting · cracked · Mar 26, 1998 · N412CE · Boeing 737205 · Fuselage Miscellaneous Structure
  > SJO - Q-CHECK, AFT GALLEY DOOR LOWER HINGE SUPPORT FITTING CRACKED, BS 954, STRINGER 14 RT. REPLACED HINGE SUPPORT FITTING PER SRM 51-10-1 PAGE 5. RIVETS REPLACED PER SRM 51-30-2. (M)
- [SDR P2EA98071](https://openairdocs.org/sdr/P2EA98071.md): Skin · corroded · Mar 25, 1998 · N412CE · Boeing 737205 · Fuselage Main, Plate/Skin
  > SJO - Q-CHECK, UPPER FUSELAGE SKIN CORRODED BEYOND LIMITS AT BS 1104, STRINGER 5 LT AND STRINGER 6LT. REPAIRED FUSELAGE SKIN SECTION FROM BS 1098 TO BS 1111, BETWEEN STRINGER 5 LT AND STRINGER 6 LT PER SRM 53-30-3, PAGE 26 FIG 1 SHEET 4. (M)

Next page: https://openairdocs.org/deregistered/N412CE-2013-07-29/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 = 'N412CE' AND deregistration_id = 'N412CE-2013-07-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N412CE-2013-07-29/reports

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