# Service difficulty reports: N344TM, cancelled Dec 28, 2005

A list on [N344TM, cancelled Dec 28, 2005](https://openairdocs.org/deregistered/N344TM-2005-12-28.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 · 81 reports

- [SDR BJNA051201](https://openairdocs.org/sdr/BJNA051201.md): Connector · dirty · Dec 2, 2005 · N344TM · Boeing 737282 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ILLUMINATED 2 TIMES ON DESCENT. CLEANED THE CONNECTORS ON THE COCKPIT REMOVABLE EMERGENCY EXIT LIGHT, SYSTEM CHECKS NORMAL. (K)
- [SDR BJNA05021](https://openairdocs.org/sdr/BJNA05021.md): Engine · failed · Feb 11, 2005 · N344TM · Boeing 737282 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED ON THE BEGINNING OF TAKEOFF ROLL, 1.6 EPR HARD COMPRESSOR STALL AND ROLL DOWN. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. ENGINE TOTAL TIME 550207, TOTAL CYCLES 52176. SINCE
- [SDR BJNA050103](https://openairdocs.org/sdr/BJNA050103.md): Line · leaking · Jan 26, 2005 · N344TM · Boeing 737282 · Turbine Engine Oil System
  > NR 1 ENGINE LOST ENGINE OIL QUANTITY AND ILLUMINATED THE LOW OIL PRESSURE LIGHT. ENGINE WAS SHUTDOWN AND WIND MILLED APPROX 20 MIN. INSPECTION FOUND THE ENGINE GEARBOX P-5 PORT THREADS STRIPPED AND THE PORTS BANJO FITTING FOR THE OIL PRESSURE SWITCH LINE LEA
- [SDR BJNA050102](https://openairdocs.org/sdr/BJNA050102.md): Battery Pack · discharged · Jan 21, 2005 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A MAINTENANCE WALK AROUND CHECK, THE LT SERVICE DOOR L2 EMERGENCY EXIT LIGHT WOULD NOR ILLUMINATE. MAINTENANCE DISCOVERED THAT THE BATTERIES WERE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK OF THE L2 EMERGENCY EXIT LIGHT IAW MM. LIG
- [SDR BJNA050101](https://openairdocs.org/sdr/BJNA050101.md): Bulb · burned out · Jan 8, 2005 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A MAINTENANCE WALK AROUND CHECK, THE LT SERVICE DOOR L2 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB OF THE L2 EMERGENCY EXIT LIGHT IAW MM. LIGHT NOW FUNCTIONS NORMALLY. (K)
- [SDR BJNA041201](https://openairdocs.org/sdr/BJNA041201.md): Battery Pack · discharged · Dec 15, 2004 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A PREFLIGHT WALK AROUND INSPECTION THE NR 1 OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT BATTERY PACK IAW MM. EMERGENCY EXIT LIGHTS NO OPERATE NORMALLY. (K)
- [SDR BJNA041003](https://openairdocs.org/sdr/BJNA041003.md): Bulb · burned out · Oct 10, 2004 · N344TM · Boeing 737282 · Emergency Lighting
  > LT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT BULB AND CLEANED SOCKET IAW AMM 33-51-101.
- [SDR BJNA040904](https://openairdocs.org/sdr/BJNA040904.md): Battery Pack · inoperative · Sep 19, 2004 · N344TM · Boeing 737282 · Emergency Equipment
  > FOUND CABIN EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M)
- [SDR BJNA040809](https://openairdocs.org/sdr/BJNA040809.md): Floor Support · corroded · Aug 25, 2004 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 12 WITH LEVEL 2 CORROSION. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW BOEING 737 STRUCTURAL REPAIR MANUAL 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2
- [SDR BJNA040807](https://openairdocs.org/sdr/BJNA040807.md): Door Frame · cracked · Aug 25, 2004 · N344TM · Boeing 737282 · Fuselage Main, Structure
  > DURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER FORWARD CORNER FRAME CRACKED. INSTALLED NEW LOWER FORWARD CORNER AT C1 DOOR IAW SRM 51-20-1 AND SERVICE BULLETIN 737-52A1100 REV 4. (M) BJNA
- [SDR BJNA040808](https://openairdocs.org/sdr/BJNA040808.md): Door Frame · cracked · Aug 25, 2004 · N344TM · Boeing 737282 · Fuselage Main, Structure
  > DURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER AFT CORNER FRAME CRACKED. INSTALLED NEW LOWER AFT CORNER AT C1 DOOR IAW SRM 51-20-1 AND SB 737-52A1100 REV 4. (M) BJNA
- [SDR BJNA040804](https://openairdocs.org/sdr/BJNA040804.md): Floor Support · corroded · Aug 13, 2004 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-19222 IAW THE BOEING 737 STRUCTRUAL REPAIR MANUAL 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2. (M)BJNA
- [SDR BJNA040805](https://openairdocs.org/sdr/BJNA040805.md): Floor Support · corroded · Aug 13, 2004 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 LBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW THE SRM 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2. (M)
- [SDR BJNA040803](https://openairdocs.org/sdr/BJNA040803.md): Intercostal · corroded · Aug 12, 2004 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 306 LBL 12. REMOVED AND REPLACED FLOORBEAM INTERCOSTAL AT BS 306 LBL 12 IAW THE STRUCTURAL REPAIR MANUAL 53-30-2. (M)
- [SDR BJNA040901](https://openairdocs.org/sdr/BJNA040901.md): Crossbeam · cracked · Aug 6, 2004 · N344TM · Boeing 737282 · Cargo/Baggage Doors
  > DURING C-CHECK INSPECTION FOUND C-1 DOOR LOWER CROSS BEAM HAS WEB CRACK NEAR AFT CORNER. FABRICATED FILLER,.875 INCH BY 5 INCH AND 5 INCH BY 4 INCH MATERIAL USED 2024T3.050. INSTALLED REPAIR IAW SB 737-52A1100, REV 4 AND SRM 51-30-2 AND 51-10-2. (M)
- [SDR BJNA040902](https://openairdocs.org/sdr/BJNA040902.md): Skin · cracked · Aug 6, 2004 · N344TM · Boeing 737282 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BOTTOM OF L1 DOOR CUT OUT BS 336. INSTALLED DOUBLER AND STRAP AT L1 DOOR LOWER CUTOUT IAW SB 737-53-1083 REV 3. (M)
- [SDR BJNA040802](https://openairdocs.org/sdr/BJNA040802.md): Skin · cracked · Aug 6, 2004 · N344TM · Boeing 737282 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT LOWER AFT CORNER OF R1 DOOR CUTOUT AT BS 344. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30-3 FIG 26. (M)
- [SDR BJNA040801](https://openairdocs.org/sdr/BJNA040801.md): Skin · cracked · Aug 6, 2004 · N344TM · Boeing 737282 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT L1 DOOR LOWER HINGE CUTOUT AT BS 304. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30-3 FIGURE 31. (M)
- [SDR BJNA040503](https://openairdocs.org/sdr/BJNA040503.md): Light · burned out · May 12, 2004 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A MAINTENANCE WALK AROUND CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP OF THE AFT SECTION OF EMERGENCY FLOOR TRACK IAW EEL COMPONENT MAINTENANCE MANUAL 33-50-01. SYSTEM NOW C
- [SDR BJNA040502](https://openairdocs.org/sdr/BJNA040502.md): Actuator · leaking · May 3, 2004 · N344TM · Boeing 737282 · Drag Control System
  > AFTER TAKEOFF, FLT CREW NOTICED HYD SYSTEM-A QUANTITY LOSS. A/C RETURNED TO MFE & MADE UNEVENTFUL OVERWEIGHT LANDING. B AND STANDBY HYD SYS NOT AFFECTED. MX DISCOVERED FLUID LEAKING FROM SHAFT SEALS ON NR 4 SPOILER ACTUATOR. SPOILER ACTUATORS ARE UNDER A-S
- [SDR BJNA040202](https://openairdocs.org/sdr/BJNA040202.md): Wire · loose · Feb 24, 2004 · N344TM · Boeing 737282 · Light System Wiring
  > FORWARD FLOOR TRACK LIGHTING INOPERATIVE. INSPECTED THE EMERGENCY LIGHT POWER SUPPLY FOUND WIRE PULLED FROM THE CONNECTOR, REPLACED THE POWER SUPPLY, OPS CHECK OK. (M)
- [SDR BJNA040203](https://openairdocs.org/sdr/BJNA040203.md): Power Supply · inoperative · Feb 23, 2004 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND THE EMERGENCY BATTERY PACK IAW BOEING MM 33-51-0, SYSTEM NOW CHECKS NORMAL.
- [SDR BJNA040102](https://openairdocs.org/sdr/BJNA040102.md): Connector · inoperative · Jan 28, 2004 · N344TM · Boeing 737282 · Electrical Connectors
  > DURING A MAINTENANCE WALKAROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTORS ON THE FORWARD BATTERY CHARGER AND OPERATIONALLY CHECKED SYSTEM. SYSTEM CHECKED NORMAL. WORK IAW MANUFACTURES
- [SDR BJNA031101](https://openairdocs.org/sdr/BJNA031101.md): Battery Pack · inoperative · Nov 9, 2003 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A SCHEDULED MAINTENANCE CHECK THE EMERGENCY EXIT LIGHTS AT DOOR R-2, AND L2 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE R-2, AND L2 EMERGENCY BATTERY PACK IAW BOEING MM 33-51-01, LIGHTS NOW ILLUMINATE. (M)
- [SDR BJNA030801](https://openairdocs.org/sdr/BJNA030801.md): Bearing · failed · Aug 13, 2003 · N344TM · Boeing 737282 · Turbine Engine Oil System
  > AT FL 310, NR 1 ENGINE OIL PRESSURE NOTICED DROPPING, OIL QUANTITY WENT TO HALF GALLON, AND OIL TEMPERATURE ROSE TO THE YELLOW BAND. ENGINE WAS SHUTDOWN, LOW OIL PRESSURE LIGHT CAME ON AND THE ENGINE WIND-MILLED ABOUT 23 MINUTES AT 5-8 PSI OIL PRESSURE. DISA
- [SDR BJNA030700](https://openairdocs.org/sdr/BJNA030700.md): Light · inoperative · Jul 14, 2003 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A MAINTENANCE PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT LOCATED BY THE LEFT AFT ENTRY DOOR EXTERIOR WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BULB IAW BOEING MM 33-51-0, SYSTEM NOW CHECKS NORMALLY. (M)
- [SDR BJNA030601](https://openairdocs.org/sdr/BJNA030601.md): Odor · detected · Jun 10, 2003 · N344TM · Boeing 737282 · Air Distribution System
  > BURNING ODOR IN COCKPIT AND CABIN ON TAKEOFF. INSPECTED AIRCRAFT, RAN ENGINES, CHECKED AIR CONDITIONING PACKS AND VENTILATION SYSTEM. UNABLE TO DUPLICATE, NO FAULTS FOUND. (M)
- [SDR BJNA030501](https://openairdocs.org/sdr/BJNA030501.md): Gearbox · leaking · May 6, 2003 · N344TM · Boeing 737282 · Turbine Engine Accessory Drive
  > NR 2 ENGINE DEVELOPED OIL LEAK IN FLIGHT, ENGINE SHUT DOWN, AIRCRAFT LANDED WITHOUT INCIDENT. FOND THE ENGINE GEARBOX P-5 PORT THREADS STRIPPED, OIL LEAKING AROUND THE PORTS BANJO FITTING FOR THE OIL PRESSURE SWITCH'S OIL LINE. INSTALLED A HELICAL COIL IAW P
- [SDR BJNA021202](https://openairdocs.org/sdr/BJNA021202.md): Battery Pack · discharged · Dec 30, 2002 · N344TM · Boeing 737282 · Emergency Lighting
  > LT EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT OVERWING EXIT. REPLACE LT EXTERIOR EMERGENCY BATTERY PACK POWER SUPPLY IN THE AFT CARGO PIT IAW MM.
- [SDR BJNA021102](https://openairdocs.org/sdr/BJNA021102.md): Cover · broken · Nov 10, 2002 · N344TM · Boeing 737200 · Turbine Engine Air Inlet Section
  > HARD COMPRESSOR STALL ON NR 1 ENGINE AT 2.20 EPR - 96 PERCENT N1 - 20 KNOTS SPEED, POWER WAS PULLED TO IDLE WITHIN 300 FT OF TAKE OFF ROLL, TAKE OFF ABORTED. ENGINE INSPECTION: NOSE CONE OFF AND DAMAGED BASEBALL SIZE DAMAGE TO INNER LINER AND HONEYCOMB STRUC
- [SDR BJNA021001](https://openairdocs.org/sdr/BJNA021001.md): Case · damaged · Oct 9, 2002 · N344TM · Boeing 737282 · Turbine Engine Compressor Section
  > ON TAKEOFF ROLL AT 115 KNOTS AIRCRAFT VEERED TO THE LT, CAPTAIN REPORTED HEARING A LOUD BANG. ABORTED TAKEOFF. MAINTENANCE REPORTED MAJOR DAMAGE TO TURBINE SECTION OF ENGINE. UPON FURTHER INSPECTION REVEALED THAT ALL DAMAGE WAS TOTALLY CONTAINED TO THE ENGI
- [SDR BJNA020832](https://openairdocs.org/sdr/BJNA020832.md): Spar · corroded · Aug 27, 2002 · N344TM · Boeing 737282 · Horizontal Stabilizer, Spar/Rib
  > FOUND LT HORIZONTAL STAB CENTER SECTION REAR SPAR TOP CHORD FORWARD LUG HAS LEVEL 2 CORROSION INSIDE BORE. REMOVED CORROSION BORED I/D OF LUG TO 1.564 INCH, ROTO TREATED AND INSTALLED BUSHING. (M)
- [SDR BJNA020828](https://openairdocs.org/sdr/BJNA020828.md): Frame · corroded · Aug 16, 2002 · N344TM · Boeing 737282 · Fuselage Main, Frame
  > FOUND LEVEL 2 CORROSION UNDER 3 EACH SCREW HOLES AT FRAME RBL 28 BETWEEN BS 955 TO BS 967. REMOVED FRAME ORDERED AND RECEIVED NEW FRAME (BEAM) DRILLED, DEBBARRD, TREATED PRIMED AND INSTALLED IAW B737-200 SRM 51-10-6 PAGE 12, 51-30-2 PAGE 3, AND B737 MM 51-21-
- [SDR BJNA020827](https://openairdocs.org/sdr/BJNA020827.md): Beam · corroded · Aug 15, 2002 · N344TM · Boeing 737282 · Fuselage Main, Structure
  > FOUND LEVEL 2 CORROSION 4 EACH PLACES ON UPPER SURFACE OF BEAM 294.5 BETWEEN LBL 10 TO RBL 20. REMOVED CORROSION AND TREAT. REPAINT SURFACE CHECK LIMITS. (M)
- [SDR BJNA020824](https://openairdocs.org/sdr/BJNA020824.md): Frame · corroded · Aug 15, 2002 · N344TM · Boeing 737282 · Fuselage Main, Frame
  > FOUND FRAME AT STATION 328 HAS SURFACE CORROSION AROUND FASTENER HOLES ON UNDER SIDE OF FRAME. LEVEL 2 CORROSION. REMOVED CORROSION AT 328 FABRICATED REPAIR ANGLES IAW B737 SRM 53-10-9 PAGE 26. (M)
- [SDR BJNA020818](https://openairdocs.org/sdr/BJNA020818.md): Panel · corroded · Aug 14, 2002 · N344TM · Boeing 737282 · Fuselage Main, Plate/Skin
  > FOUND CORROSION IN FORWARD PIT LEFT SIDE TRANSITION PANEL FROM STATION 500B TO 520, LEVEL 2 CORROSION. REMOVED OLD TRANSITION PANEL, FABRICATED NEW SECTION OF PANEL, INSTALLED NEW SECTION OF TRANSITION PANEL LEFT STATION 500B TO 520 IAW B737 SRM 51-402 FIGURE
- [SDR BJNA020833](https://openairdocs.org/sdr/BJNA020833.md): Skin · corroded · Aug 12, 2002 · N344TM · Boeing 737282 · Fuselage Main, Plate/Skin
  > FORWARD FRAME OF THE C-2 DOOR CUT OUT ABOVE TRANSITION PANEL HAS LEVEL 2 CORROSION. REMOVED CORRODED FRAME IAW 737 SRM 51-30-2 AND REO L00 588. REPAIRED FRAME IAW REO L00 588 REV IR. FABRICATED FRAME SPLICES AND INSTALLED IAW REO L00588 AND B737 SRM 51-20-1
- [SDR BJNA020831](https://openairdocs.org/sdr/BJNA020831.md): Frame · corroded · Aug 10, 2002 · N344TM · Boeing 737282 · Fuselage Main, Frame
  > FOUND LEVEL 2 CORROSION FORWARD PIT STATION 500 RBL 12 FRAME LOWER LEG. CORROSION REMOVED AND FOUND REMAINING MATERIAL OUT OF LIMITS, FABRICATED, TRIMMED DRILLED, ALODINED PRIMED AND INSTALLED REPAIR IAW B737 SRM 51-10-6, 53-10-1, 53-10-4 FIGURE 6 PAGE 13-15.
- [SDR BJNA020813](https://openairdocs.org/sdr/BJNA020813.md): Door Frame · gouged · Aug 9, 2002 · N344TM · Boeing 737282 · Fuselage Main, Structure
  > FOUND RIGHT SIDE FORWARD EDGE OF AFT CARGO DOOR OPENING IS GOUGED AND TORN. CUT OUT DAMAGED AREA AND FABRICATED STACKED DOUBLER REPAIR PER B737 SRM 53-30-3 FIG 46. INSTALLED REPAIR PER B737 SRM 31-30-2, 51-20-4, 53-30-3 FIG 46. (M)
- [SDR BJNA020810](https://openairdocs.org/sdr/BJNA020810.md): Seat Track · corroded · Aug 8, 2002 · N344TM · Boeing 737282 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION ON SEAT TRACK AT RBL 32 AT BS 328, LEVEL 2 CORROSION. FOUND CORROSION ON SEAT TRACK OUT OF LIMITS, CUT NEW TRACK FROM BAC1520-792 16 INCH INSTALLED IAW 727 SRM 51-10-2, 51-10-1 AND 51-30-2. (M)
- [SDR BJNA020825](https://openairdocs.org/sdr/BJNA020825.md): Stringer · corroded · Aug 7, 2002 · N344TM · Boeing 737282 · Fuselage Main, Longeron/Stringer
  > AFT AIRCRAFT INSIDE RIGHT SIDE STRINGER 17 AT FS 986.5 UNDER CUSP LONGERON HAS LEVEL 2 CORROSION. REMOVED CORROSIN FABRICATED AND INSTALLED NEW CUSP WEB IAW B737 SRM 51-20-1, 53-10-2, FIGURE 5, 53-10-1 FIGURE 1 AND 51-10-6. (M)
- [SDR BJNA020812](https://openairdocs.org/sdr/BJNA020812.md): Tie Clip · cracked · Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > FOUND TENSION TIE FITTING AT STA 104 STR 19L AND 20L CRACKED ON CORNER. LEVEL 2 CORROSION. REMOVED SECTION OF STATION 19L AT FS 104 FABRICATED REPAIR SECTION OF STATION AND TIE CLIP AT 19L AND 1104 TREATED, PRIMED AND INSTALLED STRINGER, SPLICES SECTION AND
- [SDR BJNA020811](https://openairdocs.org/sdr/BJNA020811.md): Shear Tie · corroded · Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Main, Structure
  > FOUND CORROSION IN FORWARD PIT AT STA 500 LBL 2 TO RBL 2 FRAME LOWER LEG, LEVEL 2 CORROSION. CUT AND REMOVED CORROSION FROM SHEAR TIE LEG. FABRICATED AND INSTALLED SHEAR TIE REPAIR AND DOUBLER IAW SRM.
- [SDR BJNA020820](https://openairdocs.org/sdr/BJNA020820.md): Floor Support · corroded · Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > FORWARD PIT FLOOR SUPPORT BS 520 LBL 17 TO LBL 20 LEVEL 2 CORROSION AROUND 4 EACH NUT CLIPS AND 1 MISSING. REMOVED CORROSION FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR IAW 737 SRM 51-10-2, 51-30-2, 51-40-4, FIGURE 1 AND 53-10-1. (M)
- [SDR BJNA020819](https://openairdocs.org/sdr/BJNA020819.md): Angle · corroded · Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Main, Frame
  > FORWARD PIT BS 500 RBL 28 FRAME SUPPORT LOWER LEG FORWARD AND AFT HAS LEVEL 2 CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED ANGLE REPAIR IAW B737 SRM 51-20-01, 51-10-6, AND 51-10-1. (M)
- [SDR BJNA020823](https://openairdocs.org/sdr/BJNA020823.md): Torque Box · corroded · Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > FOUND BS 1100 LEFT TOP CORNER OF TORQUE BOX NUT PLATE HAS LEVEL 2 CORROSION. CUT OUT CORRODED AREA FABRICATED AND INSTALLED FILLER ANGLE AND RADIUS BLOCK IAW B737 SRM 51-40-5, FIGURE 1 PAGE 1. (M)
- [SDR BJNA020822](https://openairdocs.org/sdr/BJNA020822.md): Torque Box · gouged · Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > FOUND BS 1104 TORQUE BOX LEFT CENTER SIDE HAS DEEP GOUGE. CUT OUT GOUGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW B737 SRM 51-40-2 FIGURE 1 PAGE 1-3. (M)
- [SDR BJNA020821](https://openairdocs.org/sdr/BJNA020821.md): Stringer · gouged · Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Main, Longeron/Stringer
  > TAIL COMPARTMENTS BS 1044 STRINGER 26L HAS DEEP CHAFE FROM BLEED AIR DUCT. CUT OUT CHAFED SECTION OF STRINGER, FABRICATED AND INSTALLED STRINGER REPAIR IAW 53-10-3, 51-30-2 FIGURE 1 SHEETS 1 THROUGH 8. (M)
- [SDR BJNA020809](https://openairdocs.org/sdr/BJNA020809.md): Structure · corroded · Aug 6, 2002 · N344TM · Boeing 73728 · Fuselage Main, Structure
  > FOUND CORROSION ON 4 SCREW HOLES AT RBL 20 BETWEEN BS 986.5 TO BS 967, CORROSION LEVEL 2. (M)
- [SDR BJNA020806](https://openairdocs.org/sdr/BJNA020806.md): Frame · corroded · Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Main, Frame
  > CORROSION ON FRAME RBL 8 NEAR BEAM BS 967. REMOVED 18.8750 INCH SECTION, FABRICATED AND INSTALLED REPAIR SECTION OF FRAME IAW SRM.

Next page: https://openairdocs.org/deregistered/N344TM-2005-12-28/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 = 'N344TM' AND deregistration_id = 'N344TM-2005-12-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N344TM-2005-12-28/reports

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