# Service difficulty reports: N233TM, cancelled Nov 21, 2005 A list on [N233TM, cancelled Nov 21, 2005](https://openairdocs.org/deregistered/N233TM-2005-11-21.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 BJNA051101](https://openairdocs.org/sdr/BJNA051101.md): Landing Gear · unknown · Nov 9, 2005 · N233TM · Boeing 737282 · Main Landing Gear > AFTER TAKEOFF, RETRACTED LANDING GEAR AND 3 RED LIGHTS REMAINED ILLUMINATED. CYCLED LANDING GEAR DOWN AND UP, 3 GREEN LIGHTS WHEN DOWN, 3 RED LIGHTS WHEN UP. LANDED WITH 3 GREEN LIGHTS. PERFORMED LANDING GEAR ACCY MODULE TEST IAW AMM, COULD NOT DUPLICATE ON - [SDR BJNA050301](https://openairdocs.org/sdr/BJNA050301.md): Battery Pack · discharged · Mar 16, 2005 · N233TM · Boeing 737282 · Emergency Lighting > RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE RIGHT OVERWING EXIT LIGHT BATTERY IAW 33-51-21. (M) - [SDR BJNA050203](https://openairdocs.org/sdr/BJNA050203.md): Battery Pack · discharged · Feb 27, 2005 · N233TM · Boeing 737282 · Emergency Equipment > CABIN EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M) - [SDR BJNA050104](https://openairdocs.org/sdr/BJNA050104.md): Battery Pack · discharged · Feb 2, 2005 · N233TM · Boeing 737282 · Emergency Lighting > DURING A MAINTENANCE WALK AROUND CHECK, THE AFT RT SERVICE DOOR (R2) EMERGENCY EXIT ESCAPE SLIDE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REOMVED AND REPLACED THE BATTERY PACK FOR THE AFT RT SERVICE DOOR (R2 EMERGENCY EXIT SLIDE LIGHT IAW MM. EMERGENCY EXIT L - [SDR 2005F00029](https://openairdocs.org/sdr/2005F00029.md): Stringer · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer > IG CORROSION ON SRTINGER 27L AT STATION 950 LBL5)LEVEL2) - [SDR 2005F00028](https://openairdocs.org/sdr/2005F00028.md): Stringer · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer > STRINGER 23L AT STA 950 BL 10L HAS IG CORROSION(LEV. 2) - [SDR 2005F00027](https://openairdocs.org/sdr/2005F00027.md): Frame · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Frame > IG CORROSION ON FRAME AT BS 285 FROM STRINGER 24L TO STR 28L. - [SDR 2005F00026](https://openairdocs.org/sdr/2005F00026.md): Support Bracket · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings > SUPPORT BRACKET FOR NOSE STEERING BRACKET PULLEYS AT BS 289 STRINGER 26 L AND 27L --IG CIRROSION (LEVEL 2) - [SDR 2005F00025](https://openairdocs.org/sdr/2005F00025.md): Stringer Clip · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings > STRINGER TIES AT STA 947, STR.26L AND 27L -IG CORROSION (LEVEL 2). - [SDR 2005F00015](https://openairdocs.org/sdr/2005F00015.md): Bracket · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings > BRACKET AT STA 950 LBL 15 HAS IG CORROSION (LEVEL 2). - [SDR BJNA041106](https://openairdocs.org/sdr/BJNA041106.md): Bracket · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Miscellaneous Structure > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A BRACKET LOCATED AT STATION 950 LBL 15. REMOVED AND REPLACED CORRODED BRACKET LOCATED AT STATION 950 LBL 15. BRACKET WAS FABRICATED FROM 7075-T6.050. WORK DONE IAW BOEING SRM 51- - [SDR BJNA041105](https://openairdocs.org/sdr/BJNA041105.md): Stringer Clip · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER TIES AT STATION 967 STRINGER 26L AND STRINGER 27L. REMOVED AND REPLACED CORRODED STRINGER TIES OF STRINGER 26L AND STRINGER 27L AT STATION 967. STRINGER TIES WERE FABRICATE - [SDR BJNA041103](https://openairdocs.org/sdr/BJNA041103.md): Frame · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Frame > DURING A SCHEDULED C CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A FRAME RIB AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. CUTOUT CORRODED AREA OF FRAME AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. FABRICATED FILLER AND DOUBLER USING 707 - [SDR BJNA041107](https://openairdocs.org/sdr/BJNA041107.md): Stringer Clip · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON TWO STRINGER TIE OF STRINGER 26L LOCATED AT STATION 947. REMOVED AND REPLACED CORRODED STRINGER TIE OF STRINGERS 26L AT STATION 947. STRINGER TIES WERE FABRICATED FROM 7075-T6.063. - [SDR BJNA041104](https://openairdocs.org/sdr/BJNA041104.md): Stringer · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 27L AT STATION 950 LBL 5. REMOVED AND REPLACED CORRODED SECTION OF STRINGER 27L AT STATION 950 LBL 5 IAW BOEING SRM CHAPTER 53-10-3. (M) - [SDR BJNA041101](https://openairdocs.org/sdr/BJNA041101.md): Support Bracket · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Leading Edge Devices > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A LEADING EDGE SLAT ACTUATOR SUPPORT BRACKET ON THE LEFT WING SPAR AT WING STATION 421. REMOVED AND REPLACED THE SUPPORT BRACKET AT THE CENTER OF THE NUMBER TWO LEADING EDGE SLAT ACT - [SDR BJNA041102](https://openairdocs.org/sdr/BJNA041102.md): Stringer · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 26L STATION 950 BL 10L. REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER 26L AT STATION 950 BL 10L IAW BOEING SRM 53-10-3. (M) - [SDR BJNA041004](https://openairdocs.org/sdr/BJNA041004.md): Light · inoperative · Oct 12, 2004 · N233TM · Boeing 737282 · Emergency Lighting > AFT EMERGENCY TRACK LIGHT AND BOTTOM AFT EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP IAW CMM 33-50-01. OPERATIONAL CHECK OK. - [SDR BJNA041001](https://openairdocs.org/sdr/BJNA041001.md): Battery Pack · discharged · Oct 5, 2004 · N233TM · Boeing 737282 · Emergency Lighting > LT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD. - [SDR BJNA041002](https://openairdocs.org/sdr/BJNA041002.md): Battery Pack · discharged · Oct 5, 2004 · N233TM · Boeing 737282 · Emergency Lighting > RT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD. - [SDR BJNA040906](https://openairdocs.org/sdr/BJNA040906.md): Battery Pack · inoperative · Sep 19, 2004 · N233TM · Boeing 737282 · Emergency Lighting > FOUND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M) - [SDR BJNA040905](https://openairdocs.org/sdr/BJNA040905.md): Battery Pack · inoperative · Sep 19, 2004 · N233TM · Boeing 737282 · Emergency Lighting > FOUND LEFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M) - [SDR BJNA040704](https://openairdocs.org/sdr/BJNA040704.md): Battery · inoperative · Jul 16, 2004 · N233TM · Boeing 737282 · Emergency Lighting > DURNG A MAINTENANCE WALK AROUND CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER ASSEMBLY P/N 6104789 FOR THE LEFT OVERWING EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE L - [SDR BJNA040702](https://openairdocs.org/sdr/BJNA040702.md): Battery · inoperative · Jul 16, 2004 · N233TM · Boeing 737282 · Emergency Lighting > DURING A MAINTENANCE WALK AROUND CHECK, THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE IAW BOEING MM 33-51-31. THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT NOW OPERATED NORMALLY. (M) - [SDR BJNA040701](https://openairdocs.org/sdr/BJNA040701.md): Battery Pack · inoperative · Jul 16, 2004 · N233TM · Boeing 737282 · Emergency Lighting > DURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD CABIN DOOR R1 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE FWD R1 CABIN DOOR IAW BOEING MM 33-51-81. THE FWD R1 CABIN DOOR EMERGENCY EXIT LIGHT NOW OP - [SDR BJNA040703](https://openairdocs.org/sdr/BJNA040703.md): Battery · inoperative · Jul 16, 2004 · N233TM · Boeing 737282 · Emergency Lighting > DURING A MAINTENANCE WALK AROUND CHECK, THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE FOR THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE AFT CABIN OVERHEAD EM - [SDR BJNA040501](https://openairdocs.org/sdr/BJNA040501.md): Battery Pack · discharged · May 3, 2004 · N233TM · Boeing 737282 · Emergency Lighting > DURING A MAINTENANCE WALK AROUND CHECK, AN AISLE EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE PER BOEING MM 33-51-81, SYSTEM NOW CHECKS NORMAL. (M) - [SDR BJNA031201](https://openairdocs.org/sdr/BJNA031201.md): Engine · failed · Dec 17, 2003 · N233TM · Boeing 737282 · Engine (Turbine/Turboprop) > ON TAKEOFF AT 80 KNOTS, NR 1 ENGINE FAILED. THE TOWER REPORTED THE ENGINE WAS ON FIRE, NO FIRE WARNING INDICATION. DISCHARGED THE FIRE BOTTLE. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. FAILUR - [SDR BJNA030701](https://openairdocs.org/sdr/BJNA030701.md): Tire · separated · Jul 23, 2003 · N233TM · Boeing 737282 · Tire > ON TAKEOFF ROLL HEARD LOUD BANG JUST BEFORE ROTATION. INSPECTION FOUND NR 2 NOSE TIRE HAD THROWN TREAD. (M) - [SDR BJNA03042](https://openairdocs.org/sdr/BJNA03042.md): Light · inoperative · Apr 22, 2003 · N233TM · Boeing 737282 · Emergency Lighting > DURING A MAINTENANCE PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT OVER THE R-2 DOOR WOULD NOT ILLUMINATE WITH THE SWITCH IN THE ON POSITON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, SYSTEM CHECKS NORMALLY. (M) - [SDR BJNA03041](https://openairdocs.org/sdr/BJNA03041.md): Light · disconnected · Apr 7, 2003 · N233TM · Boeing 737282 · Emergency Lighting > EMERGENCY FLOOR PROXIMITY LIGHTING (FROM PASSENGER ROWS 14 THROUGH 17) NOT LIGHTING DURING OPERATIONAL CHECK. MAINTENANCE DISCOVERED THAT THE LIGHTING STRIP FOR THIS SECTION HAD BECOME DISCONNECTED FROM ITS POWER SOCKET. LIGHT STRIP WAS REATTACHED AND OPERAT - [SDR BJNA030302](https://openairdocs.org/sdr/BJNA030302.md): Light · broken · Mar 12, 2003 · N233TM · Boeing 737282 · Emergency Lighting > EMERGENCY FLOOR LIGHTING STRIP BROKEN AT SEAT 15D. INSTALLED LIGHT STRIP AS REQUIRED, OPS CHECK GOOD, IAW AMM 33-51-07. (M) - [SDR BJNA021201](https://openairdocs.org/sdr/BJNA021201.md): Battery Pack · discharged · Nov 29, 2002 · N233TM · Boeing 737282 · Emergency Equipment > AFT EMERGENCY FLASH LIGHT BATTERY CONDITION INDICATOR NOT BLINKING. REPLACED BATTERY PACK, NORMAL MAINTENANCE. (M) - [SDR BJNA021010](https://openairdocs.org/sdr/BJNA021010.md): Floorbeam · corroded · Oct 23, 2002 · N233TM · Boeing 737282 · Fuselage Main, Floor Beam > CORROSION ADJACENT TO WATER DRAIN LINE FORWARD UNDER SIDE OF R2 DOOR SCUFF PLATE AREA BS 958 RBL 53. REMOVED CORROSION FROM LOWER OUTBOARD FLOORBEAM SUPPORT, CORROSION WENT OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 SRM 51-40-3, 51-10-2, - [SDR BJNA021005](https://openairdocs.org/sdr/BJNA021005.md): Floorbeam · corroded · Oct 23, 2002 · N233TM · Boeing 737282 · Fuselage Main, Floor Beam > DURING A SCHEDULED C-CHECK INSPECTION DISCOVERED LEVEL 2 CORROSION ADJACENT TO WATER DRAIN LINE FORWARD UNDER SIDE OF R2 DOOR SCUFF PLATE AREA BS 958 RBL 53. REMOVED CORROSION FROM LOWER OUTBOARD FLOORBEAM SUPPORT, CORROSION WENT OUT OF LIMITS. FABRICATED RE - [SDR BJNA021017](https://openairdocs.org/sdr/BJNA021017.md): Floor Support · corroded · Oct 20, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous Structure > DURING SCHEDULED C-CHECK INSPECTION DISCOVERED, L1 DOOR AFT GIRTH BAR ATTACH FITTING AND OUTBOARD FLOORBOARD SUPPORT AT BS 346 LBL 60 CORRODED. FOUND GIRTH BAR FITTING AND FLOORBOARD SUPPORT CORRODED OUT OF LIMITS FORMED REPAIR FLOORBOARD SUPPORT AND GIRTH BA - [SDR BJNA021009](https://openairdocs.org/sdr/BJNA021009.md): Floor Support · corroded · Oct 19, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous Structure > DURING SCHEDULED C-CHECK INSPECTION DISCOVERED FLOOR SUPPORT BETWEEN FRAME 947-967 RIGHT APPROX BL40R HAS FLAKING CORROSION. FLOOR SUPPORT CORRODED OUT OF LIMITS. FABRICATED REPLACEMENT SUPPORT AND INSTALLED IAW B737 SRM 53-10-1, 51-10-2 AND 51-30-2. (M) - [SDR BJNA021004](https://openairdocs.org/sdr/BJNA021004.md): Stringer · corroded · Oct 19, 2002 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer > DURING A SCHEDULED C-CHECK INSPECTION OF THE AFT CARGO COMPARTMENT BILGE AREA, DISCOVERED LEVEL 2 CORROSION. ON THE FORWARD END OF STRINGERS 25L AT STATION 967. CUT OUT DAMAGED SECTION, IAW BOEING SRM 53-10-3 FIGURE 1. FABRICATED AND INSTALLED STRINGER REPA - [SDR BJNA021002](https://openairdocs.org/sdr/BJNA021002.md): Floor Support · corroded · Oct 19, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous Structure > DURING A SCHEDULED C-CHECK INSPECTION, DISCOVERED AFT FUSELAGE FLOOR SUPPORT FRAME AT STATION 951 FROM LBL 20 TO LBL 36 HAS LEVEL 2 CORROSION. REMOVED FLOOR SUPPORT FRAME, FABRICATED AND INSTALLED FRAME REPAIR IAW BOEING SRM 53-10-2 AND 51-30-2. (M) - [SDR BJNA021003](https://openairdocs.org/sdr/BJNA021003.md): Stringer · corroded · Oct 19, 2002 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer > DURING A SCHEDULED C-CHECK INSPECTION OF THE FORWARD CARGO COMPARTMENT, DISCOVERED A TWO INCH SPOT OF LEVEL 2 CORROSION ON STRINGER 27L AT STATION 389. FABRICATED AND INSTALLED STRINGER REPAIR IAW BOEING 737 SRM 51-10-2, 51-10-6, 51-30-2, 53-10-01 FIGURE 1 AN - [SDR BJNA021007](https://openairdocs.org/sdr/BJNA021007.md): Floorbeam · corroded · Oct 18, 2002 · N233TM · Boeing 737282 · Fuselage Main, Floor Beam > DURING SCHEDULED C-CHECK INSPECTION DISCOVERED FORWARD LAVATORY FLOOR STATION 294.5 WL 208 LBL 12 FLOORBEAM HAS 12 INCHES OF CORROSION. FLOORBEAM CORRODED MORE THAN 50 PERCENT, OUT OF LIMITS. REMOVED CORRODED FLOORBEAM UPPER T-CAP AND SPLICE. FABRICATED REP - [SDR BJNA021008](https://openairdocs.org/sdr/BJNA021008.md): Angle · cracked · Oct 15, 2002 · N233TM · Boeing 737282 · Horizontal Stabilizer Miscellaneous Structure > LEFT CENTER HORIZONTAL STABILIZER REAR STABILIZER FITTING HAS CRACKED ANGLE STATION 1170, BELOW LEFT HORIZONTAL STABILIZER PIN/AFT. REMOVED CRACKED ANGLE IAW B737 SRM 51-30-2. TRIMMED TO FIT NEW SUPPORT ANGLE IAW B737 SRM 51-30-5, 51-10-1, 51-20-1 FIG 1/2. - [SDR BJNA021101](https://openairdocs.org/sdr/BJNA021101.md): Skin · delaminated · Oct 10, 2002 · N233TM · Boeing 737282 · Trailing Edge Flaps > DURING SCHEDULED C-CHECK INSPECTION DISCOVERED RIGHT WING INBOARD AFT FLAP LOWER SKIN DELAMINATED AT T/E SECTION. CUT OUT DELAMINATED AREA.5 INCH BY 1 INCH. FABRICATED AND INSTALLED SKIN SECTION AND DOUBLER. BONDED AND APPLIED FIBERGLASS REPAIR IAW B737 SR - [SDR BJNA021014](https://openairdocs.org/sdr/BJNA021014.md): Skin · gouged · Oct 10, 2002 · N233TM · Boeing 737282 · Trailing Edge Flaps > RIGHT WING OUTBOARD FLAP, LOWER FORE FLAP LEADING EDGE SKIN GOUGED, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 57-50-4 FIG 2, 51-10-2 AND 51-30-8. (M) - [SDR BJNA021013](https://openairdocs.org/sdr/BJNA021013.md): Stringer Clip · corroded · Oct 10, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous Structure > AFT FUSELAGE FLOORBEAM STATION 967 LEFT SIDE WHERE MEETS CIRCUMFERENTIAL FRAME HAS CORRODED STRINGER TIE. REMOVED STRINGER TIE CLIP, FABRICATED AND INSTALLED REPAIR CLIP IAW B737 SRM 51-10-2, 51-30-2 AND 51-20-1. (M) - [SDR BJNA021011](https://openairdocs.org/sdr/BJNA021011.md): Intercostal · corroded · Oct 10, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous Structure > NOSE WHEEL WELL LEFT SIDE AT AFT ACCESS PANEL SUPPORT BEAMS, THREE EACH HAS EXFOLIATED CORROSION FS 280. REMOVED AND REPLACED TWO EXFOLIATED INTERCOSTALS IAW B737 SRM 51-30-2, 51-20-1, B737 MM 51-21-0. REMOVED CORROSION FROM THIRD VERICAL BEAM FOUND TO BE WI - [SDR BJNA021015](https://openairdocs.org/sdr/BJNA021015.md): Skin · cracked · Oct 9, 2002 · N233TM · Boeing 737282 · Leading Edge Devices > LEFT WING NR 2 SLAT TRAILING EDGE CHAFED AND CRACKED AT OUTBOARD AUX SLAT TRACK. REPAIRED CRACKED AND CHAFED LEFT WING NR 2 SLAT TRAILING EDGE AT OUTBOARD AUX SLAT TRACK BY CUTTING OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B7 - [SDR BJNA021012](https://openairdocs.org/sdr/BJNA021012.md): Floorbeam · corroded · Oct 9, 2002 · N233TM · Boeing 737282 · Fuselage Main, Floor Beam > FLOORBEAM BS 976, LBL 53 HAS EXFOLIATED CORROSION. REMOVED FLOORBEAM, FABRICATED AND INSTALLED FLOORBEAM REPAIR 55 INCHES BY 1.5 INCHES BAC1505-100617, IAW TIMCO REO-L00597 REV A. (M) - [SDR BJNA021006](https://openairdocs.org/sdr/BJNA021006.md): Stringer · corroded · Oct 9, 2002 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer > DURING SCHEDULED C-CHECK INSPECTION DISCOVERED AFT LOWER BILGE STATION 1006, STRINGER 23L, CLIP CORRODED. REMOVED CLIP AND S23L IN THE AFT LOWER BILGE BS 1006. FORMED REPAIR STRINGER AND CLIP AND INSTALLED IAW B737 SRM 53-10-3 AND 51-10-2. (M) - [SDR BJN2002F00003](https://openairdocs.org/sdr/BJN2002F00003.md): Light · inoperative · Jun 3, 2002 · N233TM · Boeing 737282 · Emergency Lighting > FLOOR EMERGENCY LIGHTS MID-SECTION INOPERATIVE. RECONNECTED LAMP TESTED. Next page: https://openairdocs.org/deregistered/N233TM-2005-11-21/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 = 'N233TM' AND deregistration_id = 'N233TM-2005-11-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N233TM-2005-11-21/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.