# Service difficulty reports: N673MC, cancelled Mar 18, 2013 A list on [N673MC, cancelled Mar 18, 2013](https://openairdocs.org/deregistered/N673MC-2013-03-18.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 · 55 reports - [SDR HALA0100006](https://openairdocs.org/sdr/HALA0100006.md): Battery Pack · discharged · Jan 5, 2000 · N673MC · Doug DC951 · Emergency Lighting > FLT 123 - HNL - EMERGENCY LIGHTS CEILING INOPERATIVE. SCATTERED THROUGH CABIN. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS. OPS CHECK OK. (M) - [SDR HALA9900099](https://openairdocs.org/sdr/HALA9900099.md): Intercostal · cracked · Apr 14, 1999 · N673MC · Doug DC951 · Fuselage Miscellaneous Structure > AFT ACCESSORY COMPARTMENT FUSELAGE STATION 1293, STRINGER 12R INTERCOSTAL HAS ABOUT.5625 INCH LONG CRACK AND LIGHT SURFACE CORROSION LEVEL 1. REMOVED AND REPLACED FABRICATED INTERCOSTAL IAW SRM 51-10-3, SRM 51-10-2, SRM 51-30-5. (M) - [SDR HALA9900102](https://openairdocs.org/sdr/HALA9900102.md): Doubler · gouged · Apr 13, 1999 · N673MC · Doug DC951 · Leading Edge Devices > RIGHT WING LEADING EDGE AT MOST INBOARD EXISTING REPAIR DOUBLER, HAS DEEP. GOUGES INBOARD OR NR 1 SLAT TELESCOPIC DUCT. REMOVED DOUBLER, FABRICATED NEW DOUBLER PER SRM 57-06A FIG 3, TREAT, PRIMED PER SRM. (M) - [SDR HALA9900101](https://openairdocs.org/sdr/HALA9900101.md): Stringer · corroded · Apr 6, 1999 · N673MC · Doug DC951 · Wing, Longeron/Stringer > FOUND CORROSION ON STRINGER UNDER SPOILER XRS 280-300. FABRICATED ANGLE, LOWER INTERCOSTAL SUPPORT ANGLE, SPLICE ANGLE 2 EACH SHIMS, PER SRM 57-01 FIG 3. TREATED AND PRIMED PER SRM 51-10-3 AND INSTALLED PER 51-30-2. (M) - [SDR HALA9900100](https://openairdocs.org/sdr/HALA9900100.md): Splice · corroded · Apr 3, 1999 · N673MC · Doug DC951 · Fuselage Miscellaneous Structure > AFT CARGO DOOR JAMB PAN SPLICE ANGLE AT STATION 1079 HAS LEVEL 2 CORROSION. FABRICATED AND LOCATED 2 DOUBLERS AND INSTALLED IAW SRM 51-30-1, 51-10-3, 53-05. (M) - [SDR HALA9900058](https://openairdocs.org/sdr/HALA9900058.md): Switch · failed · Feb 21, 1999 · N673MC · Doug DC951 · Leading Edge Slat Position Indicating System > FLT 201 - HNL - WITH SLAT EXTEND AND FLAP 50 DEGREES SET, ON FINAL 8L HNL SLAT EXTEND LIGHT WENT OUT, STALL INDICATION LIGHT ILLUMINATED AND JUST PRIOR TO TOUCHDOWN, STICK SHAKER. REMOVED AND REPLACED RIGHT SLAT EXTEND SWITCH, OPS CHECK OK. (M) - [SDR HALA9800326](https://openairdocs.org/sdr/HALA9800326.md): Clamp · loose · Sep 17, 1998 · N673MC · Doug DC951 · Extinguishing System > KOA - FLT 317 - FIRE PROTECTION AGENT LOW LIGHT ON. FOUND LOWER FIRE BOTTLE THERMO DISCHARGED ONLY. REPLACED ACM PNEU DUCT, CLAMP LOOSE, RETORQUED AND SAFETIED. LEAK CHECK OK, LOW LIGHT CHECK OK. (M) - [SDR HALA9800183](https://openairdocs.org/sdr/HALA9800183.md): Control Panel · malfunctioned · Jun 30, 1998 · N673MC · Doug DC951 · Landing Gear Position and Warning > ITO - FLT 101 - (LOG PAGE NR A144385) - NOSE GEAR UNSAFE LIGHT COMES ON IN-FLIGHT. REPLACED L/G POSITION WARNING CONTROL PANEL AND NOSE GEAR ELECTRICAL HARNESS. (X) - [SDR HALA9800139](https://openairdocs.org/sdr/HALA9800139.md): Actuator · broken · May 31, 1998 · N673MC · Doug DC951 · Landing Gear Retraction/Extension System > FLT 552 - HNL - WHEN LANDING GEAR WAS LOWERED THE A/C SHUTTERED AND THE LEFT LANDING GEAR INSTANTLY INDICATED DOWN, WITH A GREEN LIGHT. CHECKED CONDITION AND SECURITY OF LANDING GEAR. FOUND LEFT MAIN GEAR RET CYL BROKEN AND LEFT MAIN BUNGEE CYL BROKEN, REPLA - [SDR 98ZZZM472](https://openairdocs.org/sdr/98ZZZM472.md): Actuator · broken · May 31, 1998 · N673MC · Doug DC951 · Landing Gear Actuator > FLT 552 - HNL - WHEN LANDING GEAR WAS LOWERED THE A/C SHUTTERED AND THE LEFT LANDING GEAR INSTANTLY INDICATED DOWN, WITH A GREEN LIGHT. CHECKED CONDITION AND SECURITY OF LANDING GEAR. FOUND LEFT MAIN GEAR RET CYL BROKEN AND LEFT MAIN BUNGEE CYL BROKEN, REPLA - [SDR HALA9800072](https://openairdocs.org/sdr/HALA9800072.md): Grd Shift Contl · out of adjust · Mar 25, 1998 · N673MC · Doug DC951 · Landing Gear Retraction/Extension System > FLT 530 - HNL - A/C WAS UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. SUSPECT GROUND SHIFT FAILURE. A/C MADE AN UNEVENTFUL LANDING IN HNL. ADJUSTED GROUND SHIFT CONTROL MECHANISM, PER M/M 32-231. (M) - [SDR HALA9800028](https://openairdocs.org/sdr/HALA9800028.md): Battery · discharged · Jan 30, 1998 · N673MC · Doug DC951 · Emergency Lighting > HNL - FLT 128 - EMERGENCY LIGHTS MID CABIN ON CEILING, DO NOT COME ON. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. (M) - [SDR HALA9700223](https://openairdocs.org/sdr/HALA9700223.md): Intercostal · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Miscellaneous Structure > INTERCOSTAL FS 1223 RIGHT SIDE OF TAIL SKID FITTING CORRODED OUT OF LIMITS. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPAIR INTERCOSTAL FROM 7075-0.040 INCH AND HEAT TREATED TO T6. REPAIR IS PER SRM 53-13-4 FIG 1. (M) - [SDR HALA9700222](https://openairdocs.org/sdr/HALA9700222.md): Jamb · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Miscellaneous Structure > AFT CARGO DOORWAY, LOWER SECTION OF DOOR JAMB CORRODED FROM FORWARD TO AFT END. REMOVED LOWER SECTION OF PAN AND SPLICE DOUBLERS, FABRICATED AND INSTALLED REPAIR LOWER PAN SECTION PER SRM 53-05 FIG 44 AND DOUBLERS PER 53-01 FIG 2. (M) - [SDR HALA9700221](https://openairdocs.org/sdr/HALA9700221.md): Frame · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Frame > LOWER FRAME ASSEMBLY AT FS 1038 HAS LEVEL 2 CORROSION. REMOVED DAMAGED AREA, FABRICATED TEE EXTRUSION AND INSTALLED PER SRM 53-01. (M) - [SDR HALA9700220](https://openairdocs.org/sdr/HALA9700220.md): Skin · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Plate/Skin > CORRODED SKIN FS 754 L30, 2 FOOT FORWARD OF GEAR DOORS. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR SKIN. (M) - [SDR HALA9700219](https://openairdocs.org/sdr/HALA9700219.md): Frame · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Ailerons > RIGHT AILERON UPPER INBOARD SIDE 5 HOLES HAVE CRACKS EXTENDING FROM THEM. REMOVED DAMAGED MATERIAL, FABRICATED REPLACEMENT SKIN AND FINGER DOUBLERS PER SRM 57-03 FIG 13, INSTALLED REPAIR. (M) - [SDR HALA9700210](https://openairdocs.org/sdr/HALA9700210.md): Skin · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Nacelle/Pylon, Plate/Skin > LEFT AFT FUSELAGE UNDER AND BETWEEN LEFT PYLON TRAILING EDGE SUPPORT RAILS CORROSION APPROX LAST 12 INCHES. REMOVED DAMAGED MATERIAL, FABRICATED DOUBLER AND SKIN OUT OF 2024-T3.040 INCH AND.050 INCH PER SRM 53-01 FIGURE 2 SHEET 4 WITH MODIFICATION PER EA DC - [SDR HALA9700209](https://openairdocs.org/sdr/HALA9700209.md): Longeron · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FORWARD CARGO COMPARTMENT, LONGERON 30 HAS CORROSION IN HAT CHANNEL FROM FS 674 TO 695 (DEEP POCKETS). REMOVED DAMAGED MATERIAL, FS 655 TO 693, INSTALLED REPAIR SECTION PER SRM 51-30. (M) - [SDR HALA9700208](https://openairdocs.org/sdr/HALA9700208.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > LEFT LONGERON 17 CRACKED AND PREVIOUS REPAIR CRACKED AT FS 1136.091. REMOVED CRACKED LONGERON, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700207](https://openairdocs.org/sdr/HALA9700207.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > RIGHT LONGERON 16 CRACKED AT FS 1136.091. REMOVED CRACKED LONGERON SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICED PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700206](https://openairdocs.org/sdr/HALA9700206.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > RIGHT LONGERON 16 CRACKED AT FS 1116. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT AND SPLICE. (M) - [SDR HALA9700204](https://openairdocs.org/sdr/HALA9700204.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 200 LONGERON 30 CRACKED AT FRAME TIE IN. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700203](https://openairdocs.org/sdr/HALA9700203.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > LONGERON 17R CRACKED AT FS 1151. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION PER SRM 53-13-3. (M) - [SDR HALA9700202](https://openairdocs.org/sdr/HALA9700202.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > RIGHT LONGERON 17 CRACKED AT FS 1116. REMOVED LONGERON 17 AND LONGERON 17 PRODUCTION SPLICE, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-13-3. (M) - [SDR HALA9700201](https://openairdocs.org/sdr/HALA9700201.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 200 LONGERON 22R CRACKED AT FRAME TIE-IN. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR SECTION PER SRM. (M) - [SDR HALA9700200](https://openairdocs.org/sdr/HALA9700200.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 200 LONGERON 23R CRACKED AT FRAME TIE-IN. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700199](https://openairdocs.org/sdr/HALA9700199.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 200 LONGERON 24R CRACKED AT FRAME TIE-IN. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700198](https://openairdocs.org/sdr/HALA9700198.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 200 LONGERON 25R CRACKED AT FRAME TIE IN. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700197](https://openairdocs.org/sdr/HALA9700197.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 200 LONGERON 27R CRACKED AT FRAME TIE-IN. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700196](https://openairdocs.org/sdr/HALA9700196.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 200 LONGERON 28R CRACKED AT FRAME TIE-IN. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700195](https://openairdocs.org/sdr/HALA9700195.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 20 LONGERON 29R CRACKED AT FRAME TIE IN. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPAIR LONGERON SECTION AND SPLICE PER SRM 53-02 FIGURE 18. (M) - [SDR HALA9700194](https://openairdocs.org/sdr/HALA9700194.md): Longeron · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > FS 200 LONGERON 29L CRACKED AT FRAME TIE IN. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-02 FIGURE 38. (M) - [SDR HALA9700193](https://openairdocs.org/sdr/HALA9700193.md): Skin · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Plate/Skin > TITANIUM SKIN CRACKED BELOW LONGERON 14L AT FS 1163. REMOVED DAMAGED SECTION, CONFIRMED DAMAGED REMOVAL BY HFEC, FABRICATED AND INSTALLED.04 INCH 6AL-4V DOUBLER PER SRM 53-04 FIGURE 46. (M) - [SDR HALA9700192](https://openairdocs.org/sdr/HALA9700192.md): Longeron · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > LONGERON 30 HAS EXFOLIATION CORROSION AT FS 1126 TO 1135, INSIDE CHANNEL. REMOVED CORRODED LONGERON SECTION, FABRICATED AND INSTALLED SPLICE AND FILLER PER SRM 53-02 FIGURE 18, TREATED AND PRIMED. (M) - [SDR HALA9700191](https://openairdocs.org/sdr/HALA9700191.md): Skin · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Plate/Skin > FIVE RIVET HEADS POPPED AT LEFT FS 1339.407 AFT OF NR 1 ENG PYLON. ACCOMP SPLICE REPAIR OF CORRODED SKIN PANELS 5210228-209 AND -213 ALONG CANTED FRAME BETWEEN L16L AND L20L AT FS 1303 AND AT THE LAP JOINT OVER CANTED FRAME FS 1339 BY REMOVAL OF DAMAGED SKIN, - [SDR HALA9700190](https://openairdocs.org/sdr/HALA9700190.md): Longeron · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Main, Longeron/Stringer > LEFT CUSP BEAM (LONGERON 18L) BETWEEN FS 1151 AND 1167 CORRODED OUT OF LIMITS. CUT OUT DAMAGED MATERIAL, FABRICATED AND INSTALLED NEW BEAM, FILLER AND STRAPS PER SRM 53-05 FIGURE 25. (M) - [SDR HALA9700189](https://openairdocs.org/sdr/HALA9700189.md): Jamb · corroded · Oct 30, 1997 · N673MC · Doug DC951 · Fuselage Miscellaneous Structure > FORWARD CARGO DOORWAY, LOWER SECTION OF DOOR JAMB CORRODED HEAVILY FROM FORE TO AFT. REMOVED LOWER SECTION OF FORWARD CARGO DOORWAY JAMB PAN, FABRICATED, AND INSTALLED REPAIR SECTION AND SPLICES PER SRM 53-05 FIGURE 44. (M) - [SDR HALA9700185](https://openairdocs.org/sdr/HALA9700185.md): Spar · cracked · Oct 30, 1997 · N673MC · Doug DC951 · Wing Spar > RIGHT WING AFT SPAR CAP CRACKED AT NR 2 FLAP HINGE LOWER INBOARD ATTACH OUTBOARD AREA. INSTALLED TEMPORARY REPAIR TO AFT RIGHT LOWER SPAR AT STATION XRS164 PER ASB 57-146 AND DWG JO60271 REV M. (M) - [SDR HALA9700135](https://openairdocs.org/sdr/HALA9700135.md): Wire · shorted · Jul 3, 1997 · N673MC · Doug DC951 · Light System Wiring > FLT 112 - HNL - STRONG BURNING SMELL COMING INTO COCKPIT. RIGHT OVER THE OVERHEAD PANEL. ODOR SEEMS STRINGER WITH LT A/C PAC ON OR SOMETHING ELECTRICAL IS SHORTING IN OVERHEAD PANEL. SECURED BROKEN WIRE, (OVERHEAD PANEL LIGHT SWITCH. OPS CHECK GOOD. (M) - [SDR HALA97196](https://openairdocs.org/sdr/HALA97196.md): Servo Valve · failed · Jan 14, 1997 · N673MC · Doug DC951 · Brake Anti-Skid Section > HNL - FLT 208 - UPON LANDING AT MKK, THE TOWER REPORTED THE LANDING GEAR WAS ON FIRE. AFTER STOPPING THE A/C PERFORMED EMERGENCY EVACUATION CHECKLIST. BOTH FORWARD SLIDES WERE DEPLOYED AS A PRECAUTION. THERE WAS NO FIRE, SPARKS WERE GENERATED DUE TO FLAT TI - [SDR HALA96155](https://openairdocs.org/sdr/HALA96155.md): Battery Pack · discharged · Nov 3, 1996 · N673MC · Doug DC951 · Emergency Lighting > HNL - FLT 767 - THE AFT CABIN EMERGENCY FLOOR LIGHTS ARE DIM. REPLACED THE BATTERY PACK AND THE OPERATIONAL CHECK WAS GOOD. (M) - [SDR HALA96119](https://openairdocs.org/sdr/HALA96119.md): Battery · discharged · Aug 20, 1996 · N673MC · Doug DC951 · Emergency Lighting > HNL - FOUND AFT CABIN EMERGENCY LIGHTING INOP. REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD. (M) - [SDR HAL96104](https://openairdocs.org/sdr/HAL96104.md): Drive Mechanism · worn · Jul 31, 1996 · N673MC · Doug DC951 · Leading Edge Slat Control System > HNL - FLT 121 - LT SLAT DISAGREEMENT LIGHT ILLUMINATED DURING SLAT EXTENSION ACCOMPANIED BY AN ADVERSE ROLL TO THE RIGHT. FOUND LT WING SLAT BELLCRANK LOWER ACTUATOR EYE BOLT MOUNT HOLE DAMAGED AND LT WING SLAT BELLCRANK HUCK BOLT SHEARED. (X) - [SDR HALA96102](https://openairdocs.org/sdr/HALA96102.md): Retract Spring · broken · Jul 28, 1996 · N673MC · Doug DC951 · Landing Gear Retraction/Extension System > FLT 522 - HNL - AIR RETURN, UPON FLAP RETRACTION CLIMBING OUT OF APPROX 2000 FEET, A LOUD METALIC SOUND ORIGINATING FROM BELOW COCKPIT CREW AREA WAS HEARD AND FELT. FLIGHT ATTENDANT ALSO HEARD AND CONFIRMED. AFTER CREW DEBRIEFING MLG WAS RETRACTED AND FLAPS - [SDR HAL9691](https://openairdocs.org/sdr/HAL9691.md): Fire Loop · dirty connector · Jul 6, 1996 · N673MC · Doug DC951 · Fire Detection > HNL - NR 2 ENGINE B-LOOP INOPERATIVE. TEST OK. CLEANED NR 2 ENGINE B-LOOP ELEMENT CONNECTORS. RUN-UP ENGINE, OPERATION CHECK OK. (X) - [SDR HAL9690](https://openairdocs.org/sdr/HAL9690.md): Fire Loop · failed connector · Jul 6, 1996 · N673MC · Doug DC951 · Fire Detection > HNL - NR 1 ENGINE B-LOOP INOPERATIVE. *SUPPLEMENTAL* - REPLACED CONNECTOR FOR NR 1 ENGINE APRON B-LOOP. RUN-UP ENGINE CHECK OK. (X) - [SDR HAL9689](https://openairdocs.org/sdr/HAL9689.md): Fire Loop · inoperative · Jul 2, 1996 · N673MC · Doug DC951 · Fire Detection > HNL - NR 1 ENGINE B-LOOP INOPERATIVE. OK TO CONTINUE PER MEL 26-1. (X) - [SDR HAL9685](https://openairdocs.org/sdr/HAL9685.md): Fire Loop · loose connector · Jul 2, 1996 · N673MC · Doug DC951 · Fire Detection > HNL - LEFT ENGINE B-LOOP INOPERATIVE. *SUPPLEMENTAL* - CLEANED AND SECURED CONNECTOR. OPS CHECK OK. (X) - [SDR HALA9635](https://openairdocs.org/sdr/HALA9635.md): Prox Contl Box · inop · Apr 4, 1996 · N673MC · Doug DC951 · Landing Gear Position and Warning > HNL - FLT NR 504 - ON 'UPLATCH CHECK' LT MLG INDICATED 'UNSAFE'. LIGHT REMAINED ILLUMINATED WHEN 'UP' SELECTED. CYCLED GEAR IAW PROCEDURES. ALL DOWN SAFE. CYCLED 'UP' LT MLG STILL UNSAFE IN UP POSITION. REPLACED LANDING GEAR PROXIMITY BOX CONTROL, CLEANED Next page: https://openairdocs.org/deregistered/N673MC-2013-03-18/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 = 'N673MC' AND deregistration_id = 'N673MC-2013-03-18' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N673MC-2013-03-18/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.