# Service difficulty reports: N87555, cancelled Jun 19, 2013 A list on [N87555, cancelled Jun 19, 2013](https://openairdocs.org/deregistered/N87555-2013-06-19.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 · 67 reports - [SDR 29GA95555110712](https://openairdocs.org/sdr/29GA95555110712.md): Angle · corroded · Nov 7, 2012 · N87555 · Beech 1900D · Vertical Stabilizer, Spar/Rib > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL SPAR LEFT AND RIGHT ANGLES BELOW RUDDER ATTACH BRACKET HAS CORROSION. BLENDED CORROSION FROM LEFT AND RIGHT VERTICAL SPAR ANGLES AND PERFORMED NDT INSPECTION NO EVIDENCE OF CORROSION NOTED. - [SDR 29GA2013021395557](https://openairdocs.org/sdr/29GA2013021395557.md): Spar Cap · corroded · Nov 7, 2012 · N87555 · Beech 1900D · Wing Spar > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING MAIN SPAR UPPER CAP AT WS 124 CORRODED. BLENDED CORROSION AND PERFORMED NDT INSPECTION, NO CORROSION OR CRACKS NOTED. - [SDR 29GA2012110795557](https://openairdocs.org/sdr/29GA2012110795557.md): Spar · corroded · Nov 7, 2012 · N87555 · Beech 1900D · Wing Spar > REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING MAIN SPAR UPPER CAP HAS CORROSION. - [SDR 29GA2012110795555](https://openairdocs.org/sdr/29GA2012110795555.md): Angle · corroded · Nov 7, 2012 · N87555 · Beech 1900D · Rudder Miscellaneous Structure > REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL SPAR RIGHT ANGLE BELOW UPPER RUDDER ATTACH BRACKET HAS CORROSION. - [SDR 29GA95553082912](https://openairdocs.org/sdr/29GA95553082912.md): Skin · corroded · Aug 29, 2012 · N87555 · Beech 1900D · Fuselage Main, Plate/Skin > DURING SCHEDULE ROUTINE MAINTENANCE DISCOVERED EXFOLIATION ON OUTER BELLY SKIN BETWEEN STRINGER 14L AND 15L AT FS 318.25. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL REPAIR DOUBLER. - [SDR 29GA95571052712A](https://openairdocs.org/sdr/29GA95571052712A.md): Engine · malfunctioned · May 27, 2012 · N87555 · Beech 1900D · Engine (Turbine/Turboprop) > FLIGHT: RIGHT ENGINE OIL PRESSURE ILLUMINATED IN FLIGHT ON APPROACH ASSOCIATED SMELL OF SMOKE IN CABIN AND COCKPIT. ENGINE SECURED AND EMERGENCY DECLARED. REPLACED RIGHT ENGINE ASSEMBLY. - [SDR 29GA95532040312A](https://openairdocs.org/sdr/29GA95532040312A.md): Circuit Board · loose · Apr 3, 2012 · N87555 · Beech 1900D · Landing Gear System Wiring > FLIGHT 3994, GEAR HANDLE LIGHTS DO NOT ILLUMINATE IN FLIGHT WHEN POWER LEVERS REDUCED BELOW 85% GEAR WARNING HORN WORKS NORMAL. SECURED LANDING GEAR CONTROL RELAY BOARD. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK GOOD. - [SDR 29GA95532032312A](https://openairdocs.org/sdr/29GA95532032312A.md): Warning System · malfunctioned · Mar 23, 2012 · N87555 · Beech 1900D · Landing Gear Position and Warning > FLIGHT: 4022 TCB/FLL GEAR WARNING HORN DOES NOT GO OFF WHEN POWER LEVERS ARE BROUGHT TO IDLE AND NO GEAR LIGHTS. PERFORMED LANDING GEAR OPERATIONAL CHECKS. OPERATIONAL CHECKS NORMAL. - [SDR 29GA95553121811A](https://openairdocs.org/sdr/29GA95553121811A.md): Stringer · debonded · Dec 18, 2011 · N87555 · Beech 1900D · Fuselage Main, Longeron/Stringer > DURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED SKIN DEBONDED FROM STRINGER AT AFT EVAPORATOR BLOWER APPROXIATELY AT FS 363.25-393.25. REBONDED AND INSTALLED DOUBLER AND FILLER REPAIR TO 10.0 INCH SECTION OF STRINGER TO SKIN. - [SDR 29GA2012013000011](https://openairdocs.org/sdr/29GA2012013000011.md): Cable · failed · Dec 13, 2011 · N87555 · Beech 1900D · Passenger/Crew Doors > FLIGHT4028, PILOT REPORTED MAIN CABIN DOOR WILL NOT OPEN. REPLACED AIRSTAIR DOOR FORWARD LOWER LATCH CABLE ASSEMBLY. OPS CHECKED GOOD. - [SDR 29GA95527120611A](https://openairdocs.org/sdr/29GA95527120611A.md): Trim System · out of rig · Dec 6, 2011 · N87555 · Beech 1900D · Aileron Tab Control System > FLIGHT: 3998 FLL/FLL DURING FLIGHT THE ADDITION OF RIGHT AILERON TRIM DOES NOT ALTER THE CONTROL WHEEL FORCES NECESSARY TO MAINTAIN ATTITUDE. DECLARED AN EMERGECNY RETURNED TO FLL LANDED WITHOUT INCIDENT. PERFORMED AIRCRAFT AILERON AND RUDDER INTERCONNECT SY - [SDR 29GA95557111411A](https://openairdocs.org/sdr/29GA95557111411A.md): Skin · corroded · Nov 14, 2011 · N87555 · Beech 1900D · Wing, Plate/Skin > REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING OUTBOARD TRAILING EDGE UPPER SKIN HAS CORROSION DAMAGE. REMOVED DAMAGED AREA OF SKIN AND INSTALLED REPAIR FILLER AND AN EXTERNAL DOUBLER. - [SDR 29GA95527111411A](https://openairdocs.org/sdr/29GA95527111411A.md): Skin · damaged · Nov 14, 2011 · N87555 · Beech 1900D · Wing, Plate/Skin > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING OUTBOARD TRAILING EDGE UPPER SKIN HAS CORROSION DAMAGE. REMOVED DAMAGED AREA OF SKIN AND INSTALLED REPAIR FILLER AND AN EXTERNAL DOUBLER. - [SDR 29GA93552110911A](https://openairdocs.org/sdr/29GA93552110911A.md): Door · dirty · Nov 9, 2011 · N87555 · Beech 1900D · Emergency Exits > REPORT: DURING SCHEDULE ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT HARD TO OPEN. CLEANED AND LUBED LEFT EMERGENCY EXIT OPERATIONAL CHECK GOOD. - [SDR 29GA95552100211A](https://openairdocs.org/sdr/29GA95552100211A.md): Door · defective · Oct 2, 2011 · N87555 · Beech 1900D · Emergency Exits > DURING SCHEDULED ROUTINE C-1 INSPECTION DISCOVERED LEFT EMERGENCY EXIT HARD TO OPEN. REPLACED LEFT EMERGENCY EXIT. - [SDR 29GA95561072111A](https://openairdocs.org/sdr/29GA95561072111A.md): Power Lever · out of rig · Jul 21, 2011 · N87555 · Beech 1900D · Power Lever > FLIGHT 9185 FPO/FLL DURING APPROACH AUTOFEATHER ACTIVATED ON RIGHT ENGINE WITH TORQUE APPROXIMATELY 1000 LBS LEFT AND RIGHT ENGINES. RIGGED RIGHT ENGINE POWER LEVER TO MATCH LEFT POWER LEVER AUTOFEATHER SYSTEM TEST SATISFACTORY. - [SDR GUUA95532052111A](https://openairdocs.org/sdr/GUUA95532052111A.md): Indicator · intermittent · May 21, 2011 · N87555 · Beech 1900D · Landing Gear Position and Warning > FLIGHT: 9147 TPA/FLL PILOT REPORTED NOSE GEAR DOWN AND LOCKED LIGHT INTERMITTENT. REPLACED LANDING GEAR ANNUNCIATOR ASSY OPS CHECK GOOD. - [SDR GUUA95553050311B](https://openairdocs.org/sdr/GUUA95553050311B.md): Angle · cracked · May 3, 2011 · N87555 · Beech 1900D · Fuselage Miscellaneous Structure > DURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED RT CLOSING ANGLE CRACKED 2.1 INCHES AT FS 288.0. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE. - [SDR GUUA95553050311A](https://openairdocs.org/sdr/GUUA95553050311A.md): Angle · cracked · May 3, 2011 · N87555 · Beech 1900D · Fuselage Miscellaneous Structure > DURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED LT CLOSING ANGLE CRACKED 2.0 INCHES AT FS 288.0. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE. - [SDR GUUA95557031211B](https://openairdocs.org/sdr/GUUA95557031211B.md): Stringer · corroded · Mar 12, 2011 · N87555 · Beech 1900D · Wing, Longeron/Stringer > DURING SCHEDULED X-RAY INSP, DISCOVERED LT WING CORROSION ON STRINGER FWD OF SPAR 1.270 X 0.30 INCHES AT WS 124.25. REMOVED CORROSION FROM LEFT WING LOWER FORWARD SPAR FORWARD FLANGE COMPLIED WITH FLOURESCENT PENETRANT INSPECTION NO SIGNS OF CORROSION FOUND. - [SDR GUUA95557031211A](https://openairdocs.org/sdr/GUUA95557031211A.md): Spar · corroded · Mar 12, 2011 · N87555 · Beech 1900D · Wing Spar > DURING SCHEDULED X-RAY INSP, DISCOVERED RT WING CORROSION ON MAIN SPAR 1.3 X 0.06 INCHES AT WS 124.25. REMOVED CORROSION FROM RIGHT WING LOWER FORWARD SPAR CAP COMPLIED WITH FLOURESCENT PENETRANT INSPECTION ON BLEND OUT AREA NO SIGNS OF CORROSION FOUND ALL ARE - [SDR GUUA95532123110A](https://openairdocs.org/sdr/GUUA95532123110A.md): Annunciator · inoperative · Dec 31, 2010 · N87555 · Beech 1900D · Landing Gear Position and Warning > PILOT REPORTED LANDING GEAR "R" ANNUNCIATOR INOPERATIVE. RESET "R" ANNUNCIATOR IN SOCKET. OPS CHECK NORMAL. - [SDR GUUA95552121910A](https://openairdocs.org/sdr/GUUA95552121910A.md): Latch · out of adjust · Dec 19, 2010 · N87555 · Beech 1900D · Passenger/Crew Doors > PILOT REPORTS AIRSTAIR DOOR DIFFICULT TO CLOSE. RE-INDEXED CAM LATCHES OPS CHECK GOOD. - [SDR GUUA95552121310A](https://openairdocs.org/sdr/GUUA95552121310A.md): Handle · stiff · Dec 13, 2010 · N87555 · Beech 1900D · Emergency Exits > DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE. - [SDR GUUA52121310A](https://openairdocs.org/sdr/GUUA52121310A.md): Handle · stiff · Dec 13, 2010 · N87555 · Beech 1900D · Emergency Exits > DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE. - [SDR GUUA95552120410A](https://openairdocs.org/sdr/GUUA95552120410A.md): Cable · frayed · Dec 4, 2010 · N87555 · Beech 1900D · Passenger/Crew Doors > DURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR FWD LOWER LATCH CABLE FRAYED. REPLACED AIRSTAIR DOOR FWD LOWER LATCH CABLE OPS CHECK GOOD. - [SDR GUUA95552092110A](https://openairdocs.org/sdr/GUUA95552092110A.md): Handle · lack of lube · Sep 21, 2010 · N87555 · Beech 1900D · Emergency Exits > DURING SCHEDULED ROUTINE MX DISCOVERED 6A EMERGENCY EXIT HANDLE HARD TO OPEN. LUBRICATED 6A EMERGECNY EXIT HANDLE OPS CK OK. - [SDR GUUA95552080510A](https://openairdocs.org/sdr/GUUA95552080510A.md): Door · lack of lube · Aug 5, 2010 · N87555 · Beech 1900D · Emergency Exits > DURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT DOOR HARD TO OPEN. LUBRICATED LT EMERGENCY EXIT DOOR. - [SDR GUUA95532070310A](https://openairdocs.org/sdr/GUUA95532070310A.md): Relay · failed · Jul 3, 2010 · N87555 · Beech 1900D · Landing Gear Retraction/Extension System > FLIGHT 9242 MHH/FLL PILOT REPORTED LANDING GEAR DID NOT RETRACT. REPLACED LANDING GEAR MOTOR RELAY, OPERATIONAL CHECK OK. - [SDR GUUA95532052710A](https://openairdocs.org/sdr/GUUA95532052710A.md): Motor · inoperative · May 27, 2010 · N87555 · Beech 1900D · Landing Gear Retraction/Extension System > DURING DESCENT WHEN EXTENDING LANDING GEAR THE MOTOR STOPPED RUNNING, AND THE IN TRANSIT LIGHT REMAINED ILLUMINATED, THE LANDING GEAR HORN BEGAN TO SOUND WITH NO MOVEMENT OF POWER LEVERS, NO ILLUMINATION OF 3 GREEN LIGHTS AFTER A FEW SECONDS THE 3 GREEN LANDIN - [SDR GUUA95532052410A](https://openairdocs.org/sdr/GUUA95532052410A.md): Warning Light · false activation · May 24, 2010 · N87555 · Beech 1900D · Landing Gear Position and Warning > PILOT REPORTED LANDING GEAR WARNING LIGHTS ILLUMINATE AND HORN SOUNDS WHEN EXTENDING GEAR EVEN WITH SILENCE BUTTON DEPRESSED. PERFORMED LANDING GEAR EXTENSION AND RETRACTION COULD NOT DUPLICATE THE PROBLEM NO DEFECTS FOUND, OPS CHECK NORMAL. - [SDR GUUA95532050910A](https://openairdocs.org/sdr/GUUA95532050910A.md): Annunciator · loose · May 9, 2010 · N87555 · Beech 1900D · Landing Gear Position and Warning > PILOT REPORTED L/R GREEN GEAR ANNUNCIATOR DOES NOT SEAT PROPERLY IT NO LONGER ILLUMINATES AND WILL NOT PRESS TO TEST UNLESS YOU MANUALLY HOLD IT IN. RESECURED SOCKET AT CTR L/R GREEN ANNUNCIATOR OPS CHECK GOOD. - [SDR GUUA95532050810A](https://openairdocs.org/sdr/GUUA95532050810A.md): Indicator · loose · May 8, 2010 · N87555 · Beech 1900D · Landing Gear Position and Warning > PILOT REPORTED MIDDLE LIGHT ASSEMBLY OF GREEN GEAR INDICATOR LIGHTS DOES NOT STAY ON. RESECURED MIDDLE LIGHT ASSY OF GREEN INDICATOR LIGHT, OPS CHECK OK. - [SDR GUUA95552120409A](https://openairdocs.org/sdr/GUUA95552120409A.md): Strut · discharged · Dec 4, 2009 · N87555 · Beech 1900D · Entrance Stairs > PILOT REPORTED PASSENGER DOOR VERY HEAVY TO OPERATE GAUGE READS 1,000 PSI. SERVICED PASSENGER DOOR STRUT TO 1,400 PSI OPS CHECK GOOD. - [SDR GUUA95553091509A](https://openairdocs.org/sdr/GUUA95553091509A.md): Structure · corroded · Sep 15, 2009 · N87555 · Beech 1900D · Fuselage Main, Plate/Skin > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED CORROSION ON FUSELAGE APPROXIMATELY AT FS 243 TO 258 AT STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED INSERTION REPAIR PATCH AND EXTERNAL DOUBLER REPAIR AND REPAIRED DAMAGED STR. - [SDR GUUA95532081209A](https://openairdocs.org/sdr/GUUA95532081209A.md): Master Cylinder · failed · Aug 12, 2009 · N87555 · Beech 1900D · Master Cylinder/Brake Valve > PILOT REPORTS RT BRAKE GOES TO FLOOR WITH NO BRAKING ON CAPTAIN`S BRAKE. REPLACED CAPTAIN RT BRAKE MASTER CYL. OPS CHECK SATISFACTORY. NOTE: PREVIOUSLY SUBMITTED OPEN - [SDR GUUA95552070509A](https://openairdocs.org/sdr/GUUA95552070509A.md): Clevis · bent · Jul 5, 2009 · N87555 · Beech 1900D · Passenger/Crew Doors > PILOT REPORTED CABIN DOOR HARD TO OPEN FROM THE OUTSIDE. FOUND AIRSTAIR DOOR LWR FWD HANDRAIL CABLE UPPER CLEVIS BENT AND CATCHING ON STRUT COUNTER BALANCE, REPLACED LWR FWD AIRSTAIR DOOR HANDRAIL CABLE. - [SDR GUUA95557060509A](https://openairdocs.org/sdr/GUUA95557060509A.md): Skin · corroded · Jun 5, 2009 · N87555 · Beech 1900D · Wing, Plate/Skin > DURING SCHEDULED ROUTINE INSP DISCOVERED LT WING UPPER SKIN HAD CORROSION AT LWS 147.74. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER. - [SDR GUUA95557073008A](https://openairdocs.org/sdr/GUUA95557073008A.md): Skin · corroded · Jul 30, 2008 · N87555 · Beech 1900D · Wing, Plate/Skin > DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING, UPPER SKIN, T/E HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194.85. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER. - [SDR GUU2008F00002](https://openairdocs.org/sdr/GUU2008F00002.md): Uplock Switch · out of adjust · Jul 2, 2008 · N87555 · Beech 1900D · Landing Gear Position and Warning > DURING FLIGHT LANDING GEAR IN TRANSIT LIGHT ILLUMINATED. ADJUSTED LEFT LANDING GEAR UPLOCK SWITCH. (K) - [SDR GUU2008F00003](https://openairdocs.org/sdr/GUU2008F00003.md): Wire · broken · Jul 1, 2008 · N87555 · Beech 1900D · Landing Gear System Wiring > AFTER TAKEOFF LANDING GEAR DID NOT RETRACT, LANDING GEAR CIRCUIT BREAKER POPPED WHEN HANDLE PUT DOWN WITH ONLY (2) GREEN LIGHTS. CIRCUIT BREAKER PUSHED IN AND GEAR WENT DOWN BREAKER POPPED AGAIN. RETURNED TO PBI LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE S - [SDR GUU2008F00018](https://openairdocs.org/sdr/GUU2008F00018.md): Relay · malfunctioned · Jun 8, 2008 · N87555 · Beech 1900D · Landing Gear Retraction/Extension System > FLIGHT 9225, DURING APPROACH, LANDING GEAR RELAY POPPED ON EXTENSION OF LANDING GEAR, MOTOR RAN UNTIL IT POPPED AND RT DOWN AND LOCK ANNUNCIATOR ILLUMINATED. INSPECTED LANDING GEARS, ACTUATORS AND SWITCHES ALL SECURE. LANDING GEAR OPERATIONAL CHECKS NORMAL. (A - [SDR GUUA04210803](https://openairdocs.org/sdr/GUUA04210803.md): Cap · missing · Apr 21, 2008 · N87555 · Beech 1900D · Landing Gear Retraction/Extension System > FLIGHT 9197, AFTER TAKEOFF, NOSE LANDING GEAR TAKES EXCESS TIME TO RETRACT. INSTALLED AIR REGULATOR PORT CAP. OPERATIONAL CHECK NORMAL. - [SDR GUUA04050801](https://openairdocs.org/sdr/GUUA04050801.md): Torque Tube · corroded · Apr 5, 2008 · N87555 · Beech 1900D · Elevator Structure > DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED LT ELEVATOR TORQUE TUBE. - [SDR GUUA04040801](https://openairdocs.org/sdr/GUUA04040801.md): Cable · broken · Apr 4, 2008 · N87555 · Beech 1900D · Entrance Stairs > FLIGHT: 9205, PILOT REPORTED (4) REAR CAMS ON FWD CABIN DOOR WILL NOT ROTATE WHEN DOOR IS SECURED. REPLACED AIRSTAIR DOOR DOWN AFT CABLE. - [SDR GUUA09270702](https://openairdocs.org/sdr/GUUA09270702.md): Hinge Bracket · corroded · Sep 27, 2007 · N87555 · Beech 1900C · Horizontal Stabilizer Structure > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT OB ELEVATOR HINGE BRACKET. - [SDR GUUA09270703](https://openairdocs.org/sdr/GUUA09270703.md): Hinge Bracket · corroded · Sep 27, 2007 · N87555 · Beech 1900D · Horizontal Stabilizer Structure > AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT IB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT IB ELEVATOR HINGE BRACKET. - [SDR GUUA09260701](https://openairdocs.org/sdr/GUUA09260701.md): Skin · damaged · Sep 26, 2007 · N87555 · Beech 1900D · Fuselage Main, Plate/Skin > AT SCHEDULED INSPECTION DISCOVERED LT FUSELAGE SKIN EXFOLIATED AT FS 213.250 BETWEEN STRINGERS 13L TO 14L. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW SRM 51-70-06. - [SDR GUUA05180701](https://openairdocs.org/sdr/GUUA05180701.md): Connector · loose · May 18, 2007 · N87555 · Beech 1900D · Landing Gear System Wiring > FLIGHT:9167 PBI/TLH - AFTER TAKEOFF LANDING GEAR DID NOT RETRACT. RETURNED TO PBI, SELECTED GEAR DOWN LEFT MAIN GEAR WOULD NOT GIVE A SAFE DOWN LOCKED INDICATION. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. RESECURED MAIN LANDING GEAR LEFT AND - [SDR GUUA08020601](https://openairdocs.org/sdr/GUUA08020601.md): Hinge Bracket · corroded · Aug 2, 2006 · N87555 · Beech 1900D · Horizontal Stabilizer Structure > AT SCHEDULED ROUTINE MAINTENANCE LEFT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LEFT CENTER ELEVATOR HINGE BRACKET. Next page: https://openairdocs.org/deregistered/N87555-2013-06-19/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 = 'N87555' AND deregistration_id = 'N87555-2013-06-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N87555-2013-06-19/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.