JASC 5280

Service difficulty reports · 3,557

Reports filed under 5280 · Landing Gear Doors, newest first.

Query with SQL
duckdb -csv -c "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 jasc_code = '5280'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR RRXA002657Skin · dentedDURING A MAINTENANCE VISIT FOUND 2 DENTS IN SKIN BELOW GROUND POWER RECPT PLATE AT NOSE GEAR/FWD DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0,May 1, 2000 · N8084U · Doug DC871FSDR MWEA00386Angle · crackedLEFT MAIN LANDING GEAR DOOR JAMB ANGLE CRACKED JUST BELOW HYDRAULIC RESERVOIR. FABRICATED AND INSTALLED REPAIR DOUBLER.May 1, 2000 · N205ME · Doug DC932SDR MWEA00385Angle · crackedLEFT MAIN LANDING GEAR DOOR JAMB ANGLE CRACKED JUST ABOVE ATTACH FITTING ABOVE AFT SECTION OF DOOR HINGE. FABRICATED AND INSTALLED REPAIR PARTS.May 1, 2000 · N205ME · Doug DC932SDR P2EA00180Structure · crackedSJO - DURIG C-CHECK, FOUND THE LEFT MAIN LANDING GEAR CENTER DOOR TRAILING EDGE WITH CRACK 2 INCHES LONG BY .002 INCHES WIDE. REPAIRED THE LEFT MAIN LANDING GEAR CENTER DOOR TRAILING EDGE IAW SRM 51-40-3 FIG 1. (M)Apr 28, 2000 · N209US · Boeing 737222SDR MWEA00382Angle · crackedRIGHT MAIN LANDING GEAR DOOR JAMB ANGLE CRACKED JUST ABOVE ATTACH FITTING AND BELOW ADEL CLAMP BY AFT SECTION OF DOOR HINGE. FABRICATED AND INSTALLED REPAIR DOUBLER.Apr 26, 2000 · N205ME · Doug DC932SDR GAIA00229Fitting · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, LEFT LANDING GEAR DOOR FORWARD HINGE FITTING HAS CORROSION ON GOUGE IN LARGE HOLE. INSTALLED NEW FITTING IAW S/B 727-57-180 AND SRM 51-30-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 25, 2000 · N854AA · Boeing 727223SDR USAA000723Angle · crackedPIT - Q-6 - ANGLE BRACKET CRACKED APPROXIMATELY .50 INCH LONG. BRACKET AT FORWARD INBOARD CORNER OF WHEELWELL DOOR JAMB. REPLACED CRACKED ANGLES PER SRM 53-05-60. (X)Apr 24, 2000 · N818US · Doug DC982SDR 00FDEA00287Fitting · crackedLT MLG DOOR RIB FITTING CRACKED ABOVE THE ACTUATOR POINT. R&R LT MAIN LG DOOR IAW MM 32-12-1.Apr 24, 2000 · N222FE · Boeing 727233SDR TWAA0006611Structure · crackedDURING CHECK-C MAINT AT THE LT MAIN LANDING GEAR, CORNER BRACKET RT FWD BETWEEN MLG DOORS, FWD I/B CORNER OF RT MLG DOOR IS CRACKED AT STA 937. INSTALLED NEW CORNER BRACKET PER SRM 51-30 -05.Apr 24, 2000 · N9306T · Doug DC983SDR CALA0000478Skin · puncturedINSPECTION FOUND THREE HOLES PUNCTURED INTO RT I/B MLG DOOR OUTER SKIN UPPER BLOCK. THE DAMAGED SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 15, 2000 · N16804 · Doug DC982SDR CALA0000466Doubler · crackedINSPECTION FOUND A 6 INCH CRACK IN LT MLG DOOR I/B LOWER AFT CORNER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28 AND 51-30-5.Apr 13, 2000 · N16804 · Doug DC982SDR RRXA001901Door · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING FLYING DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW DOOR IAW DC-8 SRM 51-3-0 AND MM 52-10-0.Apr 11, 2000 · N961R · Doug DC873FSDR RRXA001765Door · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING MLG DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW DOOR IAW DC-8 SRM 51-3-0 AND DC-8 MM 52-10-0.Apr 11, 2000 · N961R · Doug DC873FSDR CALA0000461Skin · gougedINSPECTION FOUND RT MLG DOOR LOWER SKIN, GOUGED ON O/B SIDE. THE GOUGED SKIN SECTION WAS REMOVED AND A NEW SKIN SECTION WAS INSTALLED IAW SRM 51-30-2.Apr 11, 2000 · N16804 · Doug DC982SDR RRXA001967Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 898, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW CLIP IAW DC-8 SRM 5Apr 4, 2000 · N961R · Doug DC873FSDR RRXA001832Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 898, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW CLIP IAW DC-8 SRM 5Apr 4, 2000 · N961R · Doug DC873FSDR 20000504SH008Door · wrong partDOOR HAS BEEN IDENTIFIED AS A DASH 185. DOOR IS NOT A DASH 185, BUT A DASH 1. DOOR HAS NOT BEEN MODIFIED PER SB 32-318 WHICH ALLOWS USE OF LARGER DIAMETER DRAG STRUT FOR MLG. THIS DOOR WAS BINDING WITH DRAG STRUT WHICH MAY HAVE CAUSED DIFFICULTY EXTENDING TApr 4, 2000 · Boeing 727*SDR DHL200072603CDoor · crackedLEFT MAIN LANDING GEAR DOOR CRACKED AT LOWER PANEL REAR I/B AREA. STOP DRILL ON LEFT MLG WING DOOR ON LOWER PANEL REAR I/B AREA PER SRM 51-10-1. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER REPAIR PER SRM 51-40-3 FIG 1.Apr 4, 2000 · N726DH · Boeing 727228SDR RRXA001969Hinge · looseDURING A MAINTENANCE VISIT FOUND PLAY ON LEFT MAIN LANDING GEAR DOOR HINGES AT AIRFRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW HINGE IAW DC-8 SRM 51-1-20D AND 51-3-0.Mar 30, 2000 · N961R · Doug DC873FSDR RRXA001966Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, Mar 30, 2000 · N961R · Doug DC873FSDR RRXA001965Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 963, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRMMar 30, 2000 · N961R · Doug DC873FSDR RRXA001964Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 955, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRMar 30, 2000 · N961R · Doug DC873FSDR RRXA001963Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 963, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRMMar 30, 2000 · N961R · Doug DC873FSDR RRXA001834Hinge · looseDURING A MAINTENANCE VISIT FOUND PLAY IN THE I/B LEFT MLG DOOR HINGES ON AIR FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED HINGE IAW DC-8 SRM 51-1-20D AND 51-3-0.Mar 30, 2000 · N961R · Doug DC873FSDR RRXA001831Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 945, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRMMar 30, 2000 · N961R · Doug DC873FSDR RRXA001830Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 963, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED CLIP IAW DC-8 SRM 51-Mar 30, 2000 · N961R · Doug DC873FSDR RRXA001829Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 955, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED CLIP IAW DC-8 SRM 51-Mar 30, 2000 · N961R · Doug DC873FSDR RRXA001828Clip · crackedDURING A MAINENANCE VISIT FOUND A CRACK TO THE RT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 963, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED CLIP IAW DC-8 SRM 53-2Mar 30, 2000 · N961R · Doug DC873FSDR DL72K000599Door · separatedRIGHT MAIN GEAR FLYING DOOR CAME OFF DURING FLIGHT. REPLACED SAME.Mar 29, 2000 · N414DA · Boeing 727232SDR ABXA000192Door · corrodedLEFT FORWARD NOSE LANDING GEAR DOOR CORRODED AT AFT END UNDER DEFLECTOR. REPLACED DOOR IAW DC9 MM 32-22-01-2-0004.Mar 27, 2000 · N975AX · Doug DC941SDR DHL2000804138Structure · crackedRT MLG SHOCK STRUT CENTRAL DOOR STRUCTURE CRACKED. REMOVED DAMAGED DOOR PER SRM 51-1-21. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED NEW DOOR PER SRM 51-1-21.Mar 25, 2000 · N804DH · Doug DC873FSDR MWEA00186Channel · damagedLEFT MAIN LANDING GEAR DOOR OUTBOARD Z-CHANNEL AND SKIN ARE CHANGED BEYOND REPAIR LIMITS. MAINTENANCE REMOVED AND REPLACED SKIN AND Z-CHANNEL.Mar 25, 2000 · N806ME · Doug DC981SDR LR7A0031Door · bentDURING SCHEDULED A CHECK PER HA1200, FOUND AFT NLG DOOR TRAILING EDGE SKIN BENT AND TORN. REPAIRED IAW LAC MEA 382-53-00-039. D&C 2.Mar 23, 2000 · N404LC · Lkheed 382GSDR CALA0000312Angle · chafedINSPECTION FOUND RT MLG DOOR AFT LOWER INNER CORNER REPAIR ANGLE DEEPLY CHAFED. AN INNER CORNER DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 28, 51-10-04, AND 51-10-03.Mar 18, 2000 · N938AS · Doug DC982SDR RRXA001968Retainer · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR SEAL RETAINER AT STA 890 AT KEEL BEAM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SMar 14, 2000 · N961R · Doug DC873FSDR RRXA001833Retainer · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR SEAL RETAINER AT STA 890 AT KEEL BEAM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 Mar 14, 2000 · N961R · Doug DC873FSDR CALA0000303Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN PREVIOUS DOUBLER REPAIR OF UPPER FORWARD CORNER RT MLG DOOR. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Mar 13, 2000 · N17812 · Doug DC982SDR USAA000470Rib · crackedPIT - FOUND NR 6 RIB HAS 2 INCH CRACK IN RIGHT MLG DOOR 16 INCHES FROM OUTBOARD END. INSTALLED DOUBLER PER SRM 52-01, PAGE 9 FIG 2. (M)Mar 9, 2000 · N816US · Doug DC982SDR USAA000471Pan · crackedPIT - FOUND 2 INCH CRACK IN RIGHT MLG DOOR PAN CRACKED, FORWARD INBOARD SIDE BY ACTUATOR BRACKET. SPLICED INBOARD SECTION OF PAN PER SRM 52-05 FIG 28 SHT 3 VIEW B AND PG 25. (M)Mar 9, 2000 · N816US · Doug DC982SDR DHL200072439CHinge · crackedAT C CHECK, FOUND RT WW DOOR I/B SECTION, CENTER FWD HINGE CRACKED. REMOVED AND REPLACED WITH NEW CENTER FWD HINGE AT RT WW DOOR I/B SECTION. OPS CHECKED PER MM 32-30-00.Mar 2, 2000 · N724DH · Boeing 727228SDR DHL200072438CHinge · crackedFOUND AT C CHECK, RT WHEEL WELL DOOR I/B SECTION OF HINGE IS CRACKED. REMOVED AND REPLACED WITH NEW AFT HINGE AT RT WW DOOR I/B SECTION. OPS CHECKED.Mar 2, 2000 · N724DH · Boeing 727228SDR AT0000112Latch · looseAIRCRAFT RETURNED FROM FLIGHT DUE TO UNSAFE GEAR UP INDICATION. TIGHTENED LEFT GEAR DOOR LATCH IAW DC9 MM.Mar 1, 2000 · N839AT · Doug DC932SDR QXEA0000702Door · chafedPDX- RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR IS CHAFING ON THE AFT LUG OF THE AFT BRACKET AT STRUT ATTACH POINT. REPAIRED IAW HORIZON AIR EA 4-57-374.Mar 1, 2000 · N478US · Fokker F28MK4000SDR CALA0000225Channel · crackedINSPECTION FOUND A 3 INCH CRACK IN LT MLG I/B DOOR UPPER L/E CORNER. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05, AND 51-30-08.Feb 29, 2000 · N938MC · Doug DC983SDR MWEA00082Structure · damagedAFTER TOWBAR DISCONNECT, TUG DRIVER CAUSED TOWBAR TO STRIKE AIRCRAFT DAMAGING RIGHT NOSE GEAR DOOR. MAINTENANCE REMOVED AND REPLACED RIGHT NOSE GEAR DOOR.Feb 27, 2000 · N501ME · Doug DC932SDR 2000ZZZX717Support · crackedTHE CHANNEL AND CHANNEL SUPPORT ARE NOSE GEAR DOOR LINKAGE SUPPORT STRUCTURES. DURING A ROUTINE INSPECTION, THESE ITEMS WERE FOUND TO BE CRACKED AND HAD SHIFTED POSITION WITHIN THE NOSE TUNNEL STRUCTURE. EVEN A SMALL CHANGE IN THE POSITION OF THESE PARTS CHAFeb 23, 2000 · N6632R · Beech 76SDR 2000ZZZX716Channel · crackedTHE CHANNEL AND CHANNEL SUPPORT ARE NOSE GEAR DOOR LINKAGE SUPPORT STRUCTURES. DURING A ROUTINE INSPECTION, THESE ITEMS WERE FOUND TO BE CRACKED AND HAD SHIFTED POSITION WITHIN THE NOSE TUNNEL STRUCTURE. EVEN A SMALL CHANGE IN THE POSITION OF THESE PARTS CHAFeb 23, 2000 · N6632R · Beech 76SDR CALA0000179Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN LEFT MLG I/B DOOR AT LOWER FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW EA 5281-2-A064 AND ECRA 5280-01220.Feb 21, 2000 · N938MC · Doug DC983SDR ABXA000116Skin · delaminatedRIGHT MAIN LANDING GEAR OUTBOARD DOOR WAS DELAMINATED BEYOND LIMITS. REPLACED DOOR IAW DC9 SRM 51-30-2 AND DC9 OHM 32-10-6.Feb 17, 2000 · N971AX · Doug DC941SDR CA000218012Support Bracket · cracked(CAN) DURING CRUISE, CREW HEARD A KNOCKING SOUND ACCOMPANIED BY A NOISE THAT PULSATED LOUDER AS AIRSPEED INCREASED. AFTER LANDING, CREW NOTICED RT INBOARD MLG DOOR HAD PULLED FREE OF THE DOOR ROD. THE DOOR ROD RECEIVING BALL HAD PULLED THROUGH THE SUPPORT ASSFeb 1, 2000 · Emb EMB110P1
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