N396AN, cancelled Mar 23, 2022
Service difficulty reports · 137
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N396AN' AND deregistration_id = 'N396AN-2022-03-23' 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.
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 = 'N396AN' AND deregistration_id = 'N396AN-2022-03-23' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MK1Y202201025None · noneTHE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE RIGHT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR.
RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTISDR MK1Y202201024None · noneTHE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE LEFT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR.
RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTIFSDR MK1Y202201023None · noneDENT DAMAGE AND AN EXISTING BLEND-OUT WAS FOUND ON THE LOWER WING SKIN PANEL (P/N 112T4702-1) COMMON TO THE OUTBOARD STRINGER L-9.5 (P/N 767-3421-7) BETWEEN WS 990.2 AND WS 1006. AN EXISTING FREEZEPLUG AND THE OUTBOARD STRINGER L-9.5 HAD BEEN INSTALLED PER SERSDR MK1Y202201022None · nonePROBLEM DESCRIPTION: ENGINE #2, THRUST REVERSER TRANSLATING COWL, INNER SKIN, P/N CF6-F23G019, S/N R647-129:
DURING MAINTENANCE INSPECTION AT IAI A CRACKED DENT WAS FOUND IN THE INNER SKIN OF INBD THRUST REVERSE IN CLOSE PROXIMITY TO AN EXISTING REPAIR OF ENSDR MK1Y202201021None · noneR/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 – WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.SDR MK1Y202201020None · noneL/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 – WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.SDR MK1Y202201019None · nonePROBLEM DESCRIPTION: SLAT NO. 4, OSS 579.05:
SHOP FOUND A DENT ADJACENT TO A BULGE IN UPPER LE SKIN OF SLAT NO. 4. THE DAMAGED AREA LOCATED ON A RIB AND STIFFENER. SLAT: P/N 114T4104-203G; S/N 000010.SDR MK1Y202201018None · noneFUSELAGE SKIN (SEC 45), STA 999 AND STA 1043, STR-2L AND STR-2R: DURING CONVERSION PROCESS, AIRCRAFT MAINTENANCE WAS REQUIRED TO DEACTIVATE AND REMOVE THE HIGH GAIN SATCOM SYSTEM PER CUSTOMER REQUEST THAT WAS INSTALLED BY THE PREVIOUS OPERATOR. THE LARGE EXTERSDR MK1Y202201017None · nonePROBLEM DESCRIPTION: SLAT NO 5 AT OSS 389.71:
SHOP FOUND DENT AMONG FASTENERS AT THE EDGE OF SLAT LE SKIN ATTACHMENT COMMON TO A RIB. THE REPORTED DAMAGE WAS FOUND SMOOTH WITHOUT SHARP EDGES OR LOOSE FASTENERS.SDR MK1Y202201016None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT RBL10.33 STR U3 TO REAR SPAR: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WAS ACCOMPLISHED. THESDR MK1Y202201015None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT LBL10.83 STR U3 TO U2 AND LBL 11.83 STR U2 TO U1: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WSDR MK1Y202201013None · nonePROBLEM DESCRIPTION: #2 ENGINE OUTBOARD THRUST REVERSER DAGMAR FAIRING DAMAGE, ASSY IDENT: 683L136613, MODEL NO. TR-CF6-F23G019, S/N R647-129:
DURING MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOVERED ELONGATED HOLES SUNK RIVETS AND GOUGES ACROSS THE FASTSDR MK1Y202201012None · noneENGINE #1 OUTBD CORE COWL HAT FRAME NAC STA 303.75, LOWER AREA: DURING THE MAINTENANCE INSPECTION AT IAI, CRACK WAS FOUND AT DATUM LOCATION WITH 1.5 INCH LENGTH.SDR MK1Y202201011Tear Strap · corrodedTEAR STRAP, INNER SKIN, STA 544, S-1R AND S-4R, DOOR SURROUND ZONE: SHOP DISCOVERED DEEP CORROSION ON TEAR STRAP EDGE COMMON TO S-2R (LAP SPLICE). THE DAMAGED AREA IS LOCATED IN CONVERSION INSTALLATION ZONE.SDR MK1Y202201010None · nonePROBLEM DESCRIPTION: R/H WING LOWER SKIN SURFACE BETWEEN WS.994.7 AND WS.1001.7: SHOP FOUND TOOL MARK AMONG FASTENERS, PAINT STRIPPED AND PERFORMED NDT THICKNESS INSPECTION WAS PERFORMED .SDR MK1Y202201009None · noneWORN CORE COWL ALUMINUM HAT FRAME –
ENGINE# 1, R/H CORE COWL, HAT FRAME, NAC STA 303.75, UPPER AREA
DURING THE MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOVERED
ON #1 ENGINE, R/H CORE COWL HAT CHANNEL FRAME NAC STA 303.75 UPPER
SECTION WITH WORN, DAMASDR MK1Y202201008None · none. DURING A/C SURVEY AT TLV, MAINTENANCE DISCOVERED EXISTING BLENDOUT AT THE EDGE OF AN EXISTING FLUSH REPAIR CUTOUT LOCATED ON THE FUSELAGE SKIN AT STA 616 BETWEEN S38L AND S39L. THE EXISTING FLUSH REPAIR WAS FOUND TO BE INSTALLED BY THE PRIOR OPERATOR, AMERISDR MK1Y202201007None · noneENGINE # 2, LH CORE COWL, HAT FRAME, NAC STA 303.75, MID LOWER AREA: DURING MAINTENANCE INSOECTION AT IAI, MAINTENANCE DISCOVERED ON #2 ENGINE, LH CORE COWL HAT CHANNEL FRAME NAC STA 303.75 MID LOWER SECTION WITH CRACK AND GOUGE. PLEASE REFER TO FIGURE 2 FOR TSDR MK1Y202201006None · noneNLG SUPPORT STRUCTURE, AFT VERTICAL STIFFENERS, UPPER EDGES, STA 287, L/RBL 13.10 DURING THE MAINTENANCE INSPECTION AT IAI, TWO CRACKS WERE FOUND AT DATUM LOCATIONS WITH 0.6 INCH LENGTH EACH ONE. THERE IS NO APPLICABLE DAMAGE EXISTING.
VERTICAL STIFFENERS PISDR MK1Y202201005None · noneEXTERNAL FUSELAGE SKIN, STA 1487, STR-21L & STA 1460, STR-29L-STR-30L:
DURING THE MAINTENANCE INSPECTION AT IAI, SCRATCHES WERE FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUTS EXCEED\ THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFESDR MK1Y202201004None · noneEXTERNAL FUSELAGE SKIN, STA 308, STR-33L:
DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.SDR MK1Y202201003None · noneEXTERNAL FUSELAGE SKIN, STA 588, STR-33R:
DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.SDR MK1Y202201002None · noneFAN COWL SUPPORT BEAM LINK, #2 PYLON, P/N 31112522-1
DURING THE MAINTENANCE INSPECTION AT IAI, THE BORES IN THE #2 PYLON FAN COWL SUPPORT BEAM LINK PIN 311T2522-1 WERE FOUND TO BE WORN. THE BORE DIAMETERS WERE FOUND TO BE Ø.8770". THE NOMINAL DIAMETER OF THESDR MK1Y202201001None · nonePROBLEM DESCRIPTION: DURING THE MAINTENANCE INSPECTION FOUND SCRATCHES ON EXTERNAL FUSELAGE SKIN AMONG FASTENERS AREA.
- SHOP CLEANED DAMAGED AREA IAW SRM 51-10-02. SHOP REMOVEDSDR AALA2020022089025Clutch · stickingAIRCRAFT WAS NOT GROUNDED: LEFT THROTTLE STICKING AUTO AND MANUAL OPERATION DOES NOT KEEP UP WITH RIGHT THROTTLE IN AUTO MODE. REPLACED AUTO THROTTLE CLUTCH PACK PER AMM 22-32-05.SDR 2019FA0000383Light · inoperative7A SEAT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-10. OPS CHECK GOOD.SDR AALA201910039007Access Panel · damagedAIRCRAFT WAS GROUNDED: CABIN FLOOR ACCESS PANEL FOR E&E COMPARTMENT BOARD SOFT. REPLACED ACCESS PANEL PER AMM 52-48-05.SDR AALA201906189013Slide · low pressureAIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS L1 DOOR SLIDE DOES NOT SHOW NEEDLE SHADOW IN GREEN BAND AND IS OUT OF LIMITS FOR PRESSURE GAUGE ON LOW SIDE. REMOVED AND REPLACED SLIDE ASSY IAW AMM 25-66-01. ALL CHECKS NORMAL.SDR AALA20190512004Support Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SUPPORT FITTING AT BS 1570 ON THE LAVATORY DUMP CRANK TOWER. REPLACED SUPPORT FITTING PER SRM 51-40-02.SDR AALA20190512002Shear Tie · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHEAR TIE AT BS 1562 AND BL 0. REPLACED SHEAR TIE PER SRM 51-10-02-0GSDR AALA201902264001Fuel Filter · dirtyDURING CLIMB, THE RIGHT ENGINE FUEL FILTER LIGHT ILLUMINATED. REFERRED TO THE QRH, ADVISED TO LAND AS SOON AS POSSIBLE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACCOMPLISHED MCM 4918. RT FUEL FILTER ELEMENTS REMOVED ASDR AALA2018102979001Flashlight · no testEMERGENCY FLASHLIGHTS AT THE FLIGHT ATTENDANTS JUMPSEAT, DID NOT TEST. REPLACED THE FLASHLIGHT AND TESTED GOOD IAW FIM 25-60-05.SDR AALA2018101529023Battery Pack · inoperativeMID CABIN, LEFT SIDE ,AFT FLIGHT ATTENDANT SEAT FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLASHLIGHT BATTERY IAW GPM 05-01-07. OPS CHECKED GOOD.SDR AALA2018091879012Antenna · faultedWEATHER RADAR FAILED DURING FLIGHT. ACCOMPLISHED TROUBLESHOOTING IAW FIM 34-43-00, FOUND WEATHER RADAR PANEL AND ANTENNA AT FAULT. AN EMERGENCY WAS DECLARED, RETURNED TO DEPARTURE, AND AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED IASDR AALA2018091879004Control Panel · failedWEATHER RADAR FAILED DURING FLIGHT. AN EMERGENCY WAS DECLARED, RETURNED TO DEPARTURE, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED TROUBLESHOOTING IAW FIM 34-43-00, FOUND THE WEATHER RADAR PANEL AND ANTENNA AT FAULT. REPLACED IAW MM 3SDR AALA201807129024Battery · inoperativeMID GALLEY LEFT SIDE LOWER ACCESS DOOR DETACHABLE FLASHLIGHT BATTERY INOPERATIVE. REPLACED THE BATTERY. CHECKED NPRMAL.SDR AALA20180327007Light · inoperativeSEAT 3J MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED 3J SEAT MOUNTED EMERGENCY LIGHT ASSY IAW AMM 33-51-10. OPS CHECKED NORMAL. AIRCRAFT WAS GROUNDED.SDR AALA201801199005Battery · no testFLASHLIGHT AT THE JUMPSEAT REAR LEFT FLIGHT COMPARTMENT BATTERY WILL NOT TEST. REPLACED THE BATTERY IAW AMM 25-64-00.SDR AALA201712279032Threshold · looseFIRST CLASS FORWARD LAVATORY DOOR STICKING AT THRESHOLD BASE. TIGHTENED THRESHOLD SCREWS. CHECKED NORMAL.SDR AALA20171205003Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER ON FORWARD SIDE OF FRAME 246 AT LBL26. INSTALLED ANGLE STIFFENER PER SRM 53-10-51-2R3.SDR AALA20171204002Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER AT STA. 246 LEFT BUTTLINE 2 AND LEFT BUTTLINE 6. REPLACED STIFFENER AT STA. 246 LEFT BUTTLINE 2 AND LEFT BUTTLINE 6 PER SRM 53-10-51-2R3.SDR AALA20171204001Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENERS ON STA. 246 AT LEFT BUTTLINE 0 TO LEFT BUTTLINE 4. REPLACED STIFFENERS ON STA. 246 AT LEFT BUTTLINE 0 TO LEFT BUTTLINE 4 PER SRM 53-10-51-2R3.SDR AALA201709059036Smoke Detector · no testTHE AIRCRAFT WAS NOT GROUNDED. PASSENGER SMOKING IN LAV A5. SMOKE DETECTION SYSTEM DID NOT INDICATE ANY SMOKE. LAV A5 SMOKE DETECTOR OPS CHECK PERF IAW AMM 26-13-00-715-090, TEST OK. THERMAL STICKER IN WASTE BIN CHECKED FOR SIGNS OF HEAT, NIL EVIDENT. A/C OKSDR AALA201707249032Pump · failedDURING FLIGHT LEFT FWD BOOST PUMP WOULD NOT WORK AFTER BALANCING FUEL. CIRCUIT BREAKER DISCOVERED TRIPPED. REMOVED AND REPLACED LEFT FWD BOOST PUMP IAW AMM 28-22-03. OPS CHECKED AND LEAK CHECKED GOOD.SDR AALA201706279041Lens · detachedAIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE L1 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-03. OPERATIONAL CHECK GOOD.SDR AALA20170622006Lens · missingEMERGENCY EXIT CEILING LIGHT NEAR SEATS 26G AND 25H HAS A MISSING LENS. REPLACED THE LENS IAW AMM 33-51-04. OPS CHECKED GOOD.SDR AALA201706019034Attach Angle · corrodedLEFT ENGINE FAN CASE NOSE COWL ATTACH ANGLE HAS EVIDENCE OF CORROSION AT THE 4 O'CLOCK AND 5'OCLOCK POSITIONS. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT ENGINE IAW MCM 71-93-01, 71-95-22, 71-94-45, 71-94-03, AND 71-94-43. OPERATIONAL CHECK GOOD.SDR AALA201704259001Battery Pack · no testSEAT MOUNTED EMERGENCY LIGHTS ON SEATS 22 TO 28HJ FAILED TEST. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY AT M732 IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.SDR AALA201704249031Charger · no testSEAT MOUNTED EMERGENCY LIGHTS ON SEATS 22 TO 28HJ FAILED TO TEST. REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY AT M732 IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.SDR AALA20170413002Connector · brokenAIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 39H HAS A BROKEN CONNECTOR. REMOVED AND REPLACED CONNECTOR IAW SWPM 20-64-17. OPERATIONAL CHECK IAW AMM 33-51-00 GOOD.
Back to N396AN, cancelled Mar 23, 2022