JASC 5753
Service difficulty reports · 31,513
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 jasc_code = '5753' 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 SWAA2012121710719Bracket · crackedRIGHT WING NR 6 FLAP TRACK FAIRING BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM AND DRAWING.SDR SWAA2012120710306Skin · delaminatedDELAMINATION LOCATED ON LOWER SKIN I/B FORE FLAP RIGHT WING AT 47" FROM I/B EDGE. REPAIRED LOWER SKIN I/B FORE FLAP RIGHT WING AT 47" FROM I/B EDGE IAW B737-300 SRM 51-70-10-2R-0.SDR SWAA2012112809978Spherical Bearin · looseINBOARD TRAILING EDGE I/B SPHERICAL BEARING LOOSE ON FLT TRACK. REMOVED AND REPLACED BEARING PER AMM.SDR SWAA2012112809977Spherical Bearin · looseOUTBOARD FLAP OUTBOARD TRAILING EDGE SPHERICAL ON FLIGHT TRACK IS LOOSE. REMOVED AND REPLACED BEARING PER AMM.SDR REXA2012112701534Flap · bentLEFT INBOARD FLAP TRAILING EDGE BENT. REPAIRED IAW SRM 57-52-00.SDR DALA1255190183Skin · delaminatedLT WING OTBD FLAP L/E FAIRING AREA ADJACENT NR 1 FLAP TRACK INBD FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-07, PARA 5A, FIG 9.SDR IXXA2013020700005Panel · damagedRT WING OTBD FLAP LOWER PANEL WITH SEVERAL DENTS AND SCRATCHES XF 415 - 452. PERFORMED MAJOR REPAIR IAW SRM 57-7-1, FIG 4, TR 57-94. REMOVED OTBD FLAP LOWER PANEL IAW SRM 51-3-0. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21. FABRICATED NEW PANEL PLATING 0SDR UALA2012112606744Skin · dentedRIGHT WING I/B AFT FLAP, I/B END, LOWER SKIN HAS SEVERAL DENTS. EVALUATED 5 EACH DENTS WHICH ARE NOT THE SAME AS PREVIOUSLY ARCHIVED IN CF9039 AND CF9040. 4 OF 5 DENTS ARE WITHIN LIMITS OF SRM 57-53-01: DENT HAS BEEN PERMANENTLY REPAIRED PER SRM 51-70-10, 51-SDR FDEA201211224123Vane · delaminatedLEFT WING, INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED IAW MM 27-50-22-4, REVISION 74.1. ADJUSTMENT CARRIED OUT IAW MM 27-50-22-830-801, REVISION 74.1 AND FOUND SATISFACTORY. FLAP OPS TEST CARRIED OUT IAW MM 27-50-00-860-801, REVISISDR SWAA2012120410214Roller · wornWEAR ON ROLLER LOC INTERNAL AREA OF FORE FLAP TRACK OF MIDFLAP O/B LEFT (6E/A). REPLACED ROLLER LOC INTERNAL AREA OF FORE FLAP TRACK OF MID FLAP O/B LEFT (6E/A) IAW SOPM 20-50-03 AND HARDWARESDR ERAA20120105Nut Plate · strippedFUNCTIONAL CHECK OF THE LEFT NR 1 FLAP TRACK FASTENERS FAILED TORQUE CHECK. ON FLAP SUPPORT TRACK P/N 85780039. FAILED AT THREE LOCATIONS.SDR CA121123006Skin · cracked(CAN) ON A ROUTINE PHASE ISNPECTION, A SMALL CRACK WAS FOUND COMING FROM THE RT FLAP INBD HANGER ON THE BOTTOM SIDE. WHEN HANGER WAS REMOVED IT REVEALED THE CRACK TO BE APPROXIMATELY 3" WITH 90 PERCENT HIDDEN UNDER HANGER BRACKET. WHEN SKIN WAS REMOVED TO RESDR SWAA2012112609860Rib · brokenRIGHT WING OUTBOARD T/E FLAP INBOARD DEFLECTION CONTROL ROLLER RIB UPPER ATTACH LUG FOR T/E PANEL BROKEN. REMOVED AND REPLACED RIGHT WING OUTBOARD T/E DEFLECTION CONTROL ROLLER RIB PER MM SEE SUBTASK SIGNOFFS AND PER TECHICAL SERVICE REQUEST #201205241.SDR SWAA2012112609855Rib · crackedLEFT WING 3 FLAP TRACK FAIRING CRACKED. REMOVED AND REPLACED RIB IAW SRM.SDR DALA1255050183Skin · delaminatedRT WING INBD MAIIN FLAP OTBD L/E AREA FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-05, PARA 5A, FIG 5.SDR DALA1255040183Skin · delaminatedLT WING INBD MAIN FLAP OTBD L/E AREA FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-53-01, REPAIR 1, FIG 201 AND SRM 51-70-05, PARA 5A, FIG 5, NRC 5105159.SDR DALA1255030183Skin · delaminatedRT WING OTBD T/E FLAP LWR SURFACE INBD T/E AREA FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-07, PARA 5A, FIG 9.SDR DALA1255020183Skin · delaminatedLT WING OTBD LOWER SURFACE AT OTBD T/E AREA FOUND DELAMINATED. PERFORMED PREPEG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-07, PARA 5A, FIG 9.SDR REXA2012112201520Skin · chafedRIGHT INBOARD FLAP VANE UPPER SKIN AT TRAILING EDGE AT FLAP STATION 99 AND 104 CHAFED. REPAIRED IAW SRM 57-52-00/51-12-00.SDR ASAA2012112093460Skin · chafedLEFT WING OTBD FORE FLAP OTBD L/E IS CHAFED ON A PREVIOUS REPAIR. REMOVED CHAFED DOUBLER AND INSTALLED NEW DOUBLER IAW SRM 51-40-02 AND 57-53-01, FIG 201.SDR ASAA2012112093459Skin · chafedLT WING INBD MIDFLAP INBD END UPPER SURFACE IS CHAFED. CHAFE FOUND TO BE 100 PERCENT OUT OF LIMITS IAW SRM 57 53 01. R & R SKIN IAW SRM 51-40-02.SDR ASAA2012112093457Skin · dentedLEFT WING OTBD FORE FLAP LWR SURFACE AT INBD END HAS A CREASE AND SEVERAL DENTS JUST OTBD OF A PREVIOUS REPAIR. REPAIRED SKIN DAMAGE IAW SRM 51-70-10, REPAIR 4 PG 201 PAINT T/U ON WO 1009234-500-0002, AP-16-28127, AP-17 ITEM 3.SDR SWAA2012112901004Skin · corrodedCORROSION ON LOWER L/E SKIN AT INBOARD T/E AFT FLAP RIGHT WING. PERFORMED REPAIR ON LOWER L/E SKIN LOC WBL 73+19" AT INBOARD T/E AFT FLAP RIGHT WING IAW SRM B737-300 57-53-01-2R-4 REPAIR 4, 51-40-02SDR ERAA20120104Flap · delaminatedDELAMINATION DAMAGE FOUND ON TRAILING EDGE FLAP ON LEFT WING P/N 85750233 AND P/N 85750245. TWO AREAS 1. 5.3" IN LENGTH 2. 7.1" IN LENGTH.SDR FDEA201211194084Hinge Bracket · damagedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND EXCEEDED LIMITS AFTER BUSHING REMOVED. REPAIRED PER EA 1-5750-75980 REVISION A PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194097Skin · looseLEFT WING INBD FLAP UPPER SURFACE RIVETS FOUND LOOSE. REPAIRED IAW SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163534, STEP 4, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194096Skin · looseRIGHT WING INBD FLAP UPPER SURFACE RIVETS FOUND LOOSE. REMOVED AND REPAIRED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211194095Hinge Bracket · scratchedLEFT WING INBD FLAP FORWARD HINGE BRACKET PIVOT BORE OTBD SPOT FACE FOUND SCRATCHED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-07, REVISION 74. REPAIR ACCOMPLISHED PER EA 1-5750-162397, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 1SDR FDEA201211194094Hinge Bracket · corrodedRIGHT WING INBD FLAP, FORWARD HINGE BRACKET PIVOT LUG BORE INBD AND OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-07 REVISION 74. REPAIR ACCOMPLISHED AS PER EA 1-5750-163542, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR FDEA201211194092Hinge Bracket · corrodedDURING BUSHING REMOVAL, LEFT WING INBD FLAP, AFT OTBD HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED BEYOND LIMITS. ACCOMPLISHED BUSHING REPAIR PER EA 1-5750-162394 PART 1. REPAIR CLASSIFIED A MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194085Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND EXCEEDED LIMIT AFTER BUSHING REMOVED. REPAIRED IAW EA 1-5750-75980 REVISION A PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211194082Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-10-6 REVISION 74. FOUND ACCEPTABLE IAW EA 1-5750-162398 PART 1. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 74. REPAIR CARRIED OUT PER ESDR FDEA201211194083Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER MOUNT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08 REVISION 74. REPAIRED IAW EA 1-5750-162398 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211194081Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 6, 9 AND 10. REPAIR CLASSIFIED AS MAJORSDR FDEA201211194080Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 6, 9 AND 10, . WASHER AT OUTBOARD HINSDR FDEA201211194079Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING LOWER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, AND 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION SDR FDEA201211194078Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING UPPER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, AND 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVSDR FDEA201211194077Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING LOWER BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 7, 9 AND 10. REPAIR CLASSIFIED AS MSDR FDEA201211194076Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING UPPER BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITD AS PER CMM 57-44-09 REVISION 74. . REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 7, 9 AND 10. REPAIR CLASSIFIED AS MASDR FDEA201211194075Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET LOWER MOUNT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44- 09 REVISION 74. . REPAIRED PER EA 1-5750-162400 PART 1, STEPS 1, 2, 3, 4, 5, 8, 9 AND 10. REPAIR CLASSIFIED AS MAJOR PERSDR FDEA201211194093Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING THICKNESS: 0.263", MATERIAL REMOVED: 0.078", REMAINING THICKNESS: 0.185", MINIMUM THICKNESS: 0.SDR SWAA2012121110499Fairing · crackedRIGHT WING 7 FAIRING 643BB CRACKED AT I/B AND O/B. REMOVED AND REPLACED FAIRING PER SOPM.SDR IPXA2176266Skin · dentedDENT IN LT WING TE FLAP LOWER SKIN, INBD FLAP REPAIRED IAW EO A300-5750-48554-B.SDR FDEA201211174062Bracket · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. EXISTING HOLE DIAMETER = 1.224 INCH, FINAL HOLE DIAMETER = 1.228 INCH, MAXIMUM HOLE DIAMETER = 1.220 INCH. RSDR FDEA201211174065Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 REVISION 74. REPAIRED PER EA 1-5750-163540 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211174064Hinge Bracket · corrodedLT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 REVISION 74. REPAIRED PER EA 1-5750-163540 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211174063Bracket · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. FOUND EXCEEDED LIMIT AS PER MD-11 CMM 57-44-09 REVISION 74. EXISTING HOLE DIAMETER = 1.223 INCH, FINAL HOLE DIAMETER = 1.226 INCH, MAXIMUM HOLE DIAMETER = 1.220 ISDR SWAA2012112609768Plate · crackedCRACK ON PLATE LOCATED MID FLAP AT LEVEL WBL 118 INTERNAL CAVITY LEFT WING. REMOVED AND REPLACED PLATE LOCATED MID FLAP AT LEVEL WBL 118 INTERNAL CAVITY LEFT WING IAW CMM 57-53-24.SDR FDEA201211164055Skin · misrepairedLT WING NR 2 SLAT INNER SKIN AT XIS 275 MISREPAIRED. REPAIRED PER SRM 57-40-01 FIGURE 201 REPAIR 1 REVISION 51 AND EA 1-5750-163553. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211164052Skin · misrepairedLT WING INBD FLAP UPPER SURFACE CENTER BOX BETWEEN XIFH 281 AND XIFH 288 MISREPAIRED. REPAIRED IAW SRM 57-00-01 FIGURE 201 SHEET 2 REPAIR 1 REVISION 51 AND EA 1-5750-163534 STEP 2 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
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