Boeing 727-22
Service difficulty reports · 1,282
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '72722' 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 aircraft_model_key = '72722' 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 DHL200070720CDoubler · crackedCORRUGATED DOUBLER CRACKED AT T/E AREA L/W SPAR LOWER SECTION APPROX WS 546.5 (I/B SECTION OF STATION). STOP DRILLED CRACK AT CORRUGATED STRAP AT FT WING REAR SPAR AT WS 546.5 PER SRM 51-10-1. PERFORMED HFEC INSP PER NDT MAN PART 6-51-00-00 FIG 4. NO CRACK SDR DHL200070715CSkin · crackedCABIN SERVICE DOOR HAS CRACK ON EXTERNAL SKIN ON UPPER HINGE PANEL. STOP DRILLED CRACK AT CABIN SERVICE DOOR ON UPPER HINGE AREA PER SRM 51-10-1.PERFORMED HFEC INSP PER NDT MAN 51-00-00 FIG 4, NO CRACK INDICATION NOTED. INSTALLED DOUBLER REPAIR AT CABIN SERVSDR DHL200070724CPlate · crackedMAIN CARGO DOOR CUT OUT SCUFF PLATE AND ADJACENT COVER WORN AND CRACKED AT FWD LOWER CORNER. SMOOTHED OUT SCUFF PLATE AT CARGO DOOR, FWD LOWER CUT OUT AS PER SRM 51-10-1. MATERIAL LOST .003 INCH, WITHIN LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED COVER PER SSDR DHL200070723CSkin · crackedLT HORIZ STAB L/E SKIN HAS A CRACK AT RIVET HEAD STA 47.3. PERFORMED HFEC INSP AND CONFIRMED CRACK PER NDT MAN 51-00-00 PART 6 FIG 4. CUT OUT DAMAGED AREA 2.5 X 1.75 INCH PER SRM 55-10-3. APPLIED ALODINE AND PRIMER PER SRM 51-10-2. INSTALLED REPAIR AT LT HSDR DHL200070707CFrame · crackedRT MAIN LANDING GEAR WING DOOR LOWER END FRAME IS CRACKED ON O/B BEND RADIUS AT FWD END. REMOVED CRACKED END FRAME AT RT MLG WING DOOR LWR END AS PER SRM 51-30-2. INSTALLED NEW END FRAME AT RT MLG WING DOOR LOWER END FWD SIDE PER SRM 51-30-2. TREATED AND PRSDR DHL200070706CSkin · corroded1808 CR JOINT HAS +10 PERCENT IND OF CORROSION BELOW S 2L FROM LBL 13 TO 14 AFT OF AFT FASTENER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF SKIN BS 1080 FROM STR 4L TO 4R AS PER S/B 727-53-0109. VISUAL INSP ACCOMPLISHED, NO FURTHER CORROSION NOTED.SDR DHL200070703CSkin · corroded1080 CIR JOINT HAS 2090 CORR LOSS FROM S-8R TO S10R AFT OF AFT FASTENER ROW. REMOVED FASTNERS AND CUT OUT DAMAGED SECTION OF AFT SKIN 13S 1080 FROM STR 10R TO STR 4R 59 .375 X 4.125 AS PER S/B 53-0109 R 4. VISUAL INSP ACCOMP FROM 10L STRINGER TO 10R STRINGERSDR DHL200070719CPanel · crackedNR 6 L/E SLAT ANTI-ICE TELOSCOPIC DUCT FAIRING PANEL CRACKED. REMOVED AND REPLACED ANTI ICE DUCT PANEL ON NR 6 L/E SLAT PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200070718CSkin · scratchedRT WING UPPER SKIN HAS DEEP SCRATCH AT WS 546.5 APPROX. CUT OUT DAMAGED AREA AT L/E RT WING UPPER SKIN AS PER 727 SRM 57-30-4 FIG 2, CUT DIMENSIONS 4 X 2 IN. INSTALLED FLUSH REPAIR AT RT WING L/E AS PER SRM 57-30-4 FIG 2. ALODINED AND PRIMED AS PER SRM 51-1SDR DHL200070716CAngle · chafedAFT CARGO COMPT FLOORBEAM SUPPORT ANGLE IS WORN (CHAFED) ON TOP BS 111073 ABOVE STR 29R. CUT OUT DAMAGED AREA AT CARGO SUPPORT ANGLE AT AFT CARGO COMPT SUPPORT ANGLE AT BS 1110 STR 29R. CUT OUT SIZE 3 X 1 IN AS PER SRM 51-40-3. INSTALLED ANGLE REPAIR AT CARSDR DHL200070710CRib · crackedTAIL CONE INTERIOR RIB CROSS SUPPORT ANGLE CRACKED. REMOVED FIBERGLASS RIB CROSS SUPPORT ANGLE AT TAIL CONE PER SRM 51-30-2. APPLIED FIBERGLASS CLOTH OVERLAY REPIAR TO INTERIOR RIB CROSS SUPPORT ANGLE PER SRM 51-40-8 FIG 1. INSTALLED RIB SUPPORT ANGLE PER SSDR DHL200070702CRivet · looseNR 1 ENG, LWR COWLING SHOWS 8 WORKING RIVETS AT LOWER MID AREA. CUT OUT DAMAGED AREA 13.5 IN X 2.5 IN PER SRM 54-10-3 FIG 5. CLEANED, ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PARTS PER SRM 54-10-3 FIG 5.SDR DHL200070721CSlat Track · crackedTHE NR 2 SLAT O/B TRACK TO SLAT ATTACH CLIP IS CRACKED ON THE I/B RADIUS. REPLACED ATTACH CLIP AT NR 2 SLAT O/B TRACK TO SLAT PER SRM 51-30-2.SDR DHL200070709CAngle · crackedLEFT W/W, VERT ANGLE BETWEEN BULKHEAD 870 AND KEEL BEAM HAS CRACK, FWD SIDE OF APU. VERIFIED CRACK PER NDT M/M PART 6-51-00 FIG 4. REMOVED VERT ANGLE PER SRM 51-30-2. INSTALLED NEW VERT ANGLE AT LEFT W/W PER SRM 53-10-2. ALODINED AND PRIMED PER SRM 51-10-2SDR DHL200070727CSkin · delaminatedLT HORIZONTAL STAB, ELEVATOR UPPER SURFACE, HAS SEVERAL AREAS DELAMINATED. OPENED ACCESS PANEL FOR EVALUATION. REMOVED LT HORIZONTAL STAB ELEVATER UPPER SKIN FROM STA 151.81 TO STA 188.65. INSTALLED PANEL SKIN.INSTALLED BALANCE PANEL SEALED PANEL REBALANCED ELSDR DHL200070713CSeat Track · wornSEAT TRACK LBL 24 HAS LOCK LUG WORN STA 850. REMOVED SEAT TRACK PER SRM 51-30-2. INSTALLED NEW SEAT TRACK FROM STA 850 TO 870 PER SRM 53-10-5. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200070712CSeat Track · wornSEAT TRACK AT LBL 45 HAS LOCK LUG WORN AT STA 860. REMOVED SEAT TRACK AT BS 860 LBL 45 PER SRM 51-30-2. INSTALLED SEAT TRACK SECTION PER M/M 53-4-0 AND SRM 51030-2. MATERIAL USED SEAT TRACK 91 IN 1778 T6 511. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200070722CFairing · tornNR 7 FLAP JACKSCREW FAIRING TORN AT I/B EDGE, UPPER SURFACE. CUT OUT DAMAGED AREA AT NR 7 JACKSCREW FAIRING I/B EDGE PER SRM 51-40-2. MATRL LOSS .5 INCH. INSTALLED EXTERNAL DOUBLER PER SRM 51-4-02 FIG 1. ALODINED AND PRIMED AREA PER 51-10-2.SDR DHL200070717CAngle · crackedAFT AIRSTAIRS, RT SIDE FS 1263, RBL 25 SUPPORT ANGLE ON FWD SIDE OF BULKHEAD UNDER UPPER FLOOR OF LOWER TORQUE BOX CRACKED UNDER WHERE AIRSTAIRS ACTUATOR MOUNTS. REMOVED WEB AT RT SIDE FS 1263 RBL 25 FOR ACCESS PER SRM 51-30-2. INSTALLED NEW ANGLE SUPPORT ATSDR DHL200070705CSkin · corroded1080 CR JOINT HAS 20 PERCENT IND OF CORROSION LOSS 5-10L AND 3 FASTENERS UP ALSO HAS 20 PERCENT IND. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF AFT SKIN BS 1080 FROM STA 10L TO 4L 59 .375 X 4 .125 AS PER S/B 53-0109 R4. VISUAL INSP COMPLIED WITH NO FURSDR 00FDEA00320Warning Light · illuminatedAFT T/O WITH FLAPS FULLY RETRACTED, NR 2 LEADING EDGE FLAP AND LEADING EDGE (AMBER) LIGHT ILLUM ON FWD PANEL.SDR DHL200070714CSkin · corroded1080 CIR JOINT HAS PLUS 10 PERCENT IND OF CORROSION LOSS FROM S-6R AFT OF FASTENER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF AFT SKIN STA 1080 FROM STR 10R TO 4R, 59 .375 X 4 .125 AS PER S/B 53-0109. VISUAL INSP COMPLETED FROM STA 10L TO 10R, NO SDR DHL200070701Indicator · contaminatedNR 2 ENG PARAMETERS FLUCUATING. CLEARED MOISTURE TRAP OF LARGE AMOUNT OF WATER. SERVICED FUEL CONTROL BELLOWS, RAN ENG AT CRUISE AND T/O POWER FOR EXTENDED PERIOD, OPS GOOD. REF LOG PG 179027 ITEM I P.SDR 00FDEA00208Skin · crackedDURING ROUTINE INSP, EXT FUSELAGE SKIN FOUND CRACK IN THE A ROW AT 9/32 FASTENER HOLE AT BS 440, STR 4L.SDR 00FDEA00181Switch · bentNR 5 LEAD EDGE FLAP SHOW INTRANSIT ABOUT 5 MIN AFT T/O. DID RED TABS, EXT TO 5 DEG AND BACK TO 0 AND LIGHT WENT OUT. REMOVED AND REPLACED MICRO SWITCH PER MM 27-81.SDR 00FDEA00183Channel · corrodedAFT BAG BIN FLOOR SUPPORT CHANNEL CORRODED BEYOND ALLOWED LIMITS, ON LWR SURFACE, AT FASTENER HOLES BENEATH RT FLOOR TRACK BS 960. *S/D* REMOVED ANGLE, FAB AND INSTALLED NEW ANGLE IAW SRM 51-20-1 & 51-30-2.SDR 00FDEA00174Attach Fitting · corrodedDURING ROUTINE INSP, THE LEFT O/B AILERON, I/B ATTACH FITTING WAS FOUND TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED PER IAW MM 27-10-031-2.SDR 00FDEA00173Attach Fitting · corrodedDURING ROUTINE INSP, RIGHT O/B AILERON, I/B ATTACH FITTING WAS FOUND TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED PER IAW MM 27-10-031-2.SDR 00FDEA00172Web · crackedDURING ROUTINE INSP, WEB INSIDE VERTICAL STABILIZER AT FIN STA 110.4 FOUND CRACKED. REPAIRED IAW SRM 53-10-9 FIG 4.SDR 00FDEA00182Skin · crackedDURING ROUTINE INSP, FUSELAGE SKIN FOUND CRACKED AT LAP JOINT, STR 20L, BS 1185. *S/D* FAB FILLER, DOUBLER AND INSTALLED IAW SRM 53-30-3 FIG 3A.SDR CA000322003Floorbeam · corroded(CAN) INTERGRANUALLER CORROSSION ON LOWER CAP OF FLOORBEAMS AT STN 500, 540, 600, 1050 AND 1110. REPAIRED.SDR 00FDEA00144Frame · corrodedNR 833, WHILE WORKING NR-0525 FOUND CORROSION ON AFT CARGO DOOR FRAME FWD FRAME WEB STR 26 RT AREA MARKED.SDR 00FDEA00138Clamp · looseNR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. RETIGHTEN CLAMP IN THE PNEU DUCT PER MM 36-00-002-4 CK. LEAK CHECK GOOD, OK TO CONTINUE.SDR 00FDEA00119Skin · corrodedNR 112 SKIN BULGING AT LOWER NOSE CHORD BS 328, RBL 20, JUST ABOVE NOSE GEAR STRUT DOOR CUTOUT (C53-100-01). REPAIRED PER FEDEX EA 7-5330-50011.SDR CA000301017Switch · failed(CAN) NR 4 KRUGER FLAP EXTENDED GREEN LIGHT ON SHORTLY AFTER TRAILING EDGE FLAPS WERE RETRACTED. DUMPED FUEL AND RETURNED. NR 4 KRUGER FLAP EXTEND/RETRACT SWITCH AT FAULT, REPLACED A/C GROUNG CHECK SERVICEABLE.SDR 00FDEA00090Frame · corrodedWHILE WORKING NR 112 FOUND CORROSION ON NOSE CHORD AT BS 343, RBL 20, WL 149.SDR 00FDEA00089Web · corrodedNR 693 CORROSION (C57-571-01-01) ON L/W FRONT SPAR WEB AT FUEL CELL PANEL CUT OUT 7340, FWD AND AFT WEB SURFACE WS 182. REMOVED AND REPLACED CORROSION PER FEDEX SRM 57-10-1, AND IAW FEDEX EA 7-5710-47901, FUEL LEAK CK IAW FEDEX MM 28-11-000-8 DTEP 7C.SDR 00FDEA00082Frame · corrodedNR 113 - CORROSION AT INNER CHORD BS 292, RBL22, WL 154, AS SEEN THROUGH LIGHTENING HOLE INSIDE NOSE WW (C53-100-01).SDR DHL2000707005Stringer · dentedAIRCRAFT DAMAGED BY OBJECT STRIKING AIRCRAFT IN HIGH WINDS AT STA 520, STRINGER BENT AT S-20. DENT 5 BY 3 PREVIOUS REPAIR IN THAT AREA. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER ARM 53-10-3.SDR 00FDEA00077Strap · bentWHILE WORKING NRC-805 (FUSELAGE 194) FOUND STABILIZER STRAP BS 1030-1130, STR 27R TO BE BENT AND HAS DOUBLE HOLES. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-30-2, 53-10-1.SDR 00FDEA00076Web · gougedWHILE WORKING NR 805 (FUSELAGE 194) FOUND VERTICAL WEB TO BE GOUGED IN SEVERAL LOCATIONS BS 1057-1110, STR 27 RT. *S/D* REMOVED AND REPLACED, ALODINED, PRIMED AND PAINTED IAW FEDEX MM 51-20-151.SDR 00FDEA00073Switch · out of adjustAFT GEAR RETRACTION, LMG DOOR RED AND AMBER LIGHT DID NOT EXTINGUISH. RECYCLED THE GEAR AND LIGHT EXT IND ALL GEAR DOOR UP. ADJUSTED LANDING GEAR DOOR SWITCH PER 727-100 MM 32-62-011-4. OPER CK NORM.SDR 00FDEA00063Frame · corrodedWHILE WORKING NR 113, FOUND SHEAR TIE AT BS 320, RBL 18-21, WL 151 TO BE CORRODED. *S/D* REPAIRED IAW FEDEX SRM 53-10-4 FIG 15.SDR 00FDEA00062Frame · corrodedWHILE WORKING NR 112 FOUND HORIZONTAL CHORD CORRODED BS 348, WL 168, RBL 16. *S/D* REMOVED AND REPLACED CHORD PER IAW FEDEX SRM 51-30-2.SDR 00FDEA00061Skin · corrodedCORROSION AND FASTENERS PULLED THRU OUTER SKIN AT BOTTOM SIDE OF CARGO CUTOUT BS 1065 - 1090, STR 26R. *S/D* REPAIRED AFT CARGO DOOR PER FEDEX EA 7-5330-50016.SDR 00FDEA00040Shear Tie · corrodedWHILE WORKING NR 0113, FOUND SHEAR TIE AT BS 344, RBL 21-24, WL 151 TO BE CORRODED. *S/D* REPAIRED IAW FEDEX SRM 53-10-4, FIG 11.SDR 00FDEA00039Frame · gougedMAIN CARGO DOOR REPAIR DOUBLER ON LWR AFT SIDE FRAME WAS GOUGED. *S/D* REMOVED AND REPLACED ALODINED, PRIMED AND INSTALLED PER FEDEX SRM 51-10-2, 51-30-8, 51-20-1, 51-10-3.SDR 00FDEA00034Frame · crackedCRACKED FRAME BS 1050 BETWEEN STR 26 RT & 27 RT. *S/D* REMOVED AND REPLACED PER FEDEX EA 7-5310-47886.SDR 00FDEA00033Skin · crackedNR 805 - CORROSION AND FASTENERS PULLED THROUGH OUTER SKIN, BOTTOM SIDE OF CARGO DOOR CUT-OUT BS 1065-1090, STR 26R.SDR 00FDEA00035Bulkhead · damagedWHILE WORKING 71C101-02, FOUND STRUCTURAL DAMAGE AT BS 227.8, LBL 12, WL 163 ON PRESSURE BULKHEAD. *S/D* REMOVED AND REPLACED PER SRM 51-40-2 FIG 1.
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