Boeing 747-48EF
Service difficulty reports · 267
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 = '74748EF' 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 = '74748EF' 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 UIEA2026071300597None · noneUNABLE TO CARRY OUT LFEC PER WORK CARD 53-F64K-00-01 ON LTH DRAIN MAST CUTOUT UNDER FAIRINGS STD 42L TO 43L AT BS 870 DUE TO NO DOUBLER INSTALLED. ONLY TWO DRAIN MASTS INSTALLED (DIFFERENT FROM THE WORK CARD). PERFORMED HFEC SCAN PER 747 NDT MANUAL D6-7170, SDR UIEA2026072000632Rivet · shearedQTY 01 DENT MARK AND QTY 01 SHEARED RIVET FOUND ON FUSELAGE SKIN FWD OF STA 2598, S26-38R, JACK PAD AREA. SHEARED RIVET ON FUSELAGE SKIN ON FWD OF STA 2598 BETWEEN S-26R AND S-38R EVALUATED AND FOUND STRUCTURALLY ACCEPTABLE TO LEAVE THE DENT AS-IS ALONG WITH SDR UIEA2026072200636Beam · damagedWHILE ACCOMPLISHING SB747-53A2562 R3, FOUND EXISTING PANEL HOLE TOO CLOSE TO NEW BEAM (05EA) AT STA 340. FASTENER INTERFERENCE CONDITIONS WITH HORIZONTAL STIFFENERS ON LHS NOSE WHEEL WELL AT STA 340, WL 130 - WL 170 RECTIFIED WITH THE HORIZONTAL STIFFENER FLASDR UIEA2026072300639Tension Tie · crackedDURING HFEC OPEN HOLE INSPECTION ON LHS STA 920 TENSION TIE AND FRAME, FOUND 01EA FASTENER HOLE ON AFT CHANNEL WITH CRACK. CRACKED TENSION TIE AFT CHANNEL ON LHS STA 920 TRIMMED OUT AND SPLICE REPAIR CARRIED OUT IAW SRM 53-20-30-2R-1, REPAIR 1, FIGURE 201, BSSDR UIEA2026081100742Panel · damagedWHILE ACCOMPLISHING SB747-53A2562 R3 AT STA 340, FOUND R/H PANEL FASTENER HOLES TOO CLOSE TO NEW BEAMS (02 EA) P/N: 141U1193-29 (WL130) AND P/N: 141U1193-27 (WL150)(<P>R/H PANEL NEW BEAMS (02 EA) P/N: 141U1193-29 (WL130) AND P/N: 141U1193-27 (WL150) REPAIRED ASDR UIEA2026081200743Tee Fitting · crackedLOWER FUSELAGE: STA 250 TO STA 260 FWD BULKHEAD R/H SIDE T-CHORD FOUND CRACKED.(<P >AT R/H NOSE W/W FWD BULKHEAD STA 250 TO STA 260, CRACKED T-CHORD REMOVED AND INSTALLED WITH NEW FABRICATED T-CHORD AS PER EN 3565-26 REV.0. REPAIR CLASSIFIED AS "MAJOR" REPAIR SDR UIEA2026081200744Structure · abnormalWHILE ACCOMPLISHING SB747-53A2562 R3, AT STA 260 WL 20 L/H, FOUND EXISTING HOLE SIZE 04 EA DEVIATED FROM DRAWING: 141U1192. EXISTING HOLE SIZE = 3/16, DWG HOLE = 1/4; FOUND SHORT EDGE MARGIN. FITTING COMMON TO SEAT TRACK AND CHORD P/N: 65B11784U507.(<P >L/H ANSDR UIEA2026081200745Structure · abnormalWHILE ACCOMPLISHING SB747-53A2562 R3, AT STA 260 WL 20 RH, FOUND EXISTING HOLE SIZE 04 EA DEVIATED FROM DRAWING 141U1192. EXISTING HOLE SIZE = 3/16, DWG HOLE = 1/4; FOUND SHORT EDGE MARGIN- FITTING COMMON TO SEAT TRACK AND CHORD P/N: 65B11784U508.(<P >R/H ANGLSDR UIEA2026081900778Angle · crackedWHILE C/O DVI INSPECTION PER SB 747-53A2562 R3 STEP 22, FOUND UPPER INNER SIDE ANGLE 65B07941-544 FOUND CRACKED AT NOSE W/W RT TOP PANEL BS 260 - 340, RBL 30. >NOSE W/W R/H UPPER INNER NEW SIDE ANGLE TOP PANEL STA 260 - STA 340 RBL 30 (05 EA) FASTENER HOLES ESDR UIEA2026081900781Tee Fitting · crackedLOWER FUSELAGE, BS 250 - 260, FWD BULKHEAD LT SIDE TEE FITTING FOUND CRACKED. A NEW TEE FITTING FABRICATED IAW EN 3564-26 REV. 0. R & R IAW SRM 51-40-02-0G-0, REV 107.SDR UIEA2026082400792Doubler · crackedSUSPECTED CRACK ON MED L1 DOOR UPPER HINGE CUTOUT DOUBLER EDGE. DOUBLER FOR MED L1 DOOR UPPER HINGE CUTOUT, REMOVED AND A NEW DOUBLER FABRICATED & INSTALLED IAW EN 3413-26, REV 0.SDR UIEA2026082500794Stiffener · abnormalWHILE ACCOMPLISHING SB747-53A2562 R3 AT BS 280, RBL 20, TWO EXISTING FASTENER HOLES DEVIATED FROM THE DRAWING. EXISTING HOLE SIZE = 1/4", STIFFENER, INCOMING OVERSIZED FASTENER HOLE CONDITION COMMON TO STIFFENER WAS REPAIRED IAW EN 3594-26, REV 0. REPAIR CLASSDR UIEA2026083100828Seat Track · crackedFOUND A CRACK ON MAIN DECK SEAT TRACK, BS 260, RBL 33. THE SEAT TRACK WAS TRIMMED OFF, & A SEAT TRACK SPLICE REPAIR CARRIED OUT IAW EN 3583-26, REV 0. REPAIR CLASSIFIED AS A MAJOR REPAIR & CATEGORIZED AS A CATEGORY A PERMANENT REPAIR.SDR UIEA2026083100829Seat Track · crackedFOUND CRACK ON MAIN DECK SEAT TRACK, BS 260, LBL 33, IN FRONT OF NOSE WHEEL WELL BULKHEAD AREA. THE SEAT TRACK WAS TRIMMED OFF, & SEAT TRACK SPLICE REPAIR CARRIED OUT IAW EN 3583-26, REV 0. REPAIR CLASSIFIED AS "MAJOR" REPAIR AND CATEGORIZED AS "CATEGORY A" PSDR UIEA2026091700881Door Frame · crackedMAIN DECK L5 DOOR CUTOUT AREA AT BS 2220, STRINGER 18L FOUND CRACKED. L5 DOOR CUTOUT AREA REPAIRED IAW EN 3574-26, REV 0, & SRM 53-00-03-2R-1, REPAIR 1, REV 107.SDR UIEA2026092000887Door Frame · crackedDURING HFEC INSPECTION ON DOOR STOP SUPPORT FITTINGS AT S16L, BS 2231, FOUND ONE LOWEST FWD HOLE WITH A CRACK INDICATION AT STRAP SIDE 3 & 9 O'CLOCK POSITION LOOKING OTBD. CRACK ON BS 2231 S16L. FRAME STRAP TRIMMED OUT & REPAIR CARRIED OUT IAW EN 3430-26, RESDR UIEA2026092100889Doubler · no discrepancySECT 41 LAP JOINT INSP: EXISTING DOUBLERS (06 EA) ON S-14L STA 140-160, S-44L STA 240-260, S-44R STA 240-260, S39R STA 380-420, S45L STA 400-420 AND S45R STA 400-420 FOUND THE REPAIR NOT CONFIRMED TO SRM 53-00-01, REPAIR 10, 12 OR 16(<P >DOUBLERS AT STA 240 - SDR UIEA2026092800919Spar · damagedNR 3 PYLON UPPER SPAR WEB SKIN SUSPECT CRACK AT NAC STA 300. CRACKED NR 3 PYLON UPPER SPAR WEB SKIN R & R IAW SRM 51-40-02-0G-0 REV. 107, DWG. 311U2130. SHT. 6, REV. B; REPAIR CARRIED OUT IAW EN 3684-26, REV. 0. REPAIR CLASSIFIED AS "MAJOR" CATEGORIZED AS "CASDR UIEA2026093000925Spar · damagedDURING NDT LFEC INSPECTION ON LHW REAR SPAR LOWER CHORD AND SKIN AT LANDING GEAR BEAM ATTACHMENT FITTINGS AND TRUNNION FITTINGS (SSID), FOUND 02 EA FASTENERS AT WS 469.8. TRUNNION FITTING SHEAR CLIP AREA LARGER THAN NORMAL(<P >02 FASTENERS ON LHW REAR SPAR LOWSDR UIEA2026093000926Spar · damagedDURING NDT LFEC INSPECTION ON RHW REAR SPAR LOWER AND SKIN AT LANDING GEAR BEAM ATTACHMENT FITTINGS AND TRUNNION FITTINGS (SSID0), FOUND 02 EA FASTENERS AT WS 469.8. TRUNNION FITTING SHEAR CLIP AREA LARGER THAN NORMAL TWO FASTENERS ON RT W REAR SPAR LOWER CHORSDR UIEA2026093000927Frame · damagedPER DWG 624U0072 SHEET 13, 08 FASTENERS ARE SHOWN BETWEEN STR-7 AND STR-8, BUT AT STA 2598 BLKHD HORIZONTAL STABILIZER FWD SIDE, ONLY 04 EA FASTENERS ARE INSTALLED PER SIDE OF BOTH LHS AND RHS FRAME . REWORK CARRIED OUT AT STA 2598 BULKHEAD HORIZONTAL STABILISDR UIEA2026093000929Frame · damagedUNABLE TO PERFORM HFEC INSPECTION FULLY AROUND 04 EA FASTENERS AND 01 EDGE PER SB747-53A2837 PART 7 R0 STEP 1 & 2 OF FIGURE 42 AND DWG 624U0072 SHEET 13 AT LHS STA 2598 BLKHD FWD AND AFT FRAME OUTER CHORD. REWORKS CARRIED OUT AT THE LT STA 2598 BULKHEAD FWD ASDR UIEA2026093000930Frame · damagedUNABLE TO PERFORM HFEC INSPECTION FULLY AROUND 06 EA FASTENERS AND 01 EDGE PER SB747-53A2837 PART 8 R0 STEP 1 & 2 OF FIGURE 42 AND DWG 624U0072 SHEET 13 AT RHS STA 2598 BLKHD FWD AND AFT FRAME OUTER CHORD. REWORK CARRIED OUT AT RHS STA 2598 BULKHEAD FWD AND ASDR UIEA2026093000933Door Sill · corrodedAFT CARGO DOOR LOWER SILL FOUND CORRODED. CORRODED DOOR SILL ON AFT CARGO DOOR AREA REMOVED AND REPLACED, AND REPAIR CARRIED OUT AS PER SRM 51-40-2-0G-0 REV. 107 AND EN 3557-26, REV. 0. REPAIR CLASSIFIED AS "MAJOR" AND CATEGORIZED AS "CATEGORY A" PERMANENT RESDR UIEA2026100300940Door Frame · crackedDURING HFEC INSPECTION ON LOWER LOBE AFT CARGO DOOR CUTOUT FORWARD UPPER CORNERS, FOUND CRACK APPROX 0.3" IN LENGTH AS MARKED(<P>DOUBLER REPAIR CARRIED OUT ON THE LOWER LOBE AFT CARGO DOOR CUTOUT FWD UPPER CORNER CRACKED AREA AS PER SRM 53-60-01-2R-3 REPAIR 3,SDR UIEA2026100300941Frame · crackedDURING HFEC OPEN HOLE INSPECTION ON RHS STA 940 TENSION TIE AND FRAME, FOUND 02 EA FASTENER HOLE ON FRAME AND CHORD WITH CRACK(<P >FRAME SPLICE REPAIR CARRIED OUT ON RHS STA 940 TENSION TIE AND FRAME CRACK 02 FASTENER HOLES AREAS AS PER SRM 53-20-07-2R-8 FIGURSDR UIEA2026100500952Doubler · misinstalledSEC 42 LAP JOINT INSP OF EXISTING DOUBLERS (02 EA) ON S39L, STA 940-960 AND S39R, STA 920-960; FOUND THE REPAIR NOT CONFIRMED TO SRM 53-00-01, REPAIR 10,12 OR 16. BODY FAIRING PANEL REMOVED & REINSTALLED IAW AMM 53-51-01-004-001, REV 117 & AMM 53-51-01-404-00SDR UIEA2026100600964Doubler · misinstalledSECT 46 LAP JOINT INSP OF EXISITNG DOUBLERS (05 EA), STRINGER 14L, BS 1980-2020, S12L, BS 1720-1740, S12L, STA 2140-2160, S34L, STA 1640-1960 AND S40L, STA 1640-1820; FOUND THE REPAIR NOT CONFORMED TO SRM 53-00-01, REPAIR 10, 12 OR 16. REPAIRED IAW EN 3737-SDR UIEA2026100600965Tension Tie · crackedDURING HFEC OPEN HOLE INSPECTION ON LHS STA 920 TENSION TIE AND FRAME, FOUND 01 EA FASTENER HOLE ON AFT CHANNEL WITH CRACK. TENSION TIE AFT CHANNEL TRIMMED OUT AND SPLICE REPAIR CARRIED OUT IAW SRM 53-20-30-2R-1, REPAIR 1, FIGURE 201, REV. 107. REPAIR CLASSIFSDR UIEA2026100700966Support Frame · damagedHFEC OPEN HOLE INSPECTION CARRIED OUT ON 02 EA FASTENER HOLES AT STA 2598 BLKHD FRAME SUPPORT STA 2598 BELOW S-11L AND FOUND 02 EA HOLES DAMAGED ON THE 2ND LAYER, VIEW I/B AND FITTING HOLES. DAMAGED AREAS ON BS 2598 BULKHEAD FRAME SUPPORT AREAS REPAIRED IAW ESDR UIEA2026011200009Wire · shortedNUMBER 4 ENGINE FIRE INDICATION ON ENG SHUTDOWN. PERFORMED ENG FIRE ON GROUND QRH.DISCHARGED BTH FIRE BOTTLES PER QRH INDICATION EXTINGUISHED AFTER SECOND BOTTLE. C/W FIM 26-11 TASK 808, NO FIRE CONDITION, FOUND T5683 LP A SHORT TO GROUND AND LOOP B BROKEN WSDR UIEA2025103001286Stringer · crackedPERFORMED EO 4453C398, CRACK FOUND AT S-23R NEAR STA 1460 DURING HFEC INSPECTION (1 EA)(<P>REPAIRED CRACK AT S-23R NEAR STA 1460 PER EO 4453C398. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025103001287Stringer · crackedPERFORMED EO 4453C398, CRACK FOUND AT S-23L NEAR STA 1460 DURING HFEC INSPECTION (3EA). REPAIRED CRACK AT S-23L NEAR STA 1460 PER EO 4453C398. NO FURTHER DEFECTS NOTED.SDR GTIA202508040001Tire · failedDURING TAKEOFF A TIRE BLEW OFF, A/C CONSEQUENTLY ABORTED TAKEOFF. A/C STAYED ON GROUND FOR LONG REPAIRS.SDR UIEA2025032600390Actuator · faultedPACK 2 EICAS (PACK 3 ALREADY DEFERRED).(<P>(ITEM 1 LP 1996448) - R & R PACK 2 RAM AIR EXIT DOOR ACTUATOR AND PERFORMED A&B GROUND TESTS, TESTS OKAY PER AMM 21-62-05/401. (ITEM 6 LP 1996449) ACCOMPLISHED DISTANCE CHECK ACTUATOR AND LIMIT SWITCH WITHIN RANGE PERSDR UIEA2024121901174Start Valve · malfunctioned1. STARTER CUTOUT 2 EICAS AT CRUISE W/ ENG 2 START VLV STATUS MSG 2. ENG #4 N1 COMMAND BAR FLUCTUATING(<P>T/S AND PERFORMED WIRING CHK BTWN #2 STARTER VALVE & EEC THEN HARNESS CHKS NORMAL. FOUND #2 STARTER VALVE NOT FULLY CLOSED. REMOVED & REPLACED #2 SSDR UIEA2024101100974Seat Track · damagedBROKEN DAMAGE ON THE MAIN DECK SEAT TRACK NEAR STA 1720 RBL 98.58.(<P>1. PERFORMED EI T2024A53M-2422 REV=0. 2. ACCOMPLISH WORK SHEET NO: 40816 (SRM 53-00-52-2R-6 REV=101) AND EI T2024A53M-2422 REV=1. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100975Skin · chafedCHAFING - PNL, L/H WING INBD AILERON OUTBD LOWER SIDE.(<P>1. PERFORM REPAIR L/H WING INBD AILERON OUTBD LOWER SIDE PANEL CHAFING. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATISFACTORY IAW SRM 51-70-06-SDR UIEA2024101100976Longeron Fitting · crackedCRACK DAMAGE IN HOLE #11 OF LONGERON EXTENSION FITTING DURING PERORMING SB 747-53A2390 AT STA 1480 RH SIDE.(<P>1. ACCOMPLISHED EL T2024A53M-2366 REV=0. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100977Skin Splice · crackedCRACK DAMAGE ON THE HST OUTBOARD SECTION RH SIDE DURING INSPECTION PER SB 747-55A2050.(<P>1. REMOVE FASTENERS I.A.W SRM 51-40-02-0G-0 REV.101. 2. REPAIR DAMAGE AREA I.A.W EL T2024A55M-2240 REV.4. 3. INSTALL SPLICE I.A.W DWG 65B03560 SH14 REV.D AND 65B03621 SH6SDR UIEA2024101100978Stringer · noneREPAIR-EXISTING REPAIR ON STRINGER S-39R BETWEEN STA 400 AND STA 420.(<P>1. ACCOMPLISH EL T2024A53M-2334 REV.2. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100979Stringer · noneREPAIR-EXISTING REPAIR ON STRINGER S-39R BETWEEN STA 360 AND STA 400.(<P>1. ACCOMPLISH EL NO. T2024A53M-2253 REV.2. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100980Stringer · noneREPAIR-EXISTING REPAIR ON STRINGER S-40R BETWEEN STA 380 AND STA 400.(<P>1. ACCOMPLISH EL T2024A53M-2254 REV.1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100981Stringer · noneREPAIR-EXISTING REPAIR ON STRINGER S-38R BETWEEN STA 360 AND STA 400.(<P>1. ACCOMPLISH EL NO. T2024A53M-2166 REV.3. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100982Fitting · crackedCRACK- FITTING, LOWER SIDE OF R/H WING #8 SPOILER MID LOWER SUPPORT FITTING, OUTBD SIDE.(<P>1. REPAIRED DAMAGE AREA I.A.W W/S #40727 (SRM 57-51-13-2R-1 REV.101). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100983Bracket · corrodedCORROSION - BRACKET, WING TO BODY FAIRING INTERNAL PNL SUPPORT STUCTURE STA 921. LBL 1.(<P>1. REMOTE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV=101. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV=101 AND BOEING DWG #65B06704, SH2 REV=F AND NO: 65B04118 SH6 REV=A. SDR UIEA2024101100984Support Angle · corrodedCORROSION-ANGLE WING TO BODY FAIRING INTERNAL PNL SUPPORT STRUCTURE STA 894 LBL 5.(<P>1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G-0 REV.101. 2. INSTALL NEW PART I.AW SRM 51-40-02-0G-0 REV.101 AND DWG #65B06714 SH3 REV.F, 65B06714 SH5 REV.A. 3. JOB COMPLETED ASDR UIEA2024101100985Support Angle · corrodedCORROSION-ANGLE WING TO BODY FAIRING INTERNAL PNL SUPPORT STRUCTURE STA 930 LBL 4.(<P>1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G-0 REV.101. 2. FABRICATED PART I.A.W W/S #40804. 3. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV=101 AND DWG #65B06712 SH3 REV=G & SSDR UIEA2024101100986Battery · inoperativeFOUND EMERGENCY LIGHT INOP IN MAIN DECK AND L1 ENTRY DOOR AREA.(<P>I.A.W AMM 33-51-04-902-001-001 REV 110 REPLACED M5170 BATTERY ASSY AND PERFORMED PWER SUPPLY TEST. THE RESULT WAS SATISFACTORY.</P>)SDR UIEA2023123001048Cable · unknownAIR TURN BACK. CAPTAIN'S LOCALIZER INOP, RIGHT HAND ILS ON DEFFERAL(<P>REMOVED & REPLACED RIGHT HAND ILS COAX CABLE AND CONNECTIONS PER SWPM 20-51-05 & OPS TEST OK PER AMM 34-31-00/501. AUTOLAND UNIQUE GROUND TEST PASSED PER AMM 22-10-00/501. CLEARED DMI 19994
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