# Service difficulty reports: N29124

A list on [N29124](https://openairdocs.org/aircraft/N29124.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 87 reports

- [SDR CALA2026100920257](https://openairdocs.org/sdr/CALA2026100920257.md): Cover · damaged · Oct 1, 2026 · N29124 · Boeing 757224 · Escape Slide
  > FA REPORTS L4 DOOR SLIDE COVER DAMAGED. SLIDE BUSTLE TAPE INTERIM REPAIR, PERFORMED INSPECTION ON INTERIM REPAIR IN REF WITH ECRA 2560-03395 PART 2, NO FURTHER DISCREPANCIES FOUND AND REPAIR STILL INTACT. REMOVED AND REPLACED 4L DOOR SLIDE COVER IAW AMM 2
- [SDR CALA2026080618335](https://openairdocs.org/sdr/CALA2026080618335.md): Unknown · smoke · Aug 3, 2026 · N29124 · Boeing 757224 · Air Distribution System
  > WILL NEED TO ACCOMPLISH THE SMOKE AND ODOR CONDITIONAL INSPECTION PER CREW REPORT PERFORMED SMOKE/ODOR IN THE FLIGHT DECK AND/OR CABIN CONDITIONAL INSPECTION TASK 05-51-58-910-801-C1. UP TO AND INCLUDING STEPS 1.C.2.I. COMPLETED SMOKE/ODOR IN THE FLIGHT DECK A
- [SDR CALA2026080518329](https://openairdocs.org/sdr/CALA2026080518329.md): Oven · faulty · Aug 3, 2026 · N29124 · Boeing 757224 · Buffet/Galleys
  > OVEN 205 HAS A SMOKE ODOR, OVEN DEACTIVATED, CIRCUIT BREAKER OPEN, & COLLARD. OVEN PLACARDED. REMOVED AND REPLACED THE OVEN IAW AMM 25-34-00-400-801-C3. OPS CHKD NORMAL.
- [SDR CALA2026080518327](https://openairdocs.org/sdr/CALA2026080518327.md): Oven · faulted · Aug 3, 2026 · N29124 · Boeing 757224 · Buffet/Galleys
  > GALLEY OVEN 305 HAS AN ELECTRICAL ODOR, OVEN DEACTIVATED, CIRCUIT BREAKER OPEN & COLLARD. OVEN PLACARDED. R & R THE OVEN IAW AMM 25-34-00-400-801-C3. OPS CHECKED GOOD.
- [SDR CALA2026080318234](https://openairdocs.org/sdr/CALA2026080318234.md): Unknown · odor · Jul 31, 2026 · N29124 · Boeing 757224 · Air Distribution System
  > LAVATORY SMOKE EICAS MESSAGE. FA REPORTS BOTH AFT LAV SMOKE ALARM ACTIVATED. MID CABIN ELECTRICAL SMOKE ODOR REPORTED ALSO. PERFORMED FIM TASK 26-14 FAULT TREE 806. SYS TEST OK FOR ALL LAV SMOKE DETECTION SYSTEMS. PERFORMED SMOKE DETECTION SELF TEST IN ALL LAV
- [SDR CALA2026061517115](https://openairdocs.org/sdr/CALA2026061517115.md): Trim Panel · loose · Jun 10, 2026 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > OVERHEAD BIN TRIM AT SEATS 35C AND 36C FELL DOWN. TRIM COULD NOT BE REMOVED DUE TO EMERGENCY LIGHT ATTACHED TO IT. FA REINSTALLED TRIM TEMPORARILY WITH LAV INOP STICKER. SECURELY INSTALLED OVERHEAD CABIN TRIM AT SEAT ROWS 35C & 35C. OPS CHECKED EMERGENCY LIGH
- [SDR CALA2025082908266](https://openairdocs.org/sdr/CALA2025082908266.md): Union · leaking · Aug 28, 2025 · N29124 · Boeing 757224 · Turbine Engine Oil System
  > R ENG OIL LEAK, REF LP 6069024 FOUND PRIMER ADAPTER/UNION ON PRESSURE OIL FILTER HOUSING, IPC 79-21-04-01, ITEM 60 LOOSE, HELD ON WIRELOCKING. PRIMER REMOVED CLEANED AND RETORQUED WITH REF TO AMM 79-21-07-434-007-R00. GROUND IDLE ENGINE RUN COMPLETED, NO LEAKS
- [SDR CALA2025062605927](https://openairdocs.org/sdr/CALA2025062605927.md): Inspection · none · Jun 20, 2025 · N29124 · Boeing 757224 · Standard Practices/Structures
  > ACCOMPLISH AN NDT INSPECTION OF THE BEAR STRAP AND INNER CHORD, IN THE AREA OF THE REPAIR (INSTALLED PER EA 5330-04213 OP 2), BEFORE 50,000 TOTAL AIRCRAFT CYCLES. AFTER THE ACCUMULATION OF 46,500 TOTAL AIRCRAFT FLIGHT CYCLES, BUT BEFORE 47,000 TOTAL AIRCRAFT F
- [SDR CALA2025061905716](https://openairdocs.org/sdr/CALA2025061905716.md): Skin · dented · Jun 17, 2025 · N29124 · Boeing 757224 · Fuselage Main, Plate/Skin
  > DENT ON FUSE. STA 625 (APPROX) HAS NEW DIA M. THAN RECORDED ON INCOMMING DMG. REPAIRED FUSE.SKIN STA 610-635 PER UAL EC/RA II 5330-07543 AND V TMAE EA 757-5330-13-A3952 REV- FAA 8100-9 ATTACHED. RII VERIFIED.
- [SDR CALA2025061805676](https://openairdocs.org/sdr/CALA2025061805676.md): Plate · corroded · Jun 17, 2025 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > STA 1680 R/H SIDE AT FLOOR ABOVE ACCELOROMETOR (M10735) IS CORRODED AND PLATE MISSING. WORK ACCOMPLISHED PER EC/RA 5360-01966 AND VTMAE 757-5360-13-A39 59 REV-.
- [SDR CALA2025061805675](https://openairdocs.org/sdr/CALA2025061805675.md): Skin · corroded · Jun 17, 2025 · N29124 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING WINGLET ADAPTER PLUG T/E TOP SKIN INBD AREA WITH CORROSION. REPAIR ACCOMPLISHED PER EC/RA 5730-03596 AND VTMAE EA 5753-13-A3 935 REV - LP: 5221586
- [SDR CALA2025061605575](https://openairdocs.org/sdr/CALA2025061605575.md): Tee Angle · corroded · Jun 15, 2025 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > RIGHT LOWER WING TO BODY TEE ANGLE HAS CORROSION UNDER PANEL 139AL KEELBEAM AREA. REMOVED AND REPLACED T- ANGLE AND SPLICE ANGLE AT RT LOWER WING TO BODY IAW SRM 51-40-02. REF L/P 5208429.
- [SDR CALA2025062605926](https://openairdocs.org/sdr/CALA2025062605926.md): Frame · dented · Jun 13, 2025 · N29124 · Boeing 757224 · Fuselage Main, Frame
  > FWD CARGO COMP. STA 660 BTW STRG 23L-24L FRAME WITH A DENT. ACCOMPLISHED REPAIRED DENT ON FRAME AT STA 660 STR 23L - 24L PER 757-200 SRM 53-00-07-2R-5 REPAIR 5 FIG 201 DETAIL II. I
- [SDR CALA2025062605925](https://openairdocs.org/sdr/CALA2025062605925.md): Frame · dented · Jun 13, 2025 · N29124 · Boeing 757224 · Fuselage Main, Frame
  > FWD CARGO COMP. STRGR 24R-25R ST A 680 FRAME WITH DENT. REPAIRED DENT ON FRAME AT STA 680 STR 24R - 25R PER 757-200 SRM 53-00-07-2R-5 REPAIR 5 FIG 201 DETAIL III.
- [SDR CALA2025061605574](https://openairdocs.org/sdr/CALA2025061605574.md): Angle · corroded · Jun 13, 2025 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > UPON FWD LEFT WASTE DRAIN VALVE ASSEMBLY REMOVAL FOUND EXFOLIATED AREA. GAINED ACCESS TO EXFOLIATED AREA FAB 16EA REPAIR PARTS, LOCATED, DRILLED, AND INSTALLED 16EA REPAIR PARTS. CLOSED GAINED ACCESS AND PERFORMED LEAK CHECK WITH NO LEAKS DETECTED IAW SRM 51-
- [SDR CALA2025062605924](https://openairdocs.org/sdr/CALA2025062605924.md): Frame · dented · Jun 11, 2025 · N29124 · Boeing 757224 · Fuselage Main, Frame
  > FWD CARGO COMP STRG 24R STA 760 FRAME WITH DENT. REPAIRED DENT ON FRAME AT STA 760 STR 24RH PER SRM 53-00-07-2R-5 REPAIR 5 FIG 201 DETAIL III.
- [SDR CALA2025062605923](https://openairdocs.org/sdr/CALA2025062605923.md): Frame · dented · Jun 11, 2025 · N29124 · Boeing 757224 · Fuselage Main, Frame
  > FWD CARGO COMP. STA 700 BTW STRG 24L-25L FRAME WITH DENT. REPAIR PERFORMED PER SRM 53-00-07-2R-5 REPAIR 5 DETAIL III.
- [SDR CALA2025062005774](https://openairdocs.org/sdr/CALA2025062005774.md): Frame · worn · Jun 11, 2025 · N29124 · Boeing 757224 · Fuselage Main, Frame
  > FWD CARGO COMPARTMENT, LH FR CLIP STA 820 STGR 22LH TO STGR 23LH HAS MARKS. REMOVED SHEAR TIE STA 820 STR 22L-23L, FABRICATED, LOCATED AND D RILLED, INSTALLED NEW SHEAR TIE IAW B757-200 SRM 51-40-02-0G, 51 -40-05-0G-0, DWG 143N1020 REV G, VTMAE TRAVELER T25/1
- [SDR CALA2025061705610](https://openairdocs.org/sdr/CALA2025061705610.md): Frame · dented · Jun 11, 2025 · N29124 · Boeing 757224 · Fuselage Main, Frame
  > (SDR)(B757-53-3-0479-19-21-AT) FWD CARGO COMP. STA 680 BTW STRG 23L-24L FRAME WITH DENT. SFR CW WSHAW REF ESFR # 1113
- [SDR CALA2025061605573](https://openairdocs.org/sdr/CALA2025061605573.md): Rib · cracked · Jun 11, 2025 · N29124 · Boeing 757224 · Wing, Rib/Bulkhead
  > LEFT WING T/E FITTING ATTACHMENT OF AILERON OUTERMOST HINGE, UPPER FLANGE IS CRACKED. CRACKED FITTING (SUPPORT RIB) WAS REMOVED AND REPLACED BY NEW SUPPORT RIB P/N: UA-113N1511-19-1, TRAVELER #T25/1812775 IAW SRM 51-40-02 AND DWG: 113N1511 REV B.
- [SDR CALA2025062605922](https://openairdocs.org/sdr/CALA2025062605922.md): Frame · dented · Jun 10, 2025 · N29124 · Boeing 757224 · Fuselage Main, Frame
  > STA 820 L/H SIDE CAFFING AND A DENT ON LOWE R FRAME. TRIMMED FRAME DAMAGE STA 820 BETWEEN S22L-23L. FAB REPAIR J SECT ION LOCATED DRILLED AND INSTALLED PER SRM 53-00-07-2R-5 DETAIL I,
- [SDR CALA2025062005773](https://openairdocs.org/sdr/CALA2025062005773.md): Tee Angle · corroded · Jun 10, 2025 · N29124 · Boeing 757224 · Aerodynamic Fairings
  > WING TO BODY LOWER T-CHORD CORROSION AT STA. 900, 0BL LH AND RH APPROX. 8". ESFR COMPLETED. REMOVED NUTPLATES OF T-CHORD FROM STA 900 IAW B757-200 SRM 51-40 -02, EVALUATED T-CHORD FROM STA 900 BTW LBL8 TO RBL8, FOUND WAS EXFOLIATION THEREFORE IS OUT OF LIMITS
- [SDR CALA2025062005772](https://openairdocs.org/sdr/CALA2025062005772.md): Floor Support · cracked · Jun 10, 2025 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON MAIN CABIN FLOOR SUPPORT AN GLE BETWEEN STA 1420-1440. ESFR COMPLETED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-40-02, RECEIVED NEW SUPPO RT ANGLE FROM FAB SHOP, TRAVELLER #T25/1813383, INSTALLED SUPPOR T ANGLE IAW SRM 51-40-02.
- [SDR CALA2025062005771](https://openairdocs.org/sdr/CALA2025062005771.md): Support · corroded · Jun 10, 2025 · N29124 · Boeing 757224 · Aerodynamic Fairings
  > LWR MID FUSELAGE FR860 TO FR900 LBL 6 FAIR ING SUPPORT HAS CORROSION AS MARKED. ESFR COMPLETED. ADD EMP:V917067 REMOVED CORROSION IAW B757-200 SRM 51-10-02-0G, EVALUATED AREA W ITH FOLLOWING MEASURES: ORIGINAL THICKNESS: 0.080", REMAINING TH ICKNESS: 0.072", T
- [SDR CALA2025061605572](https://openairdocs.org/sdr/CALA2025061605572.md): Panel · cracked · Jun 9, 2025 · N29124 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE GAP PAN EL HAS A CRACK. REPAIRED RT WING L/E GAP PANEL. IAW SRM 57-41-01-2R-3 REPAIR 3.
- [SDR CALA2025061205496](https://openairdocs.org/sdr/CALA2025061205496.md): Floor Support · cracked · Jun 9, 2025 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON MAIN CABIN FLOOR SUPPORT A NGLE BETWEEN STA 1320-1340 BL 0. REMOVED SUPPORT ANGLE STA 1320-1340 BL0, FABRICATED NEW SUPPORT ANGLE ON VTMAE TRAVELER T25/1813382. LOCATED DRILLED AND INSTALL ED NEW SUPPORT ANGLE IAW B757-200 SRM 51-40 -02 51-40-
- [SDR CALA2025061205495](https://openairdocs.org/sdr/CALA2025061205495.md): Frame Splice · worn · Jun 9, 2025 · N29124 · Boeing 757224 · Fuselage Main, Frame
  > FWD CARGO COMP. STA 740 BTW STRG 24L-26L FRAME SPLICE WORN. ESFR COMPLETED. ADD EMP:V950831 DAMAGE WAS EVALUATE NO REPLACED FRAME SPLICE AT FWD CARGO COMP C OMP STA 740 BTW STRG 24L-26L IAW B757-200 SRM 51-40-2 NOT RII. NOT MAJOR REPAIR.
- [SDR CALA2025060905385](https://openairdocs.org/sdr/CALA2025060905385.md): Floor Support · cracked · Jun 7, 2025 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AT FWD CARGO COMPARTMENT CEILING AREA FLOOR SUPPORT INTERCOSTAL AT STA 720 RBL25 ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW B757-200 SRM 51- 40-02-0G.
- [SDR CALA2025062005770](https://openairdocs.org/sdr/CALA2025062005770.md): Web · corroded · Jun 5, 2025 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (53-2060-1-1633) AFT PIT BETWEEN STA 1280 AND 1300 AT STRINGER 2 7 L/H SIDE WEB HAS CORROSION. DOT 140-014 ESFR COMPLETED. REMOVED AND EVALUATED CORROSION AT INTERCOSTAL WEB. FOUND AT LIM ITS IAW B757-200 SRM 53-00-04-1A OT:0.32, ML:0.007" (-97483),REM OVED
- [SDR CALA2025060205171](https://openairdocs.org/sdr/CALA2025060205171.md): Frame · worn · May 31, 2025 · N29124 · Boeing 757224 · Rudder Structure
  > RUDDER LH GAP SEAL PANEL ATTACHMENT FRAME LWR END IS WORN (MARKED) SFR REPORTING ONLY REMOVED AND REPLACED BEAM WITH P/N 7075-T6511 ON RUDDER LH GAP S EAL PANEL ATTACHMENT FRAME LWR IAW B757-200 SRM 51-40-02.
- [SDR CALA2025060205170](https://openairdocs.org/sdr/CALA2025060205170.md): Angle · worn · May 31, 2025 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > PANEL 324AL LWR ATTACHMENT FRAME RIVETED TO FUSELAGE SKIN IS WORN (MARKED). SFR REPORTING ONLY REMOVED AND REPLACED ANGLE P/N 148N3140-1 BTCH 4398237 ON PANEL 324ALLWR ATTACHMENT FRAME RIVETED TO FUSELAGE SKIN IAW B757-200 SRM 51-40-02.
- [SDR CALA2025032103045](https://openairdocs.org/sdr/CALA2025032103045.md): Divider · leaking · Mar 20, 2025 · N29124 · Boeing 757224 · APU Engine Fuel and Control
  > STRONG FUEL ODOR W/APU RUNNING AND PACKS ON REF L/P 4230884 FOUND AND FIXED APU FUEL FLOW DIVIDER FUEL LEAK. TAXIED AIRCRAFT FOR 30 MINUTES. NO FUEL SMELL DETECTED IN FLIGHT DECK OR CABIN. OK TO CONTINUE.
- [SDR CALA2025020302175](https://openairdocs.org/sdr/CALA2025020302175.md): Slide · not reported · Jan 31, 2025 · N29124 · Boeing 757224 · Emergency Equipment
  > REMOVED SERVICEABLE DOOR R4 ESCAPE SLIDE IRW TASK CARD 5210-03349-006. INSTALLED (SAME)R4 DOOR MOUNTED EMERGENCY ESCAPE SLIDE IAW AMM 25-66-01-404-044, OPS CHECK GOOD C/W RII FOR THE INSTALLATION AND ACTIVATION OF THE R4 DOOR ESCAPE SLIDE PER THE GMM
- [SDR CALA2025011301884](https://openairdocs.org/sdr/CALA2025011301884.md): Elec Connector · damaged · Jan 9, 2025 · N29124 · Boeing 757224 · Equipment/Furnishings Wiring
  > DURING RT OVERWING SLIDE CHANGE FOUND CONNECTOR D05546, RT SLIDE VALVE SQUIB (M10570) DAMAGED. REPLACED CONNECTOR D05546, PER SWPM 20-65-21-1, REF WDM 25-65-21-1. SQIUB OPS CKS GOOD.
- [SDR CALA2024112501261](https://openairdocs.org/sdr/CALA2024112501261.md): Oven · faulty · Nov 23, 2024 · N29124 · Boeing 757224 · Buffet/Galleys
  > BURNING SMELL AFT GALLEY. SMOKE ODOR FORM UPDATE. FOUND ALL 3 AFT GALLEY OVENS STAINED WITH OILY BURNT SUBSTANCE, REF. PHOTOS. REQUESTING MEL FOR ALL "3" OVENS IN AFT GALLEY TO BE REPLACED. PERFORMED AMM 05-51-58-910-801-C1 FOUND THE "3" OVENS IN THE AFT GALL
- [SDR CALA2024092300668](https://openairdocs.org/sdr/CALA2024092300668.md): Unknown · smoke · Sep 21, 2024 · N29124 · Boeing 757224 · Air Distribution System
  > CREW REPORTED SMOKE AND ODOR ON CLIMB @ 170 IN FLIGHT DECK AND MID CABIN. DISSIPATED SHORTLY THERE AFTER WITH NO EICAS MESSAGES OR VISUAL FAULTS ON OVERHEAD PANEL. CREW NEEDS TO FILL OUT SMOKE ODOR FORM 46-6020 AND WORK AMM TASK 05-51-58-910-801-C1 SMOKE ODOR
- [SDR CALA2024090200529](https://openairdocs.org/sdr/CALA2024090200529.md): Actuator · failed · Aug 31, 2024 · N29124 · Boeing 757224 · Landing Gear Retraction/Extension System
  > ON DEPT GOT L HYD FLUID ALL FLUID W/ 0/ZERO HYD IND...PTU ON STA TUS PG PER CREW DEBRIEF. SHORTLY AFTER TAKE-OFF AND DURING GEAR RETRACTION, CREW NOTICED L HYD FLUID LOSS TO 40% THEN 0%. LEFT GEAR STAYED DOWN. NOSE GEAR AND RIGHT GEAR RETRACTED STAYING UP. POW
- [SDR CALA2024083002337](https://openairdocs.org/sdr/CALA2024083002337.md): Hydraulic Line · unserviceable · Aug 29, 2024 · N29124 · Boeing 757224 · Hydraulic System, Main
  > L HYD QTY AND L SYS PRESS EICAS. L HYD QTY 0.13 RF FOUND LEFT MAIN GEAR DOWNLOCK ACTUATOR HYDRAULIC LINE BURST. PN SYSTEM TO NORMAL LEVEL. VISUALLY INSPECTED BOTH ENGINE AND 19-3232-3-0060,QTY:1 19-2911-3-0116,QTY:1 00-0585-3-0287,QTY 19-3232-3-0060. REM
- [SDR CALA2024062801923](https://openairdocs.org/sdr/CALA2024062801923.md): Fmc · faulted · Jun 27, 2024 · N29124 · Boeing 757224 · Flight Management Computing Hardware System
  > AUTO PIILOT/ A/T FMC FAILURE MULTI TIME CURRENT FAULTS PER MCDP BITE FOR PREV FLT FAULTS ARE A/P CTN FMC L-R CH PERFORMED MCDP TEST 1 (FCC), 10 (A/T) AND 30 WITH NO DEFECTS - 34-61-00 WITH NO DEFECTS. A/C REMAINS FULL CAT QUALIFIED. T/S DIAG CODES 110081, 120
- [SDR CALA2024022700552](https://openairdocs.org/sdr/CALA2024022700552.md): Actuator · disconnected · Feb 24, 2024 · N29124 · Boeing 757224 · Leading Edge Slat Control System
  > LE SLAT ASYM EICAS FOUND "RT SLAT DRIVE" FAULT ON FLAP/SLAT ELEX UNIT 1 WITH MSG 325. ALSO RIGHT OUTBOARD SLATS ARE LOCKED AT TAKEOFF POSITION (THEY WILL NOT MOVE). TRIE TO RETRACT ELECTRICALLY, NO HELP. AFTER PANEL REMOVAL FOUND TORQUE TUBES DISCONNECTED FROM
- [SDR CALA2024010400025](https://openairdocs.org/sdr/CALA2024010400025.md): Controller · malfunctioned · Jan 3, 2024 · N29124 · Boeing 757224 · Cabin Pressure Controller
  > CAB DIFF STEADY CLMB INTO AMBER BAND.STAYED IN AMBER BAND JUST B ELOW RED MAX DIFF LINE CAPT. STATED A/C WAS IN AUTO 1 MODE, MODE SELECTOR WAS NEVER MOVED. OUTFLOW VALVE NEVER CLOSED BEYOND 1/2 WAY AT 25000 THROUGH 35000 FT. WALKED AROUND AIRCRAFT FOUND NOTHI
- [SDR CALA2023121303632](https://openairdocs.org/sdr/CALA2023121303632.md): Bracket · corroded · Dec 11, 2023 · N29124 · Boeing 757224 · Fuselage Main, Structure
  > WHILE WORKING NR 164654-0300-0006, FOUND APU INLET DOOR FRAME FORWARD STRAP CORRODED @ STA 1781 FROM S3R TO S6R. REMOVED AND REPLACED CORRODED STRAP P/N 148N3138-20 IAW B757 SRM 51-40-02 PARA 7 AND 9 SDR 1034547
- [SDR CALA2023121303630](https://openairdocs.org/sdr/CALA2023121303630.md): Angle · corroded · Dec 11, 2023 · N29124 · Boeing 757224 · Fuselage Miscellaneous Structure
  > CORROSION ON THE UPPER SIDE OF THE LOWER CHORD ON STR. 6R, IN THE AFT ACCESSORY, AT STA. 1819, JUST BELOW THE AFT O/B CORNER OF THE APU AIR INLET DOOR ASSEMBLY. REMOVED AND REPLACED APU INLET DOOR CHORD I.A.W B757 SRM 51-40-0 2 PAR 7 SDR 1034545
- [SDR CALA2023120803600](https://openairdocs.org/sdr/CALA2023120803600.md): Frame · cracked · Dec 6, 2023 · N29124 · Boeing 757200 · Fuselage Main, Frame
  > PANEL 571BB REINFORCEMENT FRAME CRACKED.
- [SDR CALA2023120803598](https://openairdocs.org/sdr/CALA2023120803598.md): Panel · worn · Dec 6, 2023 · N29124 · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > HINGE PANEL 415FL HAS A MISSING RIVET AND SKIN IS CHAFFED.
- [SDR CALA2023020800373](https://openairdocs.org/sdr/CALA2023020800373.md): Flap · not reported · Feb 8, 2023 · N29124 · Boeing 757200 · Trailing Flap Position Indicating System
  > TE FLAP DISAGREE EICAS FLAPS 20 USING ALT SYS PERFORMED OPS CHECK OF TE FLAP SYSTEM IAW AMM 27-51-00. PERFORMED FIM 27-51-00. NO CURRENT FAULTS. UNABLE TO DUPLICATE FAULT.
- [SDR CALA2023012300185](https://openairdocs.org/sdr/CALA2023012300185.md): Slide · unknown · Jan 23, 2023 · N29124 · Boeing 757224 · Escape Slide
  > DOOR-MOUNTED ESCAPE SYSTEM DOOR 1R - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS DOOR KNUCKLE KNOCKER REMAINS FLUSH DURING ARM 1R CYCLED DOOR. AND ARMED. COULD NOT DUPLICATE ERROR. OPS CHECK GOOD.
- [SDR CALA2022091402344](https://openairdocs.org/sdr/CALA2022091402344.md): None · none · Sep 14, 2022 · N29124 · Boeing 757 · Cabin Equipment/Furnishings
  > WHEN CATERING OPENED THE DOOR 3R THE ESCAPE SLIDE GIRT BAR DETTACHED AND HANGED OUT OF THE DOOR. THE DOOR WAS PROPERLY DISSARMED AND CATERING OPS FOLLOWED ALL THE SAFETY PROCEDURES. GIRT BAR REINSTALLED PER AMM 25-66-10-402-022. GIRT BAR HANDLING 25-66-01-206-
- [SDR CALA2022061501514](https://openairdocs.org/sdr/CALA2022061501514.md): Panel · arced · Jun 15, 2022 · N29124 · Boeing 757224 · Cabin Equipment/Furnishings
  > P-37 ARCHING FOUND AMONG EXISTING WIRING AT TERMINAL LUGS AND BR EAKERS. EA 4420-02847 REV C OP 014. REPORTED BY V931833 REPLACED WIRE W1272-006-12 AND W1272-0020-08 TERMINAL LUGS TO CB 02. NO ARCHING OR FIRE DAMAGE FOUND, EXCLUDING THE DAMAGE REFERE 3-26-00.
- [SDR CALA2022061001477](https://openairdocs.org/sdr/CALA2022061001477.md): Structure · corroded · Jun 9, 2022 · N29124 · Boeing 757200 · Standard Practices/Structures
  > REF AMES NR 0100-0200 ALC DOOR CUTOUT SILL PLATE UNDERSIDE FOUND TO BE CORRODED @ STA. 1400-1410 WHILE ACC OMPLISHING REPAIR @ STA. 1390. REMOVED AND REPLACE ALC UPPER CORD AT DOOR THRESHOLD, WITH NEW P ART P/N: 146N8522-51 IAW BOEING DRAWLING: 146N8522-REV A

Next page: https://openairdocs.org/aircraft/N29124/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N29124' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N29124/reports

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