N937DM
Registered owner: PUNK TACO LOVE II LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
32 reports on file, 2023-03-21 – 2023-07-19.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2874400) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR CENTER BALANCE BAY PANEL AT OB CORNER. REPAIRED CORRODED AREA PER ERA 609520-14 REV ORIGINAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2874325) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR OB BALANCE BAY PANEL. REPAIRED AREA OF CORROSION PER ERA 609520-14 REV ORIGINAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2874287) LH HORIZONTAL STABILIZER OB TE WEDGE UPPER ATTACH ANGLE HAS AREA OF CORROSION 28 FROM OB STABILIZER TIP. REPAIRED CORRODED AREA PER ERA 609520-14 REV ORIGINAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2874425) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR IB BALANCE BAY PANEL. REPAIRED CORRODED AREA PER DELTA ERA 609520-14.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2860460) FORWARD CARGO COMPARTMENT LH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 500C + 15 AND BS 500L. LBL 26. LOCATED AND DRILLED AND INSTALLED NEW TRANSITION PANEL REPAIR SECTION IAW. B737 SRM 53-00-53-2R REPAIR 2.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2858953) DURING CHECK AT FLIGHTSTAR (VQQ), THE UPPER CHORD AT LH HORIZONTAL STAB REAR SPAR WAS FOUND WITH FOUR CORROSION SPOTS BETWEEN STAB STA 130 & STAB STA 330. REPAIRED PER ERA 609520-14.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2853856) CORROSION IN AFT CARGO COMPARTMENT FLOOR STRUCTURE CARGO TRACK-TIE DOWN SUPPORT BETWEEN BS. 795 AND BS.835 RBL.13.84. REMOVED AND REPLACED TRACK IAW B737-900 SRM 51-40-02 AND DWG# 146A7500 REV G.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,681 hrs · 17,400 cycles
(LOG 2852397) AFT CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT RAIL (CHANNEL) HAS A GOUGE AT FASTENER HOLE BS.727L+2 LBL.3.00. CUT AND REMOVED THE DAMAGE PART OF AFT CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT RAIL (CHANNEL) BS 727+2 LBL 3 DIM.3 1/8 X 1 IAW B737-900 SRM 53-00-53-2R-2 AND INSTALLED REPAIR PER B737-900 SRM 53-00-53-2R.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2852489) CORROSION AROUND FASTENER HOLES IN AFT CARGO COMPARTMENT FLOOR STRUCTURE RT SIDE TRANSITION PANEL SECTION BETWEEN BS.727I+10 AND BS.767 RBL.21.00. REMOVED AND REPLACED SECTION OF TRANSITION PANEL PER B737-900 SRM 51-40-05, 53-60-53-01-2 AND SRM 51-40-02.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2844523) RH HORIZONTAL STABILIZER OB TE WEDGE UPPER ATTACH ANGLE HAS AREA OF CORROSION 28" FROM OB STABILIZER TIP. VIEWED THRU AFT ACCESS HOLE WITH STABILIZER TIP REMOVED. REPAIRED AREA PER DELTA ERA 609707-14 REV. ORIGINAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,681 hrs · 17,400 cycles
(LOG 2844472) AFT REMOVAL OF ADF ANTENNA #1 AND #2 FOUND MULTIPLE DOME NUT DAMAGE. REPAIRED ADF ANTENNA #1 AND #2 DOME NUTS PER DELTA ERA 608966-14 REV ORIGINAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2840745) FWD ADF ANTENNA AREA, ON TOP OF THE FUSELAGE, CORROSION AROUND THE FASTENER HOLES. REPAIRED AFFECTED AREAS PER DELTA ERA 609634-14 REV. ORIGINAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2840722) AFT ADF ANTENNA AREA, CORROSION FOUND AROUND THE FASTENER HOLES. REPAIRED AFFECTED AREAS PER DELTA ERA 609424-14 REV ORIGINAL.
Part: PANEL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2830077) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 500A AND BS 500 L RBL 26. INSTALLED NEW FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL BS 500A TO BS 500 L. RBL 26. IAW B737 SRM 51-40-02 AND SRM 53-30-53-01.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,681 hrs · 17,400 cycles
(LOG 2830670) LOCATED PREVIOUS BLENDOUT AT FUSELAGE SKIN STA 500A-500B, STR 22-21R. REPAIRED PREVIOUS BLENDOUT AREA OF FUSELAGE SKIN STA 500A-500B, STR 22-21R PER DELTA ERA 609136-14 REV ORIGINAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2828990) CORROSION AROUND FASTENER HOLES IN AFT CARGO COMPARTMENT FLOOR STRUCTURE LT SIDE TRANSITION PANEL SECTION BETWEEN BS.727A AND BS.727I+8 LBL.21.00. REMOVED, FABRICATED NEW SECTION AND INSTALLED IAW B737-900 SRM 51-40-02.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2827423) AFT CARGO ENTRY PANEL UNDER THRESHOLD HAS MULTIPLE AREAS OF CORROSION. REPAIRED AREA PER DELTA ERA 609690-14 REV ORIGINAL.
Part: SUPPORT FITTING — CORRODED (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2825881) RH AFT LAVATORY SUPPORT BEAM AT BS 953 HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN RBL 25 AND RBL 35. REMOVED AND REPLACED LAVATORY SUPPORT PER B737-900 SRM 51-40-05, 57-70-57-1A AND SRM 51-40-02.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,681 hrs · 17,400 cycles
(LOG 2821274) AFT CARGO FWD CUTOUT PANEL LWR CORNER DAMAGED. FABRICATE NEW AFT CARGO FWD CUTOUT PANEL DIM. 52.5 X 5.1 FROM MATERIAL 6013-T4 .050 IAW B737-900 SRM 51-40-05, 53-60-15 AND DWG# 146A9403 REV. A.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2821178) CORROSION AROUND FASTENER HOLES IN AFT CARGO COMPARTMENT LT SIDE TRANSITION PANEL SECTION BETWEEN BS.727K+10 AND BS.847 LBL 21.00. REMOVED CORROSION AT AROUND FASTENER HOLES IN AFT CARGO COMPARTMENT LT SIDE TRANSITION PANEL SECTION BETWEEN BS.727K+10" AND BS.847 LBL.21.00. IAW B737 SRM 51-10-02, LOCATED AND DRILLED AND INSTALLED TRANSITION PANEL IAW B737-900 SRM 51-40-05, 51-40-02.
Part: WEB — CORRODED (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2818886) FORWARD CARGO COMPARTMENT DOOR CUT OUT LOWER SILL HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 440 AND BS 490. INSTALLED NEW WEB AT FWD CARGO COMPT DOOR CUT OUT LOWER SILL BETWEEN BS 440 AND BS 490. REF USED DELTA PSM 900-2 NO. 09, DELTA PSM 900-1 NO. 07, SRM 51-10-02-0G, SRM 51-40-02-G, SRM 51-40-05-0G, SRM 51-20-01-0G.
Part: PANEL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2818828) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER AND LOWER SURFACE BETWEEN BS 490 AND BS 500A. RBL 26. REMOVED FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL BS 490 AND BS 500A. RBL 26 IAW B737 SRM 51-40-02. LOCATED, DRILLED, AND DEBURRED NEW TRANSITION PANEL IAW B737 SRM 51-40-05. TREATED AND PRIMED HOLES IAW B737 SRM 51-20-01. INSTALLED NEW FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL BS 490-500A RBL 26 IAW B737 SRM 51-40-02.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2818839) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 420 AND BS 440 RBL 26. LOCATED, DRILLED, AND DEBURRED NEW TRANSITION PANEL IAW B737 SRM 51-40-05. TREATED AND PRIMED HOLES IAW B737 SRM 51-20-01. INSTALLED NEW FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL BS 420 TO BS 440. RBL 26 IAW B737 SRM 51-40-02.
Part: PANEL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2815290) FORWARD CARGO COMPARTMENT LH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 400 AND BS 500C + 15 LBL 26. LOCATED AND DRILLED NEW TRANSISTION PANEL AND SPLICE FROM BAC1496-444-7075-T6 IAW B-737-900 SRM 53-00-53-2R REPAIR 6. INSTALLED NEW TRANSISTION PANEL IAW B-737-900 SRM 51-40-02
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
(LOG 2807753) MAIN CABIN FLOOR SUPPORT STA 951-967 LBL 30 CORRODED AROUND HOLE DOT 45/018. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-900 SRM 51-40-02.
Part: SEAT TRACK — CRACKED · airframe 24,681 hrs · 17,400 cycles
(LOG 2804399) MAIN CABIN LBL 45 SEAT TRACK LOWER SUPPORT IS CRACKED AT BS 727B. REMOVED AND REPLACED SEAT TRACK LOWER SUPPORT AT BS 727B LBL 45 IAW B737-900 SRM 51-40-02-0G.
Part: SEAT TRACK — CRACKED · airframe 24,681 hrs · 17,400 cycles
(LOG 2798299) MAIN CABIN RBL 45 SEAT TRACK LOWER SUPPORT IS CRACKED AT BS 727B. REMOVED AND REPLACE MAIN CABIN SEAT TRACK LOWER SUPPORT AT BS 727B RBL 45 PER B737-900 SRM 51-40-02.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,681 hrs · 17,400 cycles
MAIN CABIN BS 986.5 FLOOR BEAM UPPER SURFACE HAS AREAS OF CORROSION BETWEEN RBL 15 AND RBL 48. FABRICATED REPAIR PARTS REPAIR (1) STRAP FROM 7575T6 0.100" CLAD. INSTALLED REPAIR IAW B737 SRM 53-70-51-2R.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,677 hrs · 17,399 cycles
(LOG 2681778) DURING INSPECTION FOUND LT WING H-BLOCK ATTACH POINT UPPER INBD BORE PITTED ON INBD FACE. REMOVED BUSHING AND MACHINED .062 OFF OUTTER FACE TO REMOVE CORROSION PER B737 SRM 57-20-90. RORPEENED CHEM TREATED + PRIMED FACES. INSTALLED BUSHING PER B737 SRM 57-20-90.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,677 hrs · 17,399 cycles
(LOG 2681765) DURING INSPECTION FOUND LT WING H-BLOCK ATTACH POINT UPPER OUTBD BORE PITTED ON OUTBD FACE. REMOVED BUSHING AND MACHINED .042 OFF OUTTER FACE TO REMOVE CORROSION PER B737 SRM 57-20-90. RORPEENED CHEM TREATED + PRIMED FACES. INSTALLED BUSHING PER B737 SRM 57-20-90.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,677 hrs · 17,399 cycles
(LOG 2681785) DURING INSPECTION FOUND LT WING H-BLOCK ATTACH POINT LOWER INBD BORE PITTED ON INBD FACE. REMOVED BUSHING AND MACHINED .090 OFF OUTTER FACE TO REMOVE CORROSION PER B737 SRM 57-20-90. RORPEENED CHEM TREATED + PRIMED FACES. INSTALLED BUSHING PER B737 SRM 57-20-90.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 24,677 hrs · 17,399 cycles
(LOG 2681789) DURING INSPECTION FOUND LT WING H-BLOCK ATTACH POINT LOWER OUTBD BORE PITTED ON OUTBD FACE. REMOVED BUSHING AND MACHINED .070 OFF OUTTER FACE TO REMOVE CORROSION PER B737 SRM 57-20-90. PRIMED FACES + INSTALLED BUSHING PER B737 SRM 57-20-90.